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Merge pull request #298 from kruland2607/unstable

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Added case-info to motors.
This commit is contained in:
kruland2607 2016-10-23 13:21:24 -05:00 committed by GitHub
commit f5acd0ab1c
1769 changed files with 8487 additions and 63050 deletions
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4
core/build.xml
View File

@ -59,7 +59,7 @@
</target>
<!-- Executible Eclipse-Jar-In-Jar style JAR -->
<target name="jar" depends="build,serialize-motors" description="Create the OpenRocket Core">
<target name="jar" depends="build" description="Create the OpenRocket Core">
<mkdir dir="${jar.dir}" />
<jar destfile="${jar.file}" basedir="${dist.dir}">
@ -74,7 +74,7 @@
</target>
<target name="serialize-motors" depends="build" description="Preprocess the motor files into serialized form">
<java classname="net.sf.openrocket.utils.SerializeMotors"
<java classname="net.sf.openrocket.thrustcurve.SerializeThrustcurveMotors"
fork="true"
classpathref="run-classpath"
failonerror="true">

26
core/resources-src/datafiles/thrustcurves/manual/AT_F101T.eng
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@ -1,26 +0,0 @@
; TODO: Length and weights taken from F72!!
; Based on
; http://www.aerotech-rocketry.com/customersite/resource_library/Instructions/MR-SU_Instructions/d-f_non-std_su_in_21002.pdf
; Made by Sampo Niskanen
F101T 24 124 5-10-15 0.0368 0.0742 AT
0.04 85.95
0.069 83.4
0.129 86.461
0.202 94.622
0.274 100.743
0.354 104.569
0.443 106.099
0.446 102.783
0.546 96.662
0.575 90.031
0.602 89.011
0.625 84.675
0.671 80.85
0.731 76.259
0.771 58.406
0.807 33.921
0.85 18.108
0.893 11.477
0.942 0.0

27
core/resources-src/datafiles/thrustcurves/manual/Cesaroni_F31.rse
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@ -1,27 +0,0 @@
<engine-database>
<engine-list>
<engine mfg="CTI" code="56-F31-CL-12A" Type="unspecified" dia="29." len="98.0008"
initWt="102." propWt="32." delays="13,9,7,5,3" auto-calc-mass="1"
auto-calc-cg="1" avgThrust="30.41" peakThrust="64.053" throatDia="0."
exitDia="0." Itot="55.589" burn-time="1.83" massFrac="31.37" Isp="177.14"
tDiv="10" tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10"
mStep="-1." mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<comments>CTI 56-F31-CL-12A</comments>
<data>
<eng-data t="0." f="0." m="32." cg="49."/>
<eng-data t="0.001" f="3.483" m="31.999" cg="49."/>
<eng-data t="0.023" f="64.053" m="31.5714" cg="49."/>
<eng-data t="0.05" f="31.347" m="30.83" cg="49."/>
<eng-data t="0.059" f="28.459" m="30.6751" cg="49."/>
<eng-data t="0.095" f="32.027" m="30.0483" cg="49."/>
<eng-data t="0.212" f="36.189" m="27.7511" cg="49."/>
<eng-data t="0.344" f="37.549" m="24.9496" cg="49."/>
<eng-data t="1.567" f="26.165" m="2.5217" cg="49."/>
<eng-data t="1.631" f="26.93" m="1.54365" cg="49."/>
<eng-data t="1.663" f="25.316" m="1.06244" cg="49."/>
<eng-data t="1.785" f="3.653" m="0.0452111" cg="49."/>
<eng-data t="1.828" f="0." m="0." cg="49."/>
</data>
</engine>
</engine-list>
</engine-database>

27
core/resources-src/datafiles/thrustcurves/manual/Loki_J175.rse
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@ -1,27 +0,0 @@
<engine-database>
<engine-list>
<engine FDiv="10" FFix="1" FStep="-1." Isp="199.98" Itot="1157.08" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="178.012" burn-time="6.5" cgDiv="10" cgFix="1" cgStep="-1." code="J175" delays="1000" dia="54." exitDia="0." initWt="1264." len="327." mDiv="10" mFix="1" mStep="-1." massFrac="46.68" mfg="Loki Research" peakThrust="420.4" propWt="590." tDiv="10" tFix="1" tStep="-1." throatDia="0.">
<data>
<eng-data cg="163.5" f="0." m="590." t="0."/>
<eng-data cg="163.5" f="4.8" m="589.988" t="0.01"/>
<eng-data cg="163.5" f="420.4" m="580.231" t="0.1"/>
<eng-data cg="163.5" f="347.5" m="560.653" t="0.2"/>
<eng-data cg="163.5" f="349.9" m="542.873" t="0.3"/>
<eng-data cg="163.5" f="364.5" m="524.659" t="0.4"/>
<eng-data cg="163.5" f="320.7" m="507.19" t="0.5"/>
<eng-data cg="163.5" f="296.4" m="428.524" t="1."/>
<eng-data cg="163.5" f="279.4" m="355.123" t="1.5"/>
<eng-data cg="163.5" f="260." m="286.363" t="2."/>
<eng-data cg="163.5" f="238.1" m="222.867" t="2.5"/>
<eng-data cg="163.5" f="209." m="165.872" t="3."/>
<eng-data cg="163.5" f="172." m="117.304" t="3.5"/>
<eng-data cg="163.5" f="133.6" m="78.3469" t="4."/>
<eng-data cg="163.5" f="102." m="48.3135" t="4.5"/>
<eng-data cg="163.5" f="75.3" m="25.712" t="5."/>
<eng-data cg="163.5" f="46.2" m="10.2236" t="5.5"/>
<eng-data cg="163.5" f="17." m="2.1671" t="6."/>
<eng-data cg="163.5" f="0." m="0." t="6.5"/>
</data>
</engine>
</engine-list>
</engine-database>

3
core/resources-src/datafiles/thrustcurves/manual/README.txt
View File

@ -7,6 +7,3 @@ WECO_*.eng - Thrust curves for Weco Feuerwerk motors, created by Sampo N.
Klima_*.eng - Thrust curves for Klima motors, created by Leo Nutz
Loki_J175.rse - Corrected motor type from hybrid to reloadable
CTI F31 - Correct diameter to 29mm

11591
core/resources-src/datafiles/thrustcurves/thrustcurve.org/00INDEX.txt
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File diff suppressed because it is too large Load Diff

33
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AMW_I195.eng
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@ -1,33 +0,0 @@
;Animal Motor Works 38-390
I195WT 38 249 17 0.193 0.495 AMW
0.0020 10.548
0.018 42.653
0.046 136.214
0.064 179.784
0.072 191.248
0.078 197.211
0.088 198.587
0.126 198.587
0.175 207.759
0.217 211.887
0.349 216.931
0.401 221.059
0.554 225.646
0.586 228.856
0.626 228.48
0.65 230.232
1.013 231.607
1.105 230.691
1.2 225.187
1.356 210.511
1.392 207.759
1.441 206.842
1.457 205.007
1.519 181.159
1.563 155.936
1.693 49.992
1.727 28.435
1.756 16.512
1.798 7.338
1.86 1.376
1.89 0.0

46
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AMW_I195.rse
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@ -1,46 +0,0 @@
<engine-database>
<engine-list>
<engine mfg="Animal Motor Works" code="I195WW" Type="reloadable" dia="38." len="249."
initWt="495." propWt="193." delays="18" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="185.064" peakThrust="231.607" throatDia="0." exitDia="0."
Itot="349.772" burn-time="1.89" massFrac="38.99" Isp="184.8" tDiv="10"
tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."
mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<comments>Animal Motor Works 38-390</comments>
<data>
<eng-data t="0." f="0." m="193." cg="124.5"/>
<eng-data t="0.002" f="10.548" m="192.994" cg="124.5"/>
<eng-data t="0.018" f="42.653" m="192.759" cg="124.5"/>
<eng-data t="0.046" f="136.214" m="191.378" cg="124.5"/>
<eng-data t="0.064" f="179.784" m="189.808" cg="124.5"/>
<eng-data t="0.072" f="191.248" m="188.989" cg="124.5"/>
<eng-data t="0.078" f="197.211" m="188.346" cg="124.5"/>
<eng-data t="0.088" f="198.587" m="187.254" cg="124.5"/>
<eng-data t="0.126" f="198.587" m="183.09" cg="124.5"/>
<eng-data t="0.175" f="207.759" m="177.597" cg="124.5"/>
<eng-data t="0.217" f="211.887" m="172.734" cg="124.5"/>
<eng-data t="0.349" f="216.931" m="157.118" cg="124.5"/>
<eng-data t="0.401" f="221.059" m="150.834" cg="124.5"/>
<eng-data t="0.554" f="225.646" m="131.978" cg="124.5"/>
<eng-data t="0.586" f="228.856" m="127.965" cg="124.5"/>
<eng-data t="0.626" f="228.48" m="122.918" cg="124.5"/>
<eng-data t="0.65" f="230.232" m="119.881" cg="124.5"/>
<eng-data t="1.013" f="231.607" m="73.6278" cg="124.5"/>
<eng-data t="1.105" f="230.691" m="61.8937" cg="124.5"/>
<eng-data t="1.2" f="225.187" m="49.9451" cg="124.5"/>
<eng-data t="1.356" f="210.511" m="31.1929" cg="124.5"/>
<eng-data t="1.392" f="207.759" m="27.0386" cg="124.5"/>
<eng-data t="1.441" f="206.842" m="21.4336" cg="124.5"/>
<eng-data t="1.457" f="205.007" m="19.6156" cg="124.5"/>
<eng-data t="1.519" f="181.159" m="13.0101" cg="124.5"/>
<eng-data t="1.563" f="155.936" m="8.91797" cg="124.5"/>
<eng-data t="1.693" f="49.992" m="1.5321" cg="124.5"/>
<eng-data t="1.727" f="28.435" m="0.796427" cg="124.5"/>
<eng-data t="1.756" f="16.512" m="0.436809" cg="124.5"/>
<eng-data t="1.798" f="7.338" m="0.160446" cg="124.5"/>
<eng-data t="1.86" f="1.376" m="0.0113889" cg="124.5"/>
<eng-data t="1.89" f="0." m="0." cg="124.5"/>
</data>
</engine>
</engine-list>
</engine-database>

29
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AMW_I220.eng
View File

@ -1,29 +0,0 @@
;Animal Motor Works 38-390
I220SK 38 249 20 0.202 0.495 AMW
0.0050 12.747
0.019 45.25
0.036 79.666
0.052 125.554
0.069 162.519
0.076 169.53
0.095 174.629
0.167 176.541
0.229 191.199
0.447 235.175
0.602 260.668
0.733 288.073
0.85 302.095
0.974 301.457
1.094 289.985
1.184 268.954
1.268 240.273
1.302 219.879
1.388 177.178
1.418 147.224
1.435 127.467
1.473 91.139
1.504 65.645
1.543 40.789
1.593 19.12
1.622 10.197
1.65 0.0

42
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AMW_I220.rse
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@ -1,42 +0,0 @@
<engine-database>
<engine-list>
<engine mfg="Animal Motor Works" code="I220SK" Type="reloadable" dia="38." len="249."
initWt="495." propWt="202." delays="20" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="213.153" peakThrust="302.095" throatDia="0." exitDia="0."
Itot="351.702" burn-time="1.65" massFrac="40.81" Isp="177.54" tDiv="10"
tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."
mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<comments>Animal Motor Works 38-390</comments>
<data>
<eng-data t="0." f="0." m="202." cg="124.5"/>
<eng-data t="0.005" f="12.747" m="201.982" cg="124.5"/>
<eng-data t="0.019" f="45.25" m="201.749" cg="124.5"/>
<eng-data t="0.036" f="79.666" m="201.139" cg="124.5"/>
<eng-data t="0.052" f="125.554" m="200.196" cg="124.5"/>
<eng-data t="0.069" f="162.519" m="198.789" cg="124.5"/>
<eng-data t="0.076" f="169.53" m="198.122" cg="124.5"/>
<eng-data t="0.095" f="174.629" m="196.244" cg="124.5"/>
<eng-data t="0.167" f="176.541" m="188.983" cg="124.5"/>
<eng-data t="0.229" f="191.199" m="182.435" cg="124.5"/>
<eng-data t="0.447" f="235.175" m="155.743" cg="124.5"/>
<eng-data t="0.602" f="260.668" m="133.672" cg="124.5"/>
<eng-data t="0.733" f="288.073" m="113.028" cg="124.5"/>
<eng-data t="0.85" f="302.095" m="93.1987" cg="124.5"/>
<eng-data t="0.974" f="301.457" m="71.7064" cg="124.5"/>
<eng-data t="1.094" f="289.985" m="51.3247" cg="124.5"/>
<eng-data t="1.184" f="268.954" m="36.8785" cg="124.5"/>
<eng-data t="1.268" f="240.273" m="24.5946" cg="124.5"/>
<eng-data t="1.302" f="219.879" m="20.1017" cg="124.5"/>
<eng-data t="1.388" f="177.178" m="10.2956" cg="124.5"/>
<eng-data t="1.418" f="147.224" m="7.50077" cg="124.5"/>
<eng-data t="1.435" f="127.467" m="6.15974" cg="124.5"/>
<eng-data t="1.473" f="91.139" m="3.77417" cg="124.5"/>
<eng-data t="1.504" f="65.645" m="2.37841" cg="124.5"/>
<eng-data t="1.543" f="40.789" m="1.18637" cg="124.5"/>
<eng-data t="1.593" f="19.12" m="0.326147" cg="124.5"/>
<eng-data t="1.622" f="10.197" m="0.0819931" cg="124.5"/>
<eng-data t="1.65" f="0." m="0." cg="124.5"/>
</data>
</engine>
</engine-list>
</engine-database>

16
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AMW_I223.eng
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@ -1,16 +0,0 @@
; CTI Pro38-4G 434 I223 Skidmark 14A
I223SK 38 302 5-7-9-11-14 0.266 0.494 CTI
0.016 199.183
0.024 260.157
0.07 207.313
0.148 227.637
0.425 244.71
0.721 254.466
1.015 256.905
1.3 248.775
1.459 240.645
1.615 234.954
1.712 195.931
1.782 119.51
1.9 24.39
1.984 0.0

29
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AMW_I223.rse
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@ -1,29 +0,0 @@
<engine-database>
<engine-list>
<engine mfg="CTI" code="I223SK" Type="unspecified" dia="38." len="302." initWt="494."
propWt="266." delays="5,7,9,11,14" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="219.321" peakThrust="260.157" throatDia="0." exitDia="0."
Itot="435.133" burn-time="1.98" massFrac="53.85" Isp="166.81" tDiv="10"
tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."
mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<comments>CTI Pro38-4G 434 I223 Skidmark 14A</comments>
<data>
<eng-data t="0." f="0." m="266." cg="151."/>
<eng-data t="0.016" f="199.183" m="265.026" cg="151."/>
<eng-data t="0.024" f="260.157" m="263.903" cg="151."/>
<eng-data t="0.07" f="207.313" m="257.33" cg="151."/>
<eng-data t="0.148" f="227.637" m="246.96" cg="151."/>
<eng-data t="0.425" f="244.71" m="206.969" cg="151."/>
<eng-data t="0.721" f="254.466" m="161.807" cg="151."/>
<eng-data t="1.015" f="256.905" m="115.854" cg="151."/>
<eng-data t="1.3" f="248.775" m="71.8032" cg="151."/>
<eng-data t="1.459" f="240.645" m="48.0179" cg="151."/>
<eng-data t="1.615" f="234.954" m="25.3404" cg="151."/>
<eng-data t="1.712" f="195.931" m="12.5654" cg="151."/>
<eng-data t="1.782" f="119.51" m="5.81627" cg="151."/>
<eng-data t="1.9" f="24.39" m="0.626211" cg="151."/>
<eng-data t="1.984" f="0." m="0." cg="151."/>
</data>
</engine>
</engine-list>
</engine-database>

27
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AMW_I271.eng
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@ -1,27 +0,0 @@
;
; AMW 38-390
I271BB 38 258 0 0.189 0.493 AMW
0.011 119.530
0.035 213.907
0.050 245.903
0.074 262.705
0.115 269.446
0.225 267.736
0.346 282.929
0.465 296.411
0.584 303.152
0.727 311.504
0.916 318.245
1.054 324.986
1.162 331.400
1.201 326.696
1.225 313.214
1.242 286.249
1.268 240.990
1.294 188.888
1.323 136.833
1.346 87.565
1.368 45.467
1.392 18.523
1.430 0.000
;

38
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AMW_I271.rse
View File

@ -1,38 +0,0 @@
<engine-database>
<engine-list>
<engine mfg="Animal Motor Works" code="I271BB" Type="reloadable" dia="38." len="258."
initWt="493." propWt="189." delays="20" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="272.271" peakThrust="331.4" throatDia="0." exitDia="0." Itot="389.348"
burn-time="1.43" massFrac="38.34" Isp="210.07" tDiv="10" tStep="-1." tFix="1"
FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10"
cgStep="-1." cgFix="1">
<comments>AMW 38-390</comments>
<data>
<eng-data t="0." f="0." m="189." cg="129."/>
<eng-data t="0.011" f="119.53" m="188.681" cg="129."/>
<eng-data t="0.035" f="213.907" m="186.739" cg="129."/>
<eng-data t="0.05" f="245.903" m="185.065" cg="129."/>
<eng-data t="0.074" f="262.705" m="182.102" cg="129."/>
<eng-data t="0.115" f="269.446" m="176.806" cg="129."/>
<eng-data t="0.225" f="267.736" m="162.464" cg="129."/>
<eng-data t="0.346" f="282.929" m="146.292" cg="129."/>
<eng-data t="0.465" f="296.411" m="129.559" cg="129."/>
<eng-data t="0.584" f="303.152" m="112.242" cg="129."/>
<eng-data t="0.727" f="311.504" m="90.9086" cg="129."/>
<eng-data t="0.916" f="318.245" m="62.0202" cg="129."/>
<eng-data t="1.054" f="324.986" m="40.4755" cg="129."/>
<eng-data t="1.162" f="331.4" m="23.2696" cg="129."/>
<eng-data t="1.201" f="326.696" m="17.0402" cg="129."/>
<eng-data t="1.225" f="313.214" m="13.3127" cg="129."/>
<eng-data t="1.242" f="286.249" m="10.8392" cg="129."/>
<eng-data t="1.268" f="240.99" m="7.51204" cg="129."/>
<eng-data t="1.294" f="188.888" m="4.79927" cg="129."/>
<eng-data t="1.323" f="136.833" m="2.50662" cg="129."/>
<eng-data t="1.346" f="87.565" m="1.25394" cg="129."/>
<eng-data t="1.368" f="45.467" m="0.543589" cg="129."/>
<eng-data t="1.392" f="18.523" m="0.17084" cg="129."/>
<eng-data t="1.43" f="0." m="0." cg="129."/>
</data>
</engine>
</engine-list>
</engine-database>

31
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AMW_I285.eng
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@ -1,31 +0,0 @@
;
; AMW 38-390
I285GG 38 258 0 0.206 0.515 AMW
0.013 61.575
0.032 119.327
0.055 164.575
0.076 191.004
0.094 201.014
0.139 212.326
0.232 231.247
0.357 258.876
0.456 267.686
0.592 278.998
0.716 289.358
0.841 291.200
0.936 290.310
1.051 285.204
1.139 277.696
1.204 280.199
1.243 278.998
1.265 268.887
1.286 242.559
1.319 187.200
1.359 134.443
1.387 86.702
1.407 52.776
1.428 31.413
1.448 16.337
1.465 5.026
1.480 0.000
;

42
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AMW_I285.rse
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@ -1,42 +0,0 @@
<engine-database>
<engine-list>
<engine mfg="Animal Motor Works" code="I285GG" Type="reloadable" dia="38." len="258."
initWt="515." propWt="206." delays="20" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="238.835" peakThrust="291.2" throatDia="0." exitDia="0." Itot="353.476"
burn-time="1.48" massFrac="40." Isp="174.97" tDiv="10" tStep="-1." tFix="1"
FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10"
cgStep="-1." cgFix="1">
<comments>AMW 38-390</comments>
<data>
<eng-data t="0." f="0." m="206." cg="129."/>
<eng-data t="0.013" f="61.575" m="205.767" cg="129."/>
<eng-data t="0.032" f="119.327" m="204.765" cg="129."/>
<eng-data t="0.055" f="164.575" m="202.862" cg="129."/>
<eng-data t="0.076" f="191.004" m="200.687" cg="129."/>
<eng-data t="0.094" f="201.014" m="198.63" cg="129."/>
<eng-data t="0.139" f="212.326" m="193.21" cg="129."/>
<eng-data t="0.232" f="231.247" m="181.19" cg="129."/>
<eng-data t="0.357" f="258.876" m="163.338" cg="129."/>
<eng-data t="0.456" f="267.686" m="148.148" cg="129."/>
<eng-data t="0.592" f="278.998" m="126.483" cg="129."/>
<eng-data t="0.716" f="289.358" m="105.947" cg="129."/>
<eng-data t="0.841" f="291.2" m="84.8006" cg="129."/>
<eng-data t="0.936" f="290.31" m="68.7031" cg="129."/>
<eng-data t="1.051" f="285.204" m="49.4176" cg="129."/>
<eng-data t="1.139" f="277.696" m="34.9835" cg="129."/>
<eng-data t="1.204" f="280.199" m="24.4167" cg="129."/>
<eng-data t="1.243" f="278.998" m="18.0618" cg="129."/>
<eng-data t="1.265" f="268.887" m="14.5496" cg="129."/>
<eng-data t="1.286" f="242.559" m="11.4199" cg="129."/>
<eng-data t="1.319" f="187.2" m="7.28737" cg="129."/>
<eng-data t="1.359" f="134.443" m="3.53841" cg="129."/>
<eng-data t="1.387" f="86.702" m="1.7341" cg="129."/>
<eng-data t="1.407" f="52.776" m="0.921243" cg="129."/>
<eng-data t="1.428" f="31.413" m="0.406072" cg="129."/>
<eng-data t="1.448" f="16.337" m="0.127793" cg="129."/>
<eng-data t="1.465" f="5.026" m="0.021968" cg="129."/>
<eng-data t="1.48" f="0." m="0." cg="129."/>
</data>
</engine>
</engine-list>
</engine-database>

19
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AMW_I297.eng
View File

@ -1,19 +0,0 @@
; CTI Pro38-5G 543 I297 Skidmark 15A
I297SM 38 360 6-8-10-12-15 0.329 0.591 CTI
0.013 340.903
0.036 375.121
0.069 354.844
0.129 335.834
0.281 338.369
0.662 344.705
0.855 344.705
1.084 329.498
1.295 319.359
1.359 313.023
1.447 314.29
1.534 269.935
1.637 119.126
1.681 69.701
1.74 40.554
1.846 12.673
1.943 0.0

32
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AMW_I297.rse
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@ -1,32 +0,0 @@
<engine-database>
<engine-list>
<engine mfg="CTI" code="I297SM" Type="unspecified" dia="38." len="360." initWt="591."
propWt="329." delays="6,8,10,12,15" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="278.379" peakThrust="375.121" throatDia="0." exitDia="0."
Itot="540.889" burn-time="1.94" massFrac="55.67" Isp="167.65" tDiv="10"
tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."
mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<comments>CTI Pro38-5G 543 I297 Skidmark 15A</comments>
<data>
<eng-data t="0." f="0." m="329." cg="180."/>
<eng-data t="0.013" f="340.903" m="327.652" cg="180."/>
<eng-data t="0.036" f="375.121" m="322.644" cg="180."/>
<eng-data t="0.069" f="354.844" m="315.318" cg="180."/>
<eng-data t="0.129" f="335.834" m="302.714" cg="180."/>
<eng-data t="0.281" f="338.369" m="271.547" cg="180."/>
<eng-data t="0.662" f="344.705" m="192.398" cg="180."/>
<eng-data t="0.855" f="344.705" m="151.931" cg="180."/>
<eng-data t="1.084" f="329.498" m="104.976" cg="180."/>
<eng-data t="1.295" f="319.359" m="63.3383" cg="180."/>
<eng-data t="1.359" f="313.023" m="51.0295" cg="180."/>
<eng-data t="1.447" f="314.29" m="34.2405" cg="180."/>
<eng-data t="1.534" f="269.935" m="18.7824" cg="180."/>
<eng-data t="1.637" f="119.126" m="6.59496" cg="180."/>
<eng-data t="1.681" f="69.701" m="4.06814" cg="180."/>
<eng-data t="1.74" f="40.554" m="2.08977" cg="180."/>
<eng-data t="1.846" f="12.673" m="0.37386" cg="180."/>
<eng-data t="1.943" f="0." m="0." cg="180."/>
</data>
</engine>
</engine-list>
</engine-database>

34
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AMW_I315.eng
View File

@ -1,34 +0,0 @@
; This file my be used or given away. All I ask is that this header
; is maintained to give credit to NAR S&T. Thank you, Jack Kane
; The total impulse, peak thrust, average thrust and burn time are
; the same as the averaged static test data on the NAR web site in
; the certification file. The curve drawn with these data points is as
; close to the certification curve as can be with such a limited
; number of points (32) allowed with wRASP up to v1.6.
;Animal Motor Works 38-640
I315SK 38 369 20 0.3829 0.7166 AMW
0.011 314.573
0.030 312.796
0.066 300.786
0.084 300.502
0.120 304.087
0.175 312.998
0.266 324.086
0.356 332.224
0.447 347.855
0.538 371.972
0.629 382.833
0.719 385.552
0.810 385.586
0.901 384.836
0.992 382.296
1.082 378.323
1.173 370.837
1.264 357.564
1.355 347.122
1.445 328.332
1.536 202.733
1.627 90.867
1.718 35.427
1.808 8.192
1.815 0.000

34
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AMW_I315.rse
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@ -1,34 +0,0 @@
<engine-database>
<engine-list>
<engine FDiv="10" FFix="1" FStep="-1." Isp="148.78" Itot="558.679" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="308.662" burn-time="1.81" cgDiv="10" cgFix="1" cgStep="-1." code="I315SK" delays="20" dia="38." exitDia="0." initWt="716.6" len="369." mDiv="10" mFix="1" mStep="-1." massFrac="53.43" mfg="Animal Motor Works" peakThrust="385.59" propWt="382.9" tDiv="10" tFix="1" tStep="-1." throatDia="0.">
<data>
<eng-data cg="184.5" f="0." m="382.9" t="0."/>
<eng-data cg="184.5" f="314.57" m="381.822" t="0.01"/>
<eng-data cg="184.5" f="312.8" m="377.522" t="0.03"/>
<eng-data cg="184.5" f="300.79" m="369.112" t="0.07"/>
<eng-data cg="184.5" f="304.09" m="358.747" t="0.12"/>
<eng-data cg="184.5" f="300.5" m="367.035" t="0.08"/>
<eng-data cg="184.5" f="313." m="348.113" t="0.17"/>
<eng-data cg="184.5" f="324.09" m="326.281" t="0.27"/>
<eng-data cg="184.5" f="332.22" m="306.04" t="0.36"/>
<eng-data cg="184.5" f="347.86" m="285.065" t="0.45"/>
<eng-data cg="184.5" f="371.97" m="262.865" t="0.54"/>
<eng-data cg="184.5" f="382.83" m="239.585" t="0.63"/>
<eng-data cg="184.5" f="385.55" m="215.887" t="0.72"/>
<eng-data cg="184.5" f="385.59" m="192.104" t="0.81"/>
<eng-data cg="184.5" f="384.84" m="168.343" t="0.9"/>
<eng-data cg="184.5" f="382.3" m="144.683" t="0.99"/>
<eng-data cg="184.5" f="378.32" m="121.225" t="1.08"/>
<eng-data cg="184.5" f="370.84" m="98.1194" t="1.17"/>
<eng-data cg="184.5" f="357.56" m="75.6545" t="1.26"/>
<eng-data cg="184.5" f="347.12" m="51.5062" t="1.36"/>
<eng-data cg="184.5" f="328.33" m="30.6743" t="1.45"/>
<eng-data cg="184.5" f="202.73" m="14.2957" t="1.54"/>
<eng-data cg="184.5" f="90.87" m="5.24059" t="1.63"/>
<eng-data cg="184.5" f="35.43" m="1.34531" t="1.72"/>
<eng-data cg="184.5" f="8.19" m="0." t="1.81"/>
<eng-data cg="184.5" f="0." m="0." t="1.81"/>
</data>
</engine>
</engine-list>
</engine-database>

31
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AMW_I325.eng
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@ -1,31 +0,0 @@
;Animal Motor Works 38-640
I325WT 38 370 17 0.317 0.712 AMW
0.014 68.710
0.022 113.038
0.026 153.671
0.037 244.545
0.045 299.216
0.055 330.246
0.065 350.194
0.079 365.709
0.094 376.79
0.124 381.963
0.185 373.836
0.252 373.836
0.35 381.224
0.47 382.701
0.622 388.611
1.102 384.179
1.366 364.971
1.379 360.537
1.415 331.724
1.49 223.119
1.505 211.298
1.551 187.657
1.592 162.538
1.688 80.529
1.726 50.978
1.775 27.336
1.806 16.993
1.834 9.605
1.901 0.0

44
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AMW_I325.rse
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@ -1,44 +0,0 @@
<engine-database>
<engine-list>
<engine mfg="Animal Motor Works" code="I325WW" Type="reloadable" dia="38." len="370."
initWt="712." propWt="317." delays="18" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="306.99" peakThrust="388.611" throatDia="0." exitDia="0."
Itot="583.589" burn-time="1.9" massFrac="44.52" Isp="187.73" tDiv="10"
tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."
mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<comments>Animal Motor Works 38-640</comments>
<data>
<eng-data t="0." f="0." m="317." cg="185."/>
<eng-data t="0.014" f="68.71" m="316.739" cg="185."/>
<eng-data t="0.022" f="113.038" m="316.344" cg="185."/>
<eng-data t="0.026" f="153.671" m="316.054" cg="185."/>
<eng-data t="0.037" f="244.545" m="314.864" cg="185."/>
<eng-data t="0.045" f="299.216" m="313.683" cg="185."/>
<eng-data t="0.055" f="330.246" m="311.973" cg="185."/>
<eng-data t="0.065" f="350.194" m="310.125" cg="185."/>
<eng-data t="0.079" f="365.709" m="307.403" cg="185."/>
<eng-data t="0.094" f="376.79" m="304.378" cg="185."/>
<eng-data t="0.124" f="381.963" m="298.196" cg="185."/>
<eng-data t="0.185" f="373.836" m="285.675" cg="185."/>
<eng-data t="0.252" f="373.836" m="272.069" cg="185."/>
<eng-data t="0.35" f="381.224" m="251.972" cg="185."/>
<eng-data t="0.47" f="382.701" m="227.075" cg="185."/>
<eng-data t="0.622" f="388.611" m="195.233" cg="185."/>
<eng-data t="1.102" f="384.179" m="94.4879" cg="185."/>
<eng-data t="1.366" f="364.971" m="40.773" cg="185."/>
<eng-data t="1.379" f="360.537" m="38.2114" cg="185."/>
<eng-data t="1.415" f="331.724" m="31.4429" cg="185."/>
<eng-data t="1.49" f="223.119" m="20.1409" cg="185."/>
<eng-data t="1.505" f="211.298" m="18.3711" cg="185."/>
<eng-data t="1.551" f="187.657" m="13.3868" cg="185."/>
<eng-data t="1.592" f="162.538" m="9.48725" cg="185."/>
<eng-data t="1.688" f="80.529" m="3.14973" cg="185."/>
<eng-data t="1.726" f="50.978" m="1.79249" cg="185."/>
<eng-data t="1.775" f="27.336" m="0.750276" cg="185."/>
<eng-data t="1.806" f="16.993" m="0.37705" cg="185."/>
<eng-data t="1.834" f="9.605" m="0.174781" cg="185."/>
<eng-data t="1.901" f="0." m="0." cg="185."/>
</data>
</engine>
</engine-list>
</engine-database>

26
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AMW_I375.eng
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@ -1,26 +0,0 @@
;
;Animal Motor Works 38-640
I375GG 38 369 20 0.3936 0.7338 AMW
0.013 223.878
0.045 273.929
0.092 312.421
0.140 334.383
0.219 357.983
0.298 381.992
0.377 410.267
0.457 431.141
0.536 454.458
0.615 476.825
0.694 495.473
0.773 504.665
0.852 510.942
0.931 511.972
1.011 489.639
1.090 441.350
1.169 392.762
1.248 354.753
1.327 292.385
1.406 177.309
1.486 63.879
1.565 14.901
1.583 0.000

32
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AMW_I375.rse
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@ -1,32 +0,0 @@
<engine-database>
<engine-list>
<engine FDiv="10" FFix="1" FStep="-1." Isp="152.41" Itot="588.308" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="372.347" burn-time="1.58" cgDiv="10" cgFix="1" cgStep="-1." code="I375GG" delays="20" dia="38." exitDia="0." initWt="733.8" len="369." mDiv="10" mFix="1" mStep="-1." massFrac="53.64" mfg="Animal Motor Works" peakThrust="511.97" propWt="393.6" tDiv="10" tFix="1" tStep="-1." throatDia="0.">
<data>
<eng-data cg="184.5" f="0." m="393.6" t="0."/>
<eng-data cg="184.5" f="223.88" m="392.851" t="0.01"/>
<eng-data cg="184.5" f="273.93" m="387.855" t="0.04"/>
<eng-data cg="184.5" f="312.42" m="378.048" t="0.09"/>
<eng-data cg="184.5" f="334.38" m="367.23" t="0.14"/>
<eng-data cg="184.5" f="357.98" m="348.701" t="0.22"/>
<eng-data cg="184.5" f="381.99" m="328.898" t="0.3"/>
<eng-data cg="184.5" f="410.27" m="307.696" t="0.38"/>
<eng-data cg="184.5" f="431.14" m="285.179" t="0.46"/>
<eng-data cg="184.5" f="454.46" m="261.479" t="0.54"/>
<eng-data cg="184.5" f="476.82" m="239.672" t="0.61"/>
<eng-data cg="184.5" f="495.47" m="213.652" t="0.69"/>
<eng-data cg="184.5" f="504.67" m="186.887" t="0.77"/>
<eng-data cg="184.5" f="510.94" m="159.707" t="0.85"/>
<eng-data cg="184.5" f="511.97" m="132.333" t="0.93"/>
<eng-data cg="184.5" f="489.64" m="105.528" t="1.01"/>
<eng-data cg="184.5" f="441.35" m="80.6134" t="1.09"/>
<eng-data cg="184.5" f="392.76" m="58.2913" t="1.17"/>
<eng-data cg="184.5" f="354.75" m="38.2868" t="1.25"/>
<eng-data cg="184.5" f="292.38" m="20.9686" t="1.33"/>
<eng-data cg="184.5" f="177.31" m="8.39903" t="1.41"/>
<eng-data cg="184.5" f="63.88" m="1.94442" t="1.49"/>
<eng-data cg="184.5" f="14.9" m="0.0996866" t="1.56"/>
<eng-data cg="184.5" f="0." m="0." t="1.58"/>
</data>
</engine>
</engine-list>
</engine-database>

49
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AMW_J1365.rse
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@ -1,49 +0,0 @@
<engine-database>
<engine-list>
<engine mfg="Cesaroni Technology Inc." code="J1365ST" Type="reloadable" dia="54."
len="326." initWt="1200." propWt="444." delays="1000" auto-calc-mass="1"
auto-calc-cg="1" avgThrust="1355.49" peakThrust="1576.58" throatDia="0."
exitDia="0." Itot="931.222" burn-time="0.69" massFrac="29.6" Isp="213.87"
tDiv="10" tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10"
mStep="-1." mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<comments>Input by Tim Van Milligan for RockSim users. Used John Coker's ThrustCruve
Tracer program. Thrust curve from the AMW web site and CAR/NAR/TRA certified
rocket motor list dated 9/28/08. The total weight was estimated based on
similar motors such as the J325TT, J395RR, and the J401BB</comments>
<data>
<eng-data t="0." f="0." m="444." cg="163."/>
<eng-data t="0.007" f="1576.58" m="441.369" cg="163."/>
<eng-data t="0.011" f="1083.9" m="438.832" cg="163."/>
<eng-data t="0.014" f="1402.03" m="437.054" cg="163."/>
<eng-data t="0.019" f="1083.9" m="434.091" cg="163."/>
<eng-data t="0.023" f="1402.03" m="431.72" cg="163."/>
<eng-data t="0.027" f="1196.52" m="429.242" cg="163."/>
<eng-data t="0.03" f="1266.9" m="427.481" cg="163."/>
<eng-data t="0.049" f="1311.94" m="415.8" cg="163."/>
<eng-data t="0.078" f="1379.51" m="397.192" cg="163."/>
<eng-data t="0.124" f="1447.08" m="366.195" cg="163."/>
<eng-data t="0.164" f="1483.68" m="338.248" cg="163."/>
<eng-data t="0.219" f="1514.65" m="298.935" cg="163."/>
<eng-data t="0.267" f="1523.09" m="264.174" cg="163."/>
<eng-data t="0.311" f="1531.54" m="232.132" cg="163."/>
<eng-data t="0.361" f="1525.91" m="195.688" cg="163."/>
<eng-data t="0.391" f="1506.2" m="174.003" cg="163."/>
<eng-data t="0.455" f="1447.08" m="128.943" cg="163."/>
<eng-data t="0.489" f="1418.93" m="105.713" cg="163."/>
<eng-data t="0.526" f="1393.59" m="80.9048" cg="163."/>
<eng-data t="0.564" f="1371.07" m="55.8597" cg="163."/>
<eng-data t="0.595" f="1354.17" m="35.7194" cg="163."/>
<eng-data t="0.612" f="1342.91" m="24.7888" cg="163."/>
<eng-data t="0.62" f="1334.47" m="19.6826" cg="163."/>
<eng-data t="0.624" f="1300.68" m="17.1697" cg="163."/>
<eng-data t="0.633" f="1185.25" m="11.836" cg="163."/>
<eng-data t="0.643" f="881.198" m="6.90964" cg="163."/>
<eng-data t="0.649" f="661.602" m="4.70285" cg="163."/>
<eng-data t="0.655" f="458.899" m="3.10011" cg="163."/>
<eng-data t="0.663" f="289.979" m="1.67187" cg="163."/>
<eng-data t="0.676" f="135.136" m="0.354375" cg="163."/>
<eng-data t="0.687" f="0." m="0." cg="163."/>
</data>
</engine>
</engine-list>
</engine-database>

34
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AMW_J230.eng
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@ -1,34 +0,0 @@
; Kosdon J230 RASP.ENG file made from NAR published data
; File produced November 1, 2000
; The total impulse, peak thrust, average thrust and burn time are
; the same as the averaged static test data on the NAR web site in
; the certification file. The curve drawn with these data points is as
; close to the certification curve as can be with such a limited
; number of points (32) allowed with wRASP up to v1.6.
J230 54 326 8 .5008 1.1690 K
0.026 146.964
0.039 214.239
0.076 239.367
0.161 247.777
0.306 247.677
0.488 249.679
0.754 260.090
0.948 268.400
1.227 274.607
1.590 276.720
1.905 270.102
2.195 267.899
2.498 259.390
2.643 252.982
2.824 248.778
3.115 242.270
3.369 229.656
3.478 221.147
3.550 204.328
3.610 170.690
3.658 126.541
3.718 82.442
3.790 61.418
3.899 40.365
3.983 17.229
4.080 0.000

65
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AMW_J230.rse
View File

@ -1,65 +0,0 @@
<engine-database>
<engine-list>
<engine mfg="Animal Motor Works" code="J230SK" Type="reloadable" dia="54." len="326."
initWt="1183.53" propWt="525." delays="1000" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="227.973" peakThrust="277.759" throatDia="0." exitDia="0."
Itot="768.724" burn-time="3.37" massFrac="44.36" Isp="149.31" tDiv="10"
tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."
mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<comments>Input by Tim Van Milligan for RockSim users. Used John Coker's ThrustCruve
Tracer program. Thrust curve from the AMW motor assembly instructions and
CAR/NAR/TRA certified rocket motor list dated 9/28/08. The total weight was
provided by Paul Robinson of AMW.
</comments>
<data>
<eng-data t="0." f="0." m="525." cg="163."/>
<eng-data t="0.033" f="219.31" m="522.529" cg="163."/>
<eng-data t="0.048" f="257.069" m="520.089" cg="163."/>
<eng-data t="0.059" f="271.034" m="518.105" cg="163."/>
<eng-data t="0.084" f="271.034" m="513.477" cg="163."/>
<eng-data t="0.132" f="263.276" m="504.72" cg="163."/>
<eng-data t="0.176" f="253.966" m="496.948" cg="163."/>
<eng-data t="0.216" f="237.414" m="490.236" cg="163."/>
<eng-data t="0.246" f="228.621" m="485.462" cg="163."/>
<eng-data t="0.29" f="225." m="478.647" cg="163."/>
<eng-data t="0.337" f="225." m="471.424" cg="163."/>
<eng-data t="0.421" f="229.138" m="458.398" cg="163."/>
<eng-data t="0.59" f="234.828" m="431.623" cg="163."/>
<eng-data t="0.788" f="243.621" m="399.274" cg="163."/>
<eng-data t="0.96" f="248.276" m="370.383" cg="163."/>
<eng-data t="1.096" f="256.552" m="346.938" cg="163."/>
<eng-data t="1.231" f="255.517" m="323.333" cg="163."/>
<eng-data t="1.374" f="261.724" m="298.075" cg="163."/>
<eng-data t="1.646" f="270." m="248.688" cg="163."/>
<eng-data t="1.799" f="275.172" m="220.205" cg="163."/>
<eng-data t="1.851" f="277.759" m="210.387" cg="163."/>
<eng-data t="1.906" f="273.621" m="200.031" cg="163."/>
<eng-data t="1.957" f="270.517" m="190.555" cg="163."/>
<eng-data t="2.027" f="273.103" m="177.561" cg="163."/>
<eng-data t="2.078" f="272.069" m="168.067" cg="163."/>
<eng-data t="2.144" f="272.069" m="155.803" cg="163."/>
<eng-data t="2.228" f="271.552" m="140.21" cg="163."/>
<eng-data t="2.28" f="271.552" m="130.566" cg="163."/>
<eng-data t="2.316" f="267.414" m="123.941" cg="163."/>
<eng-data t="2.379" f="263.793" m="112.513" cg="163."/>
<eng-data t="2.43" f="259.655" m="103.397" cg="163."/>
<eng-data t="2.551" f="240.517" m="82.7305" cg="163."/>
<eng-data t="2.752" f="211.034" m="51.7377" cg="163."/>
<eng-data t="2.837" f="200.69" m="39.7872" cg="163."/>
<eng-data t="2.888" f="196.034" m="32.8782" cg="163."/>
<eng-data t="2.914" f="199.138" m="29.3697" cg="163."/>
<eng-data t="2.939" f="206.379" m="25.9079" cg="163."/>
<eng-data t="2.961" f="215.172" m="22.741" cg="163."/>
<eng-data t="2.983" f="219.828" m="19.4731" cg="163."/>
<eng-data t="3.016" f="206.379" m="14.6703" cg="163."/>
<eng-data t="3.057" f="158.276" m="9.56496" cg="163."/>
<eng-data t="3.093" f="113.793" m="6.22039" cg="163."/>
<eng-data t="3.145" f="69.31" m="2.96909" cg="163."/>
<eng-data t="3.185" f="40.345" m="1.47131" cg="163."/>
<eng-data t="3.236" f="14.483" m="0.516472" cg="163."/>
<eng-data t="3.287" f="5.69" m="0.165154" cg="163."/>
<eng-data t="3.372" f="0." m="0." cg="163."/>
</data>
</engine>
</engine-list>
</engine-database>

44
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AMW_J325.rse
View File

@ -1,44 +0,0 @@
<engine-database>
<engine-list>
<engine mfg="Cesaroni Technology Inc." code="J325TT" Type="reloadable" dia="54."
len="326." initWt="1230." propWt="537." delays="1000" auto-calc-mass="1"
auto-calc-cg="1" avgThrust="323.289" peakThrust="540.652" throatDia="0."
exitDia="0." Itot="1089.16" burn-time="3.37" massFrac="43.66" Isp="206.82"
tDiv="10" tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10"
mStep="-1." mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<comments>Entered by Tim Van Milligan for RockSim users. Used ThrustCurve Tracer by John
Coker. Data from CAR web site, thrust curve from AMW web site.
</comments>
<data>
<eng-data t="0." f="0." m="537." cg="163."/>
<eng-data t="0.013" f="334.689" m="535.927" cg="163."/>
<eng-data t="0.034" f="534.215" m="531.429" cg="163."/>
<eng-data t="0.046" f="523.488" m="528.3" cg="163."/>
<eng-data t="0.072" f="540.652" m="521.48" cg="163."/>
<eng-data t="0.084" f="474.143" m="518.478" cg="163."/>
<eng-data t="0.156" f="474.143" m="501.646" cg="163."/>
<eng-data t="0.215" f="474.143" m="487.853" cg="163."/>
<eng-data t="0.342" f="463.416" m="458.5" cg="163."/>
<eng-data t="0.519" f="454.834" m="418.433" cg="163."/>
<eng-data t="1.004" f="414.071" m="314.545" cg="163."/>
<eng-data t="1.286" f="392.616" m="258.465" cg="163."/>
<eng-data t="1.78" f="328.253" m="170.677" cg="163."/>
<eng-data t="2.222" f="274.617" m="104.987" cg="163."/>
<eng-data t="2.458" f="251.017" m="74.4061" cg="163."/>
<eng-data t="2.555" f="240.29" m="62.6577" cg="163."/>
<eng-data t="2.606" f="233.853" m="56.6966" cg="163."/>
<eng-data t="2.766" f="216.69" m="38.9257" cg="163."/>
<eng-data t="2.863" f="205.963" m="28.819" cg="163."/>
<eng-data t="2.922" f="199.526" m="22.9213" cg="163."/>
<eng-data t="2.964" f="188.799" m="18.9006" cg="163."/>
<eng-data t="3.011" f="173.781" m="14.6996" cg="163."/>
<eng-data t="3.057" f="150.181" m="11.0259" cg="163."/>
<eng-data t="3.104" f="124.436" m="7.84404" cg="163."/>
<eng-data t="3.15" f="98.69" m="5.3138" cg="163."/>
<eng-data t="3.243" f="57.927" m="1.72314" cg="163."/>
<eng-data t="3.289" f="34.327" m="0.676984" cg="163."/>
<eng-data t="3.369" f="0." m="0." cg="163."/>
</data>
</engine>
</engine-list>
</engine-database>

35
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AMW_J357.eng
View File

@ -1,35 +0,0 @@
; AMW Animal Motor Works fixed by dberez 12/08/03
;
;Animal Motor Works J357 White Wolf
J357WW 54 326 0 0.5481 1.2101 AMW
0.02 129.64
0.03 205.95
0.05 265.00
0.06 316.51
0.09 326.05
0.13 314.60
0.18 301.25
0.24 299.34
0.35 312.69
0.50 326.05
0.66 333.68
0.87 345.13
1.07 358.48
1.46 383.18
1.77 398.45
1.86 400.36
1.98 402.35
2.18 398.45
2.29 390.82
2.41 369.93
2.51 354.67
2.55 352.76
2.60 347.03
2.65 335.59
2.69 310.79
2.75 249.73
2.81 175.43
2.84 108.65
2.90 53.38
2.92 20.98
2.95 0.00

40
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AMW_J357.rse
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@ -1,40 +0,0 @@
<engine-database>
<engine-list>
<engine FDiv="10" FFix="1" FStep="-1." Isp="185.87" Itot="999.076" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="338.67" burn-time="2.95" cgDiv="10" cgFix="1" cgStep="-1." code="J357WW" delays="1000" dia="54." exitDia="0." initWt="1210.1" len="326." mDiv="10" mFix="1" mStep="-1." massFrac="45.29" mfg="Animal Motor Works" peakThrust="402.35" propWt="548.1" tDiv="10" tFix="1" tStep="-1." throatDia="0.">
<data>
<eng-data cg="163." f="0." m="548.1" t="0."/>
<eng-data cg="163." f="129.64" m="547.389" t="0.02"/>
<eng-data cg="163." f="205.95" m="546.468" t="0.03"/>
<eng-data cg="163." f="265." m="543.885" t="0.05"/>
<eng-data cg="163." f="316.51" m="542.289" t="0.06"/>
<eng-data cg="163." f="326.05" m="537.002" t="0.09"/>
<eng-data cg="163." f="314.6" m="529.972" t="0.13"/>
<eng-data cg="163." f="301.25" m="521.526" t="0.18"/>
<eng-data cg="163." f="299.34" m="511.641" t="0.24"/>
<eng-data cg="163." f="312.69" m="493.174" t="0.35"/>
<eng-data cg="163." f="326.05" m="466.893" t="0.5"/>
<eng-data cg="163." f="333.68" m="437.938" t="0.66"/>
<eng-data cg="163." f="345.13" m="398.836" t="0.87"/>
<eng-data cg="163." f="358.48" m="360.236" t="1.07"/>
<eng-data cg="163." f="383.18" m="280.894" t="1.46"/>
<eng-data cg="163." f="398.45" m="214.429" t="1.77"/>
<eng-data cg="163." f="400.36" m="194.709" t="1.86"/>
<eng-data cg="163." f="402.35" m="168.286" t="1.98"/>
<eng-data cg="163." f="398.45" m="124.354" t="2.18"/>
<eng-data cg="163." f="390.82" m="100.539" t="2.29"/>
<eng-data cg="163." f="369.93" m="75.4978" t="2.41"/>
<eng-data cg="163." f="354.67" m="55.6218" t="2.51"/>
<eng-data cg="163." f="352.76" m="47.8597" t="2.55"/>
<eng-data cg="163." f="347.03" m="38.262" t="2.6"/>
<eng-data cg="163." f="335.59" m="28.8997" t="2.65"/>
<eng-data cg="163." f="310.79" m="21.8076" t="2.69"/>
<eng-data cg="163." f="249.73" m="12.5824" t="2.75"/>
<eng-data cg="163." f="175.43" m="5.58504" t="2.81"/>
<eng-data cg="163." f="108.65" m="3.24731" t="2.84"/>
<eng-data cg="163." f="53.38" m="0.580591" t="2.9"/>
<eng-data cg="163." f="20.98" m="0.172647" t="2.92"/>
<eng-data cg="163." f="0." m="0." t="2.95"/>
</data>
</engine>
</engine-list>
</engine-database>

25
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AMW_J365.eng
View File

@ -1,25 +0,0 @@
;
;Animal Motor Works 54-1400
J365SK 54 403 0 0.7571 1.4593 AMW
0.029 389.731
0.123 360.219
0.218 334.200
0.376 326.150
0.534 334.217
0.692 341.669
0.850 347.676
1.007 359.408
1.165 370.043
1.323 383.343
1.481 399.248
1.639 417.477
1.797 443.735
1.955 472.683
2.112 501.668
2.270 497.077
2.428 425.371
2.586 349.017
2.744 262.068
2.902 107.073
3.060 41.821
3.157 0.000

31
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AMW_J365.rse
View File

@ -1,31 +0,0 @@
<engine-database>
<engine-list>
<engine FDiv="10" FFix="1" FStep="-1." Isp="148.91" Itot="1105.56" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="349.861" burn-time="3.16" cgDiv="10" cgFix="1" cgStep="-1." code="J365SK" delays="1000" dia="54." exitDia="0." initWt="1459.3" len="403." mDiv="10" mFix="1" mStep="-1." massFrac="51.88" mfg="Animal Motor Works" peakThrust="501.67" propWt="757.1" tDiv="10" tFix="1" tStep="-1." throatDia="0.">
<data>
<eng-data cg="201.5" f="0." m="757.1" t="0."/>
<eng-data cg="201.5" f="389.73" m="753.097" t="0.03"/>
<eng-data cg="201.5" f="360.22" m="729.986" t="0.12"/>
<eng-data cg="201.5" f="334.2" m="706.209" t="0.22"/>
<eng-data cg="201.5" f="326.15" m="670.031" t="0.38"/>
<eng-data cg="201.5" f="334.22" m="636.114" t="0.53"/>
<eng-data cg="201.5" f="341.67" m="599.086" t="0.69"/>
<eng-data cg="201.5" f="347.68" m="561.32" t="0.85"/>
<eng-data cg="201.5" f="359.41" m="522.582" t="1.01"/>
<eng-data cg="201.5" f="370.04" m="482.619" t="1.17"/>
<eng-data cg="201.5" f="383.34" m="443.925" t="1.32"/>
<eng-data cg="201.5" f="399.25" m="401.051" t="1.48"/>
<eng-data cg="201.5" f="417.48" m="356.307" t="1.64"/>
<eng-data cg="201.5" f="443.74" m="309.125" t="1.8"/>
<eng-data cg="201.5" f="472.68" m="258.919" t="1.96"/>
<eng-data cg="201.5" f="501.67" m="208.876" t="2.11"/>
<eng-data cg="201.5" f="497.08" m="154.159" t="2.27"/>
<eng-data cg="201.5" f="425.37" m="103.623" t="2.43"/>
<eng-data cg="201.5" f="349.02" m="61.1982" t="2.59"/>
<eng-data cg="201.5" f="262.07" m="29.8121" t="2.74"/>
<eng-data cg="201.5" f="107.07" m="9.58885" t="2.9"/>
<eng-data cg="201.5" f="41.82" m="1.43194" t="3.06"/>
<eng-data cg="201.5" f="0." m="0." t="3.16"/>
</data>
</engine>
</engine-list>
</engine-database>

44
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AMW_J370.eng
View File

@ -1,44 +0,0 @@
;
;Animal Motor Works 54-1050
;AMW J370GG RASP.ENG file made from NAR data
;File produced FEB 20, 2003
;This file my be used or given away. All I ask is that this header
;is maintained to give credit to NAR S&T. Thank you, Jack Kane
;The total impulse, peak thrust, average thrust and burn time are
;the same as the averaged static test data on the NAR web site in
;the certification file. The curve drawn with these data points is as
;close to the certification curve as can be with such a limited
;number of points (32) allowed with wRASP up to v1.6.
J370GG 54 326 100 0.5983 1.2491 Animal_Motor_Works
0.008 185.496
0.024 149.516
0.063 225.273
0.087 272.647
0.122 304.829
0.158 304.829
0.273 335.212
0.431 363.796
0.573 390.381
0.707 413.168
0.877 428.459
1.019 441.852
1.126 441.852
1.224 458.46
1.284 443.951
1.386 440.153
1.572 438.454
1.651 438.554
1.813 417.765
2.022 404.673
2.141 385.883
2.212 385.883
2.255 374.59
2.299 387.882
2.362 357.599
2.401 384.184
2.421 348.204
2.457 316.122
2.559 251.758
2.697 115.635
2.753 45.624
2.82 0

52
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AMW_J370.rse
View File

@ -1,52 +0,0 @@
<engine-database>
<engine-list>
<engine FDiv="10" FFix="1" FStep="-1." Isp="175.7" Itot="1030.88" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="365.561" burn-time="2.82" cgDiv="10" cgFix="1" cgStep="-1." code="J370GG" delays="1000" dia="54." exitDia="0." initWt="1249.1" len="326." mDiv="10" mFix="1" mStep="-1." massFrac="47.9" mfg="Animal Motor Works" peakThrust="458.46" propWt="598.3" tDiv="10" tFix="1" tStep="-1." throatDia="0.">
<comments><![CDATA[Animal Motor Works 54-1050
AMW J370GG RASP.ENG file made from NAR data
File produced FEB 20, 2003
This file my be used or given away. All I ask is that this header
is maintained to give credit to NAR S&T. Thank you, Jack Kane
The total impulse, peak thrust, average thrust and burn time are
the same as the averaged static test data on the NAR web site in
the certification file. The curve drawn with these data points is as
close to the certification curve as can be with such a limited
number of points (32) allowed with wRASP up to v1.6.
]]></comments>
<data>
<eng-data cg="163." f="0." m="598.3" t="0."/>
<eng-data cg="163." f="185.496" m="597.869" t="0.008"/>
<eng-data cg="163." f="149.516" m="596.314" t="0.024"/>
<eng-data cg="163." f="225.273" m="592.072" t="0.063"/>
<eng-data cg="163." f="272.647" m="588.605" t="0.087"/>
<eng-data cg="163." f="304.829" m="582.739" t="0.122"/>
<eng-data cg="163." f="304.829" m="576.37" t="0.158"/>
<eng-data cg="163." f="335.212" m="555.011" t="0.273"/>
<eng-data cg="163." f="363.796" m="522.962" t="0.431"/>
<eng-data cg="163." f="390.381" m="491.885" t="0.573"/>
<eng-data cg="163." f="413.168" m="460.639" t="0.707"/>
<eng-data cg="163." f="428.459" m="419.119" t="0.877"/>
<eng-data cg="163." f="441.852" m="383.257" t="1.019"/>
<eng-data cg="163." f="441.852" m="355.818" t="1.126"/>
<eng-data cg="163." f="458.46" m="330.214" t="1.224"/>
<eng-data cg="163." f="443.951" m="314.502" t="1.284"/>
<eng-data cg="163." f="440.153" m="288.333" t="1.386"/>
<eng-data cg="163." f="438.454" m="240.91" t="1.572"/>
<eng-data cg="163." f="438.554" m="220.805" t="1.651"/>
<eng-data cg="163." f="417.765" m="180.549" t="1.813"/>
<eng-data cg="163." f="404.673" m="130.669" t="2.022"/>
<eng-data cg="163." f="385.883" m="103.369" t="2.141"/>
<eng-data cg="163." f="385.883" m="87.4681" t="2.212"/>
<eng-data cg="163." f="374.59" m="77.9789" t="2.255"/>
<eng-data cg="163." f="387.882" m="68.2434" t="2.299"/>
<eng-data cg="163." f="357.599" m="54.6147" t="2.362"/>
<eng-data cg="163." f="384.184" m="46.2197" t="2.401"/>
<eng-data cg="163." f="348.204" m="41.969" t="2.421"/>
<eng-data cg="163." f="316.122" m="35.029" t="2.457"/>
<eng-data cg="163." f="251.758" m="18.2202" t="2.559"/>
<eng-data cg="163." f="115.635" m="3.50759" t="2.697"/>
<eng-data cg="163." f="45.624" m="0.887049" t="2.753"/>
<eng-data cg="163." f="0." m="0." t="2.82"/>
</data>
</engine>
</engine-list>
</engine-database>

67
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AMW_J395.rse
View File

@ -1,67 +0,0 @@
<engine-database>
<engine-list>
<engine mfg="Cesaroni Technology Inc." code="J395RR" Type="reloadable" dia="54."
len="326." initWt="1268." propWt="573." delays="1000" auto-calc-mass="1"
auto-calc-cg="1" avgThrust="391.129" peakThrust="467.063" throatDia="0."
exitDia="0." Itot="1079.52" burn-time="2.76" massFrac="45.19" Isp="192.11"
tDiv="10" tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10"
mStep="-1." mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<comments>Entered by Tim Van Milligan for RockSim users. Used ThrustCurve Tracer by John
Coker. Data from CAR web site, thrust curve from AMW web site.
</comments>
<data>
<eng-data t="0." f="0." m="573." cg="163."/>
<eng-data t="0.032" f="336.088" m="570.146" cg="163."/>
<eng-data t="0.036" f="390.455" m="569.374" cg="163."/>
<eng-data t="0.068" f="417.638" m="562.512" cg="163."/>
<eng-data t="0.079" f="420.11" m="560.066" cg="163."/>
<eng-data t="0.093" f="417.638" m="556.953" cg="163."/>
<eng-data t="0.108" f="412.696" m="553.648" cg="163."/>
<eng-data t="0.172" f="432.466" m="539.292" cg="163."/>
<eng-data t="0.219" f="447.293" m="528.318" cg="163."/>
<eng-data t="0.265" f="454.707" m="517.307" cg="163."/>
<eng-data t="0.308" f="459.649" m="506.872" cg="163."/>
<eng-data t="0.391" f="462.121" m="486.567" cg="163."/>
<eng-data t="0.441" f="467.063" m="474.237" cg="163."/>
<eng-data t="0.484" f="459.649" m="463.661" cg="163."/>
<eng-data t="0.527" f="462.121" m="453.142" cg="163."/>
<eng-data t="0.606" f="459.649" m="433.816" cg="163."/>
<eng-data t="0.753" f="454.707" m="398.144" cg="163."/>
<eng-data t="1.025" f="437.408" m="333.744" cg="163."/>
<eng-data t="1.215" f="422.581" m="290.378" cg="163."/>
<eng-data t="1.247" f="432.466" m="283.117" cg="163."/>
<eng-data t="1.298" f="432.466" m="271.41" cg="163."/>
<eng-data t="1.376" f="425.052" m="253.658" cg="163."/>
<eng-data t="1.566" f="417.638" m="211.165" cg="163."/>
<eng-data t="1.706" f="417.638" m="180.13" cg="163."/>
<eng-data t="1.753" f="417.638" m="169.711" cg="163."/>
<eng-data t="1.771" f="412.696" m="165.744" cg="163."/>
<eng-data t="1.814" f="412.696" m="156.325" cg="163."/>
<eng-data t="1.882" f="397.869" m="141.697" cg="163."/>
<eng-data t="1.9" f="402.811" m="137.872" cg="163."/>
<eng-data t="1.928" f="397.869" m="131.922" cg="163."/>
<eng-data t="1.961" f="397.869" m="124.953" cg="163."/>
<eng-data t="1.989" f="392.926" m="119.076" cg="163."/>
<eng-data t="2.04" f="392.926" m="108.44" cg="163."/>
<eng-data t="2.075" f="390.455" m="101.163" cg="163."/>
<eng-data t="2.129" f="397.869" m="89.865" cg="163."/>
<eng-data t="2.151" f="385.512" m="85.291" cg="163."/>
<eng-data t="2.179" f="375.627" m="79.6349" cg="163."/>
<eng-data t="2.215" f="365.743" m="72.5517" cg="163."/>
<eng-data t="2.244" f="378.099" m="66.8267" cg="163."/>
<eng-data t="2.262" f="373.156" m="63.2378" cg="163."/>
<eng-data t="2.29" f="368.214" m="57.7286" cg="163."/>
<eng-data t="2.319" f="363.271" m="52.0987" cg="163."/>
<eng-data t="2.366" f="353.386" m="43.1594" cg="163."/>
<eng-data t="2.394" f="358.329" m="37.8705" cg="163."/>
<eng-data t="2.416" f="350.915" m="33.7295" cg="163."/>
<eng-data t="2.43" f="343.501" m="31.1493" cg="163."/>
<eng-data t="2.452" f="326.203" m="27.2391" cg="163."/>
<eng-data t="2.484" f="313.847" m="21.8033" cg="163."/>
<eng-data t="2.556" f="227.353" m="11.4618" cg="163."/>
<eng-data t="2.624" f="135.918" m="4.90582" cg="163."/>
<eng-data t="2.76" f="0." m="0." cg="163."/>
</data>
</engine>
</engine-list>
</engine-database>

34
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AMW_J400.eng
View File

@ -1,34 +0,0 @@
;
;AMW J400 RASP.ENG file made from NAR published data
;File produced April 19, 2004
;The total impulse, peak thrust, average thrust and burn time are
;the same as the averaged static test data on the NAR web site in
;the certification file. The curve drawn with these data points is as
;close to the certification curve as can be with such a limited
;number of points (32) allowed with wRASP up to v1.6.
J400RR 54 326 100 0.558 1.2314 Animal_Motor_Works
0.043 246.55
0.06 317.381
0.081 344.709
0.107 358.372
0.15 356.06
0.201 365.204
0.308 392.532
0.568 435.734
0.863 458.339
1.094 469.24
1.209 467.18
1.466 460.148
1.705 443.972
1.923 423.275
2.132 409.411
2.303 413.831
2.402 420.563
2.47 413.831
2.517 395.445
2.543 347.421
2.568 265.238
2.598 128.198
2.615 68.801
2.632 25.398
2.66 0

61
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AMW_J400.rse
View File

@ -1,61 +0,0 @@
<engine-database>
<engine-list>
<engine mfg="Cesaroni Technology Inc." code="J401BB" Type="reloadable" dia="54."
len="326." initWt="1382." propWt="723." delays="1000" auto-calc-mass="1"
auto-calc-cg="1" avgThrust="396.058" peakThrust="480.548" throatDia="0."
exitDia="0." Itot="973.51" burn-time="2.46" massFrac="52.32" Isp="137.3"
tDiv="10" tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10"
mStep="-1." mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<comments>Entered by Tim Van Milligan for RockSim users. Used ThrustCurve Tracer by John
Coker. Data from CAR web site, thrust curve from AMW web site.
</comments>
<data>
<eng-data t="0." f="0." m="723." cg="163."/>
<eng-data t="0.018" f="298.416" m="721.005" cg="163."/>
<eng-data t="0.025" f="343.248" m="719.337" cg="163."/>
<eng-data t="0.033" f="381.076" m="717.186" cg="163."/>
<eng-data t="0.048" f="364.264" m="713.034" cg="163."/>
<eng-data t="0.058" f="397.888" m="710.204" cg="163."/>
<eng-data t="0.071" f="364.264" m="706.525" cg="163."/>
<eng-data t="0.084" f="386.68" m="702.9" cg="163."/>
<eng-data t="0.099" f="365.665" m="698.709" cg="163."/>
<eng-data t="0.106" f="390.883" m="696.743" cg="163."/>
<eng-data t="0.119" f="334.842" m="693.239" cg="163."/>
<eng-data t="0.137" f="353.056" m="688.641" cg="163."/>
<eng-data t="0.218" f="368.467" m="666.939" cg="163."/>
<eng-data t="0.316" f="385.279" m="639.51" cg="163."/>
<eng-data t="0.428" f="402.091" m="606.763" cg="163."/>
<eng-data t="0.562" f="417.502" m="565.981" cg="163."/>
<eng-data t="0.709" f="431.512" m="519.636" cg="163."/>
<eng-data t="0.77" f="437.116" m="499.96" cg="163."/>
<eng-data t="0.886" f="451.127" m="461.699" cg="163."/>
<eng-data t="0.975" f="455.33" m="431.742" cg="163."/>
<eng-data t="1.033" f="456.731" m="412.098" cg="163."/>
<eng-data t="1.122" f="462.335" m="381.724" cg="163."/>
<eng-data t="1.21" f="469.34" m="351.279" cg="163."/>
<eng-data t="1.284" f="470.741" m="325.447" cg="163."/>
<eng-data t="1.365" f="480.548" m="296.834" cg="163."/>
<eng-data t="1.428" f="473.543" m="274.513" cg="163."/>
<eng-data t="1.504" f="469.34" m="247.904" cg="163."/>
<eng-data t="1.577" f="466.538" m="222.534" cg="163."/>
<eng-data t="1.658" f="455.33" m="194.806" cg="163."/>
<eng-data t="1.798" f="435.715" m="148.483" cg="163."/>
<eng-data t="1.909" f="404.893" m="113.835" cg="163."/>
<eng-data t="1.998" f="381.076" m="87.8594" cg="163."/>
<eng-data t="2.069" f="361.462" m="68.2825" cg="163."/>
<eng-data t="2.109" f="351.655" m="57.6903" cg="163."/>
<eng-data t="2.124" f="336.243" m="53.8586" cg="163."/>
<eng-data t="2.15" f="341.847" m="47.3118" cg="163."/>
<eng-data t="2.182" f="348.853" m="39.1044" cg="163."/>
<eng-data t="2.188" f="355.858" m="37.5343" cg="163."/>
<eng-data t="2.205" f="340.446" m="33.1387" cg="163."/>
<eng-data t="2.233" f="320.832" m="26.2631" cg="163."/>
<eng-data t="2.286" f="243.776" m="15.1512" cg="163."/>
<eng-data t="2.319" f="197.543" m="9.7432" cg="163."/>
<eng-data t="2.355" f="138.7" m="5.24827" cg="163."/>
<eng-data t="2.408" f="65.848" m="1.22259" cg="163."/>
<eng-data t="2.458" f="0." m="0." cg="163."/>
</data>
</engine>
</engine-list>
</engine-database>

42
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AMW_J400_1.rse
View File

@ -1,42 +0,0 @@
<engine-database>
<engine-list>
<engine FDiv="10" FFix="1" FStep="-1." Isp="200.08" Itot="1094.88" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="411.61" burn-time="2.66" cgDiv="10" cgFix="1" cgStep="-1." code="J400RR" delays="1000" dia="54." exitDia="0." initWt="1231.4" len="326." mDiv="10" mFix="1" mStep="-1." massFrac="45.31" mfg="Animal Motor Works" peakThrust="469.24" propWt="558." tDiv="10" tFix="1" tStep="-1." throatDia="0.">
<comments>AMW J400 RASP.ENG file made from NAR published data
File produced April 19, 2004
The total impulse, peak thrust, average thrust and burn time are
the same as the averaged static test data on the NAR web site in
the certification file. The curve drawn with these data points is as
close to the certification curve as can be with such a limited
number of points (32) allowed with wRASP up to v1.6.
</comments>
<data>
<eng-data cg="163." f="0." m="558." t="0."/>
<eng-data cg="163." f="246.55" m="555.298" t="0.043"/>
<eng-data cg="163." f="317.381" m="552.856" t="0.06"/>
<eng-data cg="163." f="344.709" m="549.313" t="0.081"/>
<eng-data cg="163." f="358.372" m="544.654" t="0.107"/>
<eng-data cg="163." f="356.06" m="536.826" t="0.15"/>
<eng-data cg="163." f="365.204" m="527.453" t="0.201"/>
<eng-data cg="163." f="392.532" m="506.792" t="0.308"/>
<eng-data cg="163." f="435.734" m="451.916" t="0.568"/>
<eng-data cg="163." f="458.339" m="384.707" t="0.863"/>
<eng-data cg="163." f="469.24" m="330.106" t="1.094"/>
<eng-data cg="163." f="467.18" m="302.665" t="1.209"/>
<eng-data cg="163." f="460.148" m="241.935" t="1.466"/>
<eng-data cg="163." f="443.972" m="186.871" t="1.705"/>
<eng-data cg="163." f="423.275" m="138.695" t="1.923"/>
<eng-data cg="163." f="409.411" m="94.3478" t="2.132"/>
<eng-data cg="163." f="413.831" m="58.4754" t="2.303"/>
<eng-data cg="163." f="420.563" m="37.4258" t="2.402"/>
<eng-data cg="163." f="413.831" m="22.9675" t="2.47"/>
<eng-data cg="163." f="395.445" m="13.2751" t="2.517"/>
<eng-data cg="163." f="347.421" m="8.35334" t="2.543"/>
<eng-data cg="163." f="265.238" m="4.45036" t="2.568"/>
<eng-data cg="163." f="128.198" m="1.44268" t="2.598"/>
<eng-data cg="163." f="68.801" m="0.589283" t="2.615"/>
<eng-data cg="163." f="25.398" m="0.181215" t="2.632"/>
<eng-data cg="163." f="0." m="0." t="2.66"/>
</data>
</engine>
</engine-list>
</engine-database>

16
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AMW_J440.eng
View File

@ -1,16 +0,0 @@
J440-BB 54 326 0 0.536 1.229 AMW/ProX
0.01 30
0.02 700
0.06 790
0.1 800
0.2 760
0.4 725
0.6 695
0.8 680
1 658
1.32 600
1.55 400
1.7 180
1.87 175
2 75
2.1 0

29
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AMW_J440.rse
View File

@ -1,29 +0,0 @@
<engine-database>
<engine-list>
<engine mfg="AMW-ProX" code="J440-BB" Type="unspecified" dia="54." len="326."
initWt="1229." propWt="536." delays="0" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="531.026" peakThrust="800." throatDia="0." exitDia="0." Itot="1115.15"
burn-time="2.1" massFrac="43.61" Isp="212.15" tDiv="10" tStep="-1." tFix="1"
FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10"
cgStep="-1." cgFix="1">
<data>
<eng-data t="0." f="0." m="536." cg="163."/>
<eng-data t="0.01" f="30." m="535.928" cg="163."/>
<eng-data t="0.02" f="700." m="534.174" cg="163."/>
<eng-data t="0.06" f="790." m="519.85" cg="163."/>
<eng-data t="0.1" f="800." m="504.565" cg="163."/>
<eng-data t="0.2" f="760." m="467.075" cg="163."/>
<eng-data t="0.4" f="725." m="395.698" cg="163."/>
<eng-data t="0.6" f="695." m="327.446" cg="163."/>
<eng-data t="0.8" f="680." m="261.356" cg="163."/>
<eng-data t="1." f="658." m="197.045" cg="163."/>
<eng-data t="1.32" f="600." m="100.3" cg="163."/>
<eng-data t="1.55" f="400." m="45.025" cg="163."/>
<eng-data t="1.7" f="180." m="24.1166" cg="163."/>
<eng-data t="1.87" f="175." m="9.61301" cg="163."/>
<eng-data t="2." f="75." m="1.80244" cg="163."/>
<eng-data t="2.1" f="0." m="0." cg="163."/>
</data>
</engine>
</engine-list>
</engine-database>

27
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AMW_J440_1.eng
View File

@ -1,27 +0,0 @@
;Animal Motor Works 38-640
J440BB 38 369 20 0.3853 0.6985 AMW
0.007 468.505
0.022 509.996
0.037 527.687
0.052 532.792
0.082 530.181
0.127 525.586
0.202 521.566
0.277 519.840
0.352 521.522
0.426 525.414
0.501 531.248
0.576 538.724
0.651 541.761
0.726 538.508
0.801 531.072
0.876 516.175
0.950 494.942
1.025 477.251
1.100 433.297
1.175 313.900
1.250 187.467
1.325 101.546
1.400 45.751
1.474 22.083
1.497 0.000

34
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AMW_J440_1.rse
View File

@ -1,34 +0,0 @@
<engine-database>
<engine-list>
<engine FDiv="10" FFix="1" FStep="-1." Isp="167.98" Itot="634.714" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="423.143" burn-time="1.5" cgDiv="10" cgFix="1" cgStep="-1." code="J440BB" delays="20" dia="38." exitDia="0." initWt="698.5" len="369." mDiv="10" mFix="1" mStep="-1." massFrac="55.16" mfg="Animal Motor Works" peakThrust="541.76" propWt="385.3" tDiv="10" tFix="1" tStep="-1." throatDia="0.">
<data>
<eng-data cg="184.5" f="0." m="385.3" t="0."/>
<eng-data cg="184.5" f="468.51" m="383.878" t="0.01"/>
<eng-data cg="184.5" f="510." m="380.908" t="0.02"/>
<eng-data cg="184.5" f="527.69" m="374.609" t="0.04"/>
<eng-data cg="184.5" f="532.79" m="371.39" t="0.05"/>
<eng-data cg="184.5" f="530.18" m="361.711" t="0.08"/>
<eng-data cg="184.5" f="525.59" m="345.688" t="0.13"/>
<eng-data cg="184.5" f="521.57" m="323.44" t="0.2"/>
<eng-data cg="184.5" f="519.84" m="298.153" t="0.28"/>
<eng-data cg="184.5" f="521.52" m="276.027" t="0.35"/>
<eng-data cg="184.5" f="525.41" m="250.606" t="0.43"/>
<eng-data cg="184.5" f="531.25" m="228.155" t="0.5"/>
<eng-data cg="184.5" f="538.72" m="202.175" t="0.58"/>
<eng-data cg="184.5" f="541.76" m="179.218" t="0.65"/>
<eng-data cg="184.5" f="538.51" m="152.987" t="0.73"/>
<eng-data cg="184.5" f="531.07" m="130.262" t="0.8"/>
<eng-data cg="184.5" f="516.17" m="104.834" t="0.88"/>
<eng-data cg="184.5" f="494.94" m="83.351" t="0.95"/>
<eng-data cg="184.5" f="477.25" m="62.6953" t="1.02"/>
<eng-data cg="184.5" f="433.3" m="40.5855" t="1.1"/>
<eng-data cg="184.5" f="313.9" m="22.4421" t="1.18"/>
<eng-data cg="184.5" f="187.47" m="11.7897" t="1.25"/>
<eng-data cg="184.5" f="101.55" m="4.77183" t="1.33"/>
<eng-data cg="184.5" f="45.75" m="1.64221" t="1.4"/>
<eng-data cg="184.5" f="22.08" m="0.201053" t="1.47"/>
<eng-data cg="184.5" f="0." m="0." t="1.5"/>
</data>
</engine>
</engine-list>
</engine-database>

39
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AMW_J450.eng
View File

@ -1,39 +0,0 @@
;
;AMW J450 RASP.ENG file made from NAR published data
; File produced SEPT 4, 2002
; The total impulse, peak thrust, average thrust and burn time are
; the same as the averaged static test data on the NAR web site in
; the certification file. The curve drawn with these data points is as
; close to the certification curve as can be with such a limited
; number of points (32) allowed with wRASP up to v1.6.
J450 54 326 P .5331 1.1964 AMW
0.009 251.586
0.016 376.074
0.030 413.450
0.051 430.832
0.094 423.296
0.162 413.149
0.262 395.566
0.402 420.182
0.495 444.898
0.805 504.078
1.048 536.028
1.223 550.597
1.299 563.180
1.334 555.319
1.470 560.042
1.588 559.841
1.764 546.980
1.921 516.838
1.993 496.743
2.025 499.154
2.047 479.160
2.086 414.354
2.115 344.525
2.141 252.290
2.177 140.161
2.213 82.780
2.239 50.347
2.271 27.861
2.296 12.860
2.330 0.000

50
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AMW_J450.rse
View File

@ -1,50 +0,0 @@
<engine-database>
<engine-list>
<engine FDiv="10" FFix="1" FStep="-1." Isp="204.62" Itot="1069.71" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="459.105" burn-time="2.33" cgDiv="10" cgFix="1" cgStep="-1." code="J450ST" delays="1000" dia="54." exitDia="0." initWt="1196.4" len="326." mDiv="10" mFix="1" mStep="-1." massFrac="44.56" mfg="Animal Motor Works" peakThrust="563.18" propWt="533.1" tDiv="10" tFix="1" tStep="-1." throatDia="0.">
<comments><![CDATA[Animal Motor Works 54-1050
AMW J450ST RASP.ENG file made from NAR published data
File produced SEPT 4, 2002
This file my be used or given away. All I ask is that this header
is maintained to give credit to NAR S&T. Thank you, Jack Kane
The total impulse, peak thrust, average thrust and burn time are
the same as the averaged static test data on the NAR web site in
the certification file. The curve drawn with these data points is as
close to the certification curve as can be with such a limited
number of points (32) allowed with wRASP up to v1.6.
]]></comments>
<data>
<eng-data cg="163." f="0." m="533.1" t="0."/>
<eng-data cg="163." f="251.586" m="532.536" t="0.009"/>
<eng-data cg="163." f="376.074" m="531.441" t="0.016"/>
<eng-data cg="163." f="413.45" m="528.687" t="0.03"/>
<eng-data cg="163." f="430.832" m="524.269" t="0.051"/>
<eng-data cg="163." f="423.296" m="515.117" t="0.094"/>
<eng-data cg="163." f="413.149" m="500.944" t="0.162"/>
<eng-data cg="163." f="395.566" m="480.793" t="0.262"/>
<eng-data cg="163." f="420.182" m="452.335" t="0.402"/>
<eng-data cg="163." f="444.898" m="432.288" t="0.495"/>
<eng-data cg="163." f="504.078" m="358.984" t="0.805"/>
<eng-data cg="163." f="536.028" m="296.005" t="1.048"/>
<eng-data cg="163." f="550.597" m="248.622" t="1.223"/>
<eng-data cg="163." f="563.18" m="227.529" t="1.299"/>
<eng-data cg="163." f="555.319" m="217.775" t="1.334"/>
<eng-data cg="163." f="560.042" m="179.977" t="1.47"/>
<eng-data cg="163." f="559.841" m="147.049" t="1.588"/>
<eng-data cg="163." f="546.98" m="98.5088" t="1.764"/>
<eng-data cg="163." f="516.838" m="56.8911" t="1.921"/>
<eng-data cg="163." f="496.743" m="38.7066" t="1.993"/>
<eng-data cg="163." f="499.154" m="30.7656" t="2.025"/>
<eng-data cg="163." f="479.16" m="25.4025" t="2.047"/>
<eng-data cg="163." f="414.354" m="16.7194" t="2.086"/>
<eng-data cg="163." f="344.525" m="11.2356" t="2.115"/>
<eng-data cg="163." f="252.29" m="7.36905" t="2.141"/>
<eng-data cg="163." f="140.161" m="3.84859" t="2.177"/>
<eng-data cg="163." f="82.78" m="1.84871" t="2.213"/>
<eng-data cg="163." f="50.347" m="0.98623" t="2.239"/>
<eng-data cg="163." f="27.861" m="0.362621" t="2.271"/>
<eng-data cg="163." f="12.86" m="0.108951" t="2.296"/>
<eng-data cg="163." f="0." m="0." t="2.33"/>
</data>
</engine>
</engine-list>
</engine-database>

33
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AMW_J450_1.eng
View File

@ -1,33 +0,0 @@
;
;Animal Motor Works J450 Super Tiger
J450ST 54 326 0 0.5331 1.1964 AMW
0.009 251.586
0.016 376.074
0.030 413.450
0.051 430.832
0.094 423.296
0.162 413.149
0.262 395.566
0.402 420.182
0.495 444.898
0.805 504.078
1.048 536.028
1.223 550.597
1.299 563.180
1.334 555.319
1.470 560.042
1.588 559.841
1.764 546.980
1.921 516.838
1.993 496.743
2.025 499.154
2.047 479.160
2.086 414.354
2.115 344.525
2.141 252.290
2.177 140.161
2.213 82.780
2.239 50.347
2.271 27.861
2.296 12.860
2.330 0.000

23
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AMW_J475.eng
View File

@ -1,23 +0,0 @@
J475-BB 54 403 0 0.714 1.493 AMW/ProX
0.03 30
0.04 500
0.075 600
0.1 515
0.2 530
0.4 540
0.6 535
0.8 535
1 530
1.2 520
1.4 510
1.6 500
1.8 490
2 480
2.2 490
2.28 450
2.43 180
2.5 100
2.6 60
2.8 28
3 10
3.2 0

36
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AMW_J475.rse
View File

@ -1,36 +0,0 @@
<engine-database>
<engine-list>
<engine mfg="AMW-ProX" code="J475-BB" Type="unspecified" dia="54." len="403."
initWt="1493." propWt="714." delays="0" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="385.871" peakThrust="600." throatDia="0." exitDia="0." Itot="1234.79"
burn-time="3.2" massFrac="47.82" Isp="176.35" tDiv="10" tStep="-1." tFix="1"
FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10"
cgStep="-1." cgFix="1">
<data>
<eng-data t="0." f="0." m="714." cg="201.5"/>
<eng-data t="0.03" f="30." m="713.74" cg="201.5"/>
<eng-data t="0.04" f="500." m="712.207" cg="201.5"/>
<eng-data t="0.075" f="600." m="701.076" cg="201.5"/>
<eng-data t="0.1" f="515." m="693.017" cg="201.5"/>
<eng-data t="0.2" f="530." m="662.804" cg="201.5"/>
<eng-data t="0.4" f="540." m="600.933" cg="201.5"/>
<eng-data t="0.6" f="535." m="538.772" cg="201.5"/>
<eng-data t="0.8" f="535." m="476.901" cg="201.5"/>
<eng-data t="1." f="530." m="415.319" cg="201.5"/>
<eng-data t="1.2" f="520." m="354.604" cg="201.5"/>
<eng-data t="1.4" f="510." m="295.046" cg="201.5"/>
<eng-data t="1.6" f="500." m="236.644" cg="201.5"/>
<eng-data t="1.8" f="490." m="179.398" cg="201.5"/>
<eng-data t="2." f="480." m="123.309" cg="201.5"/>
<eng-data t="2.2" f="490." m="67.2201" cg="201.5"/>
<eng-data t="2.28" f="450." m="45.4784" cg="201.5"/>
<eng-data t="2.43" f="180." m="18.1566" cg="201.5"/>
<eng-data t="2.5" f="100." m="12.4899" cg="201.5"/>
<eng-data t="2.6" f="60." m="7.86403" cg="201.5"/>
<eng-data t="2.8" f="28." m="2.77554" cg="201.5"/>
<eng-data t="3." f="10." m="0.578237" cg="201.5"/>
<eng-data t="3.2" f="0." m="0." cg="201.5"/>
</data>
</engine>
</engine-list>
</engine-database>

71
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AMW_J475_1.rse
View File

@ -1,71 +0,0 @@
<engine-database>
<engine-list>
<engine mfg="Cesaroni Technology Inc." code="J475BB" Type="reloadable" dia="54."
len="326." initWt="1410." propWt="723." delays="1000" auto-calc-mass="1"
auto-calc-cg="1" avgThrust="487.929" peakThrust="613.616" throatDia="0."
exitDia="0." Itot="1032.94" burn-time="2.12" massFrac="51.28" Isp="145.69"
tDiv="10" tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10"
mStep="-1." mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<comments>Entered by Tim Van Milligan for RockSim users. Used ThrustCurve Tracer by John
Coker. Data from CAR web site, thrust curve from AMW web site.
</comments>
<data>
<eng-data t="0." f="0." m="723." cg="163."/>
<eng-data t="0.008" f="250.212" m="722.299" cg="163."/>
<eng-data t="0.032" f="402.127" m="716.82" cg="163."/>
<eng-data t="0.037" f="458.723" m="715.314" cg="163."/>
<eng-data t="0.045" f="449.787" m="712.77" cg="163."/>
<eng-data t="0.056" f="464.68" m="709.25" cg="163."/>
<eng-data t="0.077" f="458.723" m="702.463" cg="163."/>
<eng-data t="0.08" f="464.68" m="701.494" cg="163."/>
<eng-data t="0.099" f="455.744" m="695.374" cg="163."/>
<eng-data t="0.117" f="455.744" m="689.632" cg="163."/>
<eng-data t="0.128" f="449.787" m="686.146" cg="163."/>
<eng-data t="0.141" f="455.744" m="682.026" cg="163."/>
<eng-data t="0.155" f="443.829" m="677.618" cg="163."/>
<eng-data t="0.165" f="455.744" m="674.47" cg="163."/>
<eng-data t="0.197" f="464.68" m="664.162" cg="163."/>
<eng-data t="0.232" f="473.616" m="652.669" cg="163."/>
<eng-data t="0.256" f="482.552" m="644.638" cg="163."/>
<eng-data t="0.261" f="491.489" m="642.934" cg="163."/>
<eng-data t="0.267" f="482.552" m="640.888" cg="163."/>
<eng-data t="0.299" f="494.467" m="629.947" cg="163."/>
<eng-data t="0.36" f="515.318" m="608.39" cg="163."/>
<eng-data t="0.459" f="536.169" m="571.959" cg="163."/>
<eng-data t="0.594" f="565.957" m="519.888" cg="163."/>
<eng-data t="0.714" f="580.85" m="471.726" cg="163."/>
<eng-data t="0.826" f="598.722" m="425.491" cg="163."/>
<eng-data t="0.93" f="607.659" m="381.582" cg="163."/>
<eng-data t="1.005" f="613.616" m="349.526" cg="163."/>
<eng-data t="1.074" f="607.659" m="320.035" cg="163."/>
<eng-data t="1.112" f="601.701" m="303.952" cg="163."/>
<eng-data t="1.176" f="598.722" m="277.065" cg="163."/>
<eng-data t="1.25" f="589.786" m="246.285" cg="163."/>
<eng-data t="1.304" f="574.893" m="224.274" cg="163."/>
<eng-data t="1.32" f="580.85" m="217.803" cg="163."/>
<eng-data t="1.333" f="574.893" m="212.545" cg="163."/>
<eng-data t="1.368" f="568.935" m="198.534" cg="163."/>
<eng-data t="1.466" f="533.191" m="160.734" cg="163."/>
<eng-data t="1.568" f="491.489" m="124.156" cg="163."/>
<eng-data t="1.65" f="455.744" m="96.973" cg="163."/>
<eng-data t="1.703" f="428.936" m="80.5636" cg="163."/>
<eng-data t="1.741" f="402.127" m="69.5114" cg="163."/>
<eng-data t="1.765" f="399.148" m="62.7813" cg="163."/>
<eng-data t="1.802" f="387.233" m="52.5985" cg="163."/>
<eng-data t="1.818" f="390.212" m="48.2452" cg="163."/>
<eng-data t="1.826" f="387.233" m="46.0685" cg="163."/>
<eng-data t="1.845" f="387.233" m="40.9187" cg="163."/>
<eng-data t="1.869" f="390.212" m="34.3888" cg="163."/>
<eng-data t="1.879" f="387.233" m="31.6679" cg="163."/>
<eng-data t="1.901" f="375.319" m="25.7968" cg="163."/>
<eng-data t="1.906" f="354.468" m="24.5198" cg="163."/>
<eng-data t="1.938" f="294.893" m="17.2475" cg="163."/>
<eng-data t="1.981" f="214.468" m="9.58231" cg="163."/>
<eng-data t="2.015" f="148.936" m="5.25817" cg="163."/>
<eng-data t="2.061" f="83.404" m="1.51782" cg="163."/>
<eng-data t="2.101" f="17.872" m="0.100075" cg="163."/>
<eng-data t="2.117" f="0." m="0." cg="163."/>
</data>
</engine>
</engine-list>
</engine-database>

32
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AMW_J480.eng
View File

@ -1,32 +0,0 @@
;
;AMW J480 RASP.ENG file made from NAR published data
;File produced April 19, 2004
;The total impulse, peak thrust, average thrust and burn time are
;the same as the averaged static test data on the NAR web site in
;the certification file. The curve drawn with these data points is as
;close to the certification curve as can be with such a limited
;number of points (32) allowed with wRASP up to v1.6.
J480BB 54 326 100 0.556 1.2131 Animal_Motor_Works
0.015 225.429
0.041 348.18
0.071 388.127
0.194 422.453
0.385 459.49
0.699 502.347
0.968 528.042
1.2 536.573
1.454 543.15
1.674 533.763
1.887 522.321
2.044 519.41
2.108 525.131
2.164 528.042
2.197 488.095
2.25 419.543
2.283 333.928
2.328 231.15
2.354 176.95
2.392 111.309
2.418 68.501
2.436 37.106
2.49 0

40
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AMW_J480.rse
View File

@ -1,40 +0,0 @@
<engine-database>
<engine-list>
<engine FDiv="10" FFix="1" FStep="-1." Isp="212.96" Itot="1161.14" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="466.323" burn-time="2.49" cgDiv="10" cgFix="1" cgStep="-1." code="J480BB" delays="1000" dia="54." exitDia="0." initWt="1213.1" len="326." mDiv="10" mFix="1" mStep="-1." massFrac="45.83" mfg="Animal Motor Works" peakThrust="543.15" propWt="556." tDiv="10" tFix="1" tStep="-1." throatDia="0.">
<comments>AMW J480 RASP.ENG file made from NAR published data
File produced April 19, 2004
The total impulse, peak thrust, average thrust and burn time are
the same as the averaged static test data on the NAR web site in
the certification file. The curve drawn with these data points is as
close to the certification curve as can be with such a limited
number of points (32) allowed with wRASP up to v1.6.
</comments>
<data>
<eng-data cg="163." f="0." m="556." t="0."/>
<eng-data cg="163." f="225.429" m="555.19" t="0.015"/>
<eng-data cg="163." f="348.18" m="551.62" t="0.041"/>
<eng-data cg="163." f="388.127" m="546.331" t="0.071"/>
<eng-data cg="163." f="422.453" m="522.461" t="0.194"/>
<eng-data cg="163." f="459.49" m="482.13" t="0.385"/>
<eng-data cg="163." f="502.347" m="409.822" t="0.699"/>
<eng-data cg="163." f="528.042" m="343.461" t="0.968"/>
<eng-data cg="163." f="536.573" m="284.327" t="1.2"/>
<eng-data cg="163." f="543.15" m="218.666" t="1.454"/>
<eng-data cg="163." f="533.763" m="161.943" t="1.674"/>
<eng-data cg="163." f="522.321" m="108.087" t="1.887"/>
<eng-data cg="163." f="519.41" m="68.9294" t="2.044"/>
<eng-data cg="163." f="525.131" m="52.9241" t="2.108"/>
<eng-data cg="163." f="528.042" m="38.8037" t="2.164"/>
<eng-data cg="163." f="488.095" m="30.7754" t="2.197"/>
<eng-data cg="163." f="419.543" m="19.2582" t="2.25"/>
<eng-data cg="163." f="333.928" m="13.3051" t="2.283"/>
<eng-data cg="163." f="231.15" m="7.21708" t="2.328"/>
<eng-data cg="163." f="176.95" m="4.6767" t="2.354"/>
<eng-data cg="163." f="111.309" m="2.05414" t="2.392"/>
<eng-data cg="163." f="68.501" m="0.934847" t="2.418"/>
<eng-data cg="163." f="37.106" m="0.479729" t="2.436"/>
<eng-data cg="163." f="0." m="0." t="2.49"/>
</data>
</engine>
</engine-list>
</engine-database>

32
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AMW_J500.eng
View File

@ -1,32 +0,0 @@
;
;J500ST entered by Tim Van Milligan
;For RockSim - http://www.rocksim.com
;Based on TRA Certification paperwork from 06-01-2002
;Initial Mass from Jim Robinson at AMW
;Not approved by TRA or AMW.
J500ST 38 370 20 0.3265 0.744 Animal_Motor_Works
0.006 444.822
0.025 475.651
0.04 418.397
0.053 466.843
0.059 409.589
0.071 458.035
0.077 409.589
0.1 444.822
0.127 506.481
0.204 590.16
0.25 644.992
0.3 678.244
0.34 709.073
0.402 735.498
0.445 766.327
0.516 783.944
0.6 787.335
0.637 770.732
0.68 744.306
0.76 620.989
0.859 475.651
1.00464 303.888
1.122 171.763
1.227 52.8502
1.3 0

40
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AMW_J500.rse
View File

@ -1,40 +0,0 @@
<engine-database>
<engine-list>
<engine FDiv="10" FFix="1" FStep="-1." Isp="204.22" Itot="653.892" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="502.994" burn-time="1.3" cgDiv="10" cgFix="1" cgStep="-1." code="J500ST" delays="20" dia="38." exitDia="0." initWt="744." len="370." mDiv="10" mFix="1" mStep="-1." massFrac="43.88" mfg="Animal Motor Works" peakThrust="787.335" propWt="326.5" tDiv="10" tFix="1" tStep="-1." throatDia="0.">
<comments>J500ST entered by Tim Van Milligan
For RockSim - http://www.rocksim.com
Based on TRA Certification paperwork from 06-01-2002
Initial Mass from Jim Robinson at AMW
Not approved by TRA or AMW.
</comments>
<data>
<eng-data cg="185." f="0." m="326.5" t="0."/>
<eng-data cg="185." f="444.822" m="325.834" t="0.006"/>
<eng-data cg="185." f="475.651" m="321.467" t="0.025"/>
<eng-data cg="185." f="418.397" m="318.119" t="0.04"/>
<eng-data cg="185." f="466.843" m="315.246" t="0.053"/>
<eng-data cg="185." f="409.589" m="313.933" t="0.059"/>
<eng-data cg="185." f="458.035" m="311.334" t="0.071"/>
<eng-data cg="185." f="409.589" m="310.034" t="0.077"/>
<eng-data cg="185." f="444.822" m="305.128" t="0.1"/>
<eng-data cg="185." f="506.481" m="298.716" t="0.127"/>
<eng-data cg="185." f="590.16" m="277.634" t="0.204"/>
<eng-data cg="185." f="644.992" m="263.449" t="0.25"/>
<eng-data cg="185." f="678.244" m="246.931" t="0.3"/>
<eng-data cg="185." f="709.073" m="233.077" t="0.34"/>
<eng-data cg="185." f="735.498" m="210.717" t="0.402"/>
<eng-data cg="185." f="766.327" m="194.594" t="0.445"/>
<eng-data cg="185." f="783.944" m="167.114" t="0.516"/>
<eng-data cg="185." f="787.335" m="134.163" t="0.6"/>
<eng-data cg="185." f="770.732" m="119.77" t="0.637"/>
<eng-data cg="185." f="744.306" m="103.506" t="0.68"/>
<eng-data cg="185." f="620.989" m="76.237" t="0.76"/>
<eng-data cg="185." f="475.651" m="49.1321" t="0.859"/>
<eng-data cg="185." f="303.888" m="20.7878" t="1.00464"/>
<eng-data cg="185." f="171.763" m="6.85126" t="1.122"/>
<eng-data cg="185." f="52.8502" m="0.963201" t="1.227"/>
<eng-data cg="185." f="0." m="0." t="1.3"/>
</data>
</engine>
</engine-list>
</engine-database>

75
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AMW_J745.rse
View File

@ -1,75 +0,0 @@
<engine-database>
<engine-list>
<engine mfg="Cesaroni Technology Inc." code="J745WW" Type="reloadable" dia="54."
len="326." initWt="1220." propWt="549." delays="1000" auto-calc-mass="1"
auto-calc-cg="1" avgThrust="744.284" peakThrust="864.521" throatDia="0."
exitDia="0." Itot="1198.3" burn-time="1.61" massFrac="45." Isp="222.57" tDiv="10"
tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."
mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<comments>Entered by Tim Van Milligan for RockSim users. Used ThrustCurve Tracer by John
Coker. Data from CAR web site, thrust curve from AMW web site.
</comments>
<data>
<eng-data t="0." f="0." m="549." cg="163."/>
<eng-data t="0.016" f="666.494" m="546.557" cg="163."/>
<eng-data t="0.019" f="715.262" m="545.608" cg="163."/>
<eng-data t="0.029" f="744.818" m="542.263" cg="163."/>
<eng-data t="0.04" f="746.296" m="538.506" cg="163."/>
<eng-data t="0.053" f="768.463" m="533.995" cg="163."/>
<eng-data t="0.063" f="778.808" m="530.45" cg="163."/>
<eng-data t="0.075" f="812.798" m="526.075" cg="163."/>
<eng-data t="0.087" f="823.142" m="521.578" cg="163."/>
<eng-data t="0.112" f="839.398" m="512.057" cg="163."/>
<eng-data t="0.127" f="834.965" m="506.304" cg="163."/>
<eng-data t="0.144" f="846.787" m="499.754" cg="163."/>
<eng-data t="0.156" f="846.787" m="495.099" cg="163."/>
<eng-data t="0.173" f="848.265" m="488.498" cg="163."/>
<eng-data t="0.205" f="848.265" m="476.062" cg="163."/>
<eng-data t="0.213" f="848.265" m="472.953" cg="163."/>
<eng-data t="0.221" f="858.61" m="469.825" cg="163."/>
<eng-data t="0.242" f="858.61" m="461.564" cg="163."/>
<eng-data t="0.269" f="860.088" m="450.934" cg="163."/>
<eng-data t="0.279" f="863.043" m="446.986" cg="163."/>
<eng-data t="0.3" f="860.088" m="438.697" cg="163."/>
<eng-data t="0.322" f="864.521" m="430.006" cg="163."/>
<eng-data t="0.34" f="861.566" m="422.888" cg="163."/>
<eng-data t="0.348" f="858.61" m="419.736" cg="163."/>
<eng-data t="0.362" f="861.566" m="414.219" cg="163."/>
<eng-data t="0.385" f="860.088" m="405.148" cg="163."/>
<eng-data t="0.414" f="858.61" m="393.731" cg="163."/>
<eng-data t="0.443" f="855.654" m="382.343" cg="163."/>
<eng-data t="0.459" f="861.566" m="376.049" cg="163."/>
<eng-data t="0.47" f="858.61" m="371.714" cg="163."/>
<eng-data t="0.478" f="861.566" m="368.562" cg="163."/>
<eng-data t="0.489" f="855.654" m="364.235" cg="163."/>
<eng-data t="0.528" f="849.743" m="348.999" cg="163."/>
<eng-data t="0.55" f="855.654" m="340.404" cg="163."/>
<eng-data t="0.585" f="848.265" m="326.743" cg="163."/>
<eng-data t="0.619" f="849.743" m="313.518" cg="163."/>
<eng-data t="0.637" f="846.787" m="306.522" cg="163."/>
<eng-data t="0.661" f="846.787" m="297.211" cg="163."/>
<eng-data t="0.736" f="834.965" m="268.318" cg="163."/>
<eng-data t="0.826" f="817.231" m="234.255" cg="163."/>
<eng-data t="0.92" f="795.064" m="199.537" cg="163."/>
<eng-data t="1.057" f="755.163" m="150.886" cg="163."/>
<eng-data t="1.156" f="722.651" m="117.372" cg="163."/>
<eng-data t="1.228" f="707.873" m="93.7776" cg="163."/>
<eng-data t="1.305" f="693.095" m="69.0662" cg="163."/>
<eng-data t="1.347" f="679.794" m="55.8575" cg="163."/>
<eng-data t="1.392" f="666.494" m="41.9794" cg="163."/>
<eng-data t="1.416" f="666.494" m="34.6509" cg="163."/>
<eng-data t="1.426" f="666.494" m="31.5974" cg="163."/>
<eng-data t="1.448" f="666.494" m="24.8796" cg="163."/>
<eng-data t="1.477" f="666.494" m="16.0243" cg="163."/>
<eng-data t="1.48" f="665.016" m="15.1093" cg="163."/>
<eng-data t="1.485" f="633.982" m="13.6214" cg="163."/>
<eng-data t="1.493" f="561.569" m="11.4305" cg="163."/>
<eng-data t="1.515" f="366.498" m="6.75335" cg="163."/>
<eng-data t="1.533" f="257.14" m="4.18187" cg="163."/>
<eng-data t="1.555" f="162.56" m="2.06673" cg="163."/>
<eng-data t="1.583" f="81.28" m="0.502719" cg="163."/>
<eng-data t="1.61" f="0." m="0." cg="163."/>
</data>
</engine>
</engine-list>
</engine-database>

37
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AMW_K1000.eng
View File

@ -1,37 +0,0 @@
;
;AMW K1000 RASP.ENG file made from NAR published data
;File produced April 19, 2004
;The total impulse, peak thrust, average thrust and burn time are
;the same as the averaged static test data on the NAR web site in
;the certification file. The curve drawn with these data points is as
;close to the certification curve as can be with such a limited
;number of points (32) allowed with wRASP up to v1.6.
K1000SK 54 728 100 1.297 2.556 Animal_Motor_Works
0.019 1155.06
0.045 1426.12
0.094 1248.23
0.161 1112.99
0.239 1128.02
0.343 1113.99
0.377 1149.05
0.44 1121
0.544 1221.18
0.633 1178.11
0.674 1221.18
0.737 1193.13
0.883 1200.14
1.009 1194.13
1.057 1236.21
1.188 1137.03
1.299 1145.05
1.396 1087.94
1.516 954.104
1.631 855.228
1.717 827.077
1.777 650.061
1.848 465.932
1.93 303.141
2.023 147.463
2.083 83.879
2.132 41.484
2.18 0

45
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AMW_K1000.rse
View File

@ -1,45 +0,0 @@
<engine-database>
<engine-list>
<engine FDiv="10" FFix="1" FStep="-1." Isp="163.34" Itot="2077.51" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="952.987" burn-time="2.18" cgDiv="10" cgFix="1" cgStep="-1." code="K1000SK" delays="1000" dia="54." exitDia="0." initWt="2556." len="728." mDiv="10" mFix="1" mStep="-1." massFrac="50.74" mfg="Animal Motor Works" peakThrust="1426.12" propWt="1297." tDiv="10" tFix="1" tStep="-1." throatDia="0.">
<comments>AMW K1000 RASP.ENG file made from NAR published data
File produced April 19, 2004
The total impulse, peak thrust, average thrust and burn time are
the same as the averaged static test data on the NAR web site in
the certification file. The curve drawn with these data points is as
close to the certification curve as can be with such a limited
number of points (32) allowed with wRASP up to v1.6.
</comments>
<data>
<eng-data cg="364." f="0." m="1297." t="0."/>
<eng-data cg="364." f="1155.06" m="1290.15" t="0.019"/>
<eng-data cg="364." f="1426.12" m="1269.2" t="0.045"/>
<eng-data cg="364." f="1248.23" m="1228.3" t="0.094"/>
<eng-data cg="364." f="1112.99" m="1178.91" t="0.161"/>
<eng-data cg="364." f="1128.02" m="1124.35" t="0.239"/>
<eng-data cg="364." f="1113.99" m="1051.56" t="0.343"/>
<eng-data cg="364." f="1149.05" m="1027.55" t="0.377"/>
<eng-data cg="364." f="1121." m="982.904" t="0.44"/>
<eng-data cg="364." f="1221.18" m="906.868" t="0.544"/>
<eng-data cg="364." f="1178.11" m="840.212" t="0.633"/>
<eng-data cg="364." f="1221.18" m="809.506" t="0.674"/>
<eng-data cg="364." f="1193.13" m="762.027" t="0.737"/>
<eng-data cg="364." f="1200.14" m="652.955" t="0.883"/>
<eng-data cg="364." f="1194.13" m="558.786" t="1.009"/>
<eng-data cg="364." f="1236.21" m="522.371" t="1.057"/>
<eng-data cg="364." f="1137.03" m="425.325" t="1.188"/>
<eng-data cg="364." f="1145.05" m="346.253" t="1.299"/>
<eng-data cg="364." f="1087.94" m="278.641" t="1.396"/>
<eng-data cg="364." f="954.104" m="202.15" t="1.516"/>
<eng-data cg="364." f="855.228" m="137.199" t="1.631"/>
<eng-data cg="364." f="827.077" m="92.0376" t="1.717"/>
<eng-data cg="364." f="650.061" m="64.3721" t="1.777"/>
<eng-data cg="364." f="465.932" m="39.6386" t="1.848"/>
<eng-data cg="364." f="303.141" m="19.953" t="1.93"/>
<eng-data cg="364." f="147.463" m="6.87189" t="2.023"/>
<eng-data cg="364." f="83.879" m="2.53905" t="2.083"/>
<eng-data cg="364." f="41.484" m="0.621567" t="2.132"/>
<eng-data cg="364." f="0." m="0." t="2.18"/>
</data>
</engine>
</engine-list>
</engine-database>

41
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AMW_K1075.eng
View File

@ -1,41 +0,0 @@
; AMW 54-2500 Skidmark Plugged
2245-K1075-SK-P 54 728 P 1.259 2.6388 CTI
0.0070 1574.366
0.012 1038.184
0.017 1476.101
0.024 1083.044
0.029 1365.02
0.034 1117.223
0.041 1266.756
0.046 1162.083
0.049 1226.168
0.069 1159.947
0.107 1130.04
0.151 1108.678
0.21 1100.134
0.274 1102.27
0.332 1102.27
0.432 1115.087
0.523 1119.359
0.611 1132.176
0.674 1140.721
0.766 1149.266
0.881 1159.947
0.979 1179.172
1.141 1191.989
1.257 1189.853
1.379 1191.989
1.504 1202.67
1.599 1211.215
1.67 1232.577
1.744 1249.666
1.772 1226.168
1.802 1155.674
1.841 993.324
1.888 736.983
1.944 455.007
2.002 267.023
2.065 128.171
2.11 68.358
2.149 34.179
2.198 0.0

54
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AMW_K1075.rse
View File

@ -1,54 +0,0 @@
<engine-database>
<engine-list>
<engine mfg="CTI" code="2245-K1075-SK-P" Type="reloadable" dia="54." len="728."
initWt="2638.8" propWt="1259." delays="0" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="1026." peakThrust="1574.37" throatDia="0." exitDia="0." Itot="2255.14"
burn-time="2.2" massFrac="47.71" Isp="182.65" tDiv="10" tStep="-1." tFix="1"
FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10"
cgStep="-1." cgFix="1">
<comments>AMW 54-2500 Skidmark Plugged</comments>
<data>
<eng-data t="0." f="0." m="1259." cg="364."/>
<eng-data t="0.007" f="1574.37" m="1255.92" cg="364."/>
<eng-data t="0.012" f="1038.18" m="1252.28" cg="364."/>
<eng-data t="0.017" f="1476.1" m="1248.77" cg="364."/>
<eng-data t="0.024" f="1083.04" m="1243.77" cg="364."/>
<eng-data t="0.029" f="1365.02" m="1240.35" cg="364."/>
<eng-data t="0.034" f="1117.22" m="1236.89" cg="364."/>
<eng-data t="0.041" f="1266.76" m="1232.23" cg="364."/>
<eng-data t="0.046" f="1162.08" m="1228.84" cg="364."/>
<eng-data t="0.049" f="1226.17" m="1226.84" cg="364."/>
<eng-data t="0.069" f="1159.95" m="1213.52" cg="364."/>
<eng-data t="0.107" f="1130.04" m="1189.23" cg="364."/>
<eng-data t="0.151" f="1108.68" m="1161.73" cg="364."/>
<eng-data t="0.21" f="1100.13" m="1125.35" cg="364."/>
<eng-data t="0.274" f="1102.27" m="1086.01" cg="364."/>
<eng-data t="0.332" f="1102.27" m="1050.32" cg="364."/>
<eng-data t="0.432" f="1115.09" m="988.42" cg="364."/>
<eng-data t="0.523" f="1119.36" m="931.661" cg="364."/>
<eng-data t="0.611" f="1132.18" m="876.353" cg="364."/>
<eng-data t="0.674" f="1140.72" m="836.383" cg="364."/>
<eng-data t="0.766" f="1149.27" m="777.574" cg="364."/>
<eng-data t="0.881" f="1159.95" m="703.445" cg="364."/>
<eng-data t="0.979" f="1179.17" m="639.457" cg="364."/>
<eng-data t="1.141" f="1191.99" m="532.232" cg="364."/>
<eng-data t="1.257" f="1189.85" m="455.107" cg="364."/>
<eng-data t="1.379" f="1191.99" m="373.993" cg="364."/>
<eng-data t="1.504" f="1202.67" m="290.437" cg="364."/>
<eng-data t="1.599" f="1211.21" m="226.425" cg="364."/>
<eng-data t="1.67" f="1232.58" m="177.992" cg="364."/>
<eng-data t="1.744" f="1249.67" m="126.718" cg="364."/>
<eng-data t="1.772" f="1226.17" m="107.367" cg="364."/>
<eng-data t="1.802" f="1155.67" m="87.4209" cg="364."/>
<eng-data t="1.841" f="993.324" m="64.0259" cg="364."/>
<eng-data t="1.888" f="736.983" m="41.325" cg="364."/>
<eng-data t="1.944" f="455.007" m="22.692" cg="364."/>
<eng-data t="2.002" f="267.023" m="11.0022" cg="364."/>
<eng-data t="2.065" f="128.171" m="4.05242" cg="364."/>
<eng-data t="2.11" f="68.358" m="1.58376" cg="364."/>
<eng-data t="2.149" f="34.179" m="0.467496" cg="364."/>
<eng-data t="2.198" f="0." m="0." cg="364."/>
</data>
</engine>
</engine-list>
</engine-database>

39
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AMW_K1075_1.eng
View File

@ -1,39 +0,0 @@
;
;Animal Motor Works K1075 RASP.ENG file made from NAR data
;File produced Feb 22, 2003
;The total impulse, peak thrust, average thrust and burn time are
;the same as the averaged static test data on the NAR web site in
;the certification file. The curve drawn with these data points is as
;close to the certification curve as can be with such a limited
;number of points (32) allowed with wRASP up to v1.6.
K1075GG 54 726 100 1.3999 2.6658 Animal_Motor_Works
0.009 672.664
0.015 963.511
0.022 860.518
0.047 987.857
0.075 975.835
0.106 921.332
0.215 958.001
0.529 1092.05
0.878 1220.29
1.077 1269.39
1.158 1311.47
1.235 1293.43
1.448 1330.5
1.577 1318.48
1.672 1319.48
1.721 1337.52
1.759 1337.52
1.805 1337.52
1.829 1331.5
1.856 1384.67
1.889 1277.4
1.906 1216.29
1.938 1052.98
1.96 871.338
1.988 659.239
2.027 453.352
2.062 301.967
2.115 138.46
2.168 41.608
2.2 0

47
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AMW_K1075_1.rse
View File

@ -1,47 +0,0 @@
<engine-database>
<engine-list>
<engine FDiv="10" FFix="1" FStep="-1." Isp="174.27" Itot="2392.45" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="1087.48" burn-time="2.2" cgDiv="10" cgFix="1" cgStep="-1." code="K1075GG" delays="1000" dia="54." exitDia="0." initWt="2665.8" len="726." mDiv="10" mFix="1" mStep="-1." massFrac="52.51" mfg="Animal Motor Works" peakThrust="1384.67" propWt="1399.9" tDiv="10" tFix="1" tStep="-1." throatDia="0.">
<comments>Animal Motor Works K1075 RASP.ENG file made from NAR data
File produced Feb 22, 2003
The total impulse, peak thrust, average thrust and burn time are
the same as the averaged static test data on the NAR web site in
the certification file. The curve drawn with these data points is as
close to the certification curve as can be with such a limited
number of points (32) allowed with wRASP up to v1.6.
</comments>
<data>
<eng-data cg="363." f="0." m="1399.9" t="0."/>
<eng-data cg="363." f="672.664" m="1398.13" t="0.009"/>
<eng-data cg="363." f="963.511" m="1395.26" t="0.015"/>
<eng-data cg="363." f="860.518" m="1391.52" t="0.022"/>
<eng-data cg="363." f="987.857" m="1378." t="0.047"/>
<eng-data cg="363." f="975.835" m="1361.92" t="0.075"/>
<eng-data cg="363." f="921.332" m="1344.71" t="0.106"/>
<eng-data cg="363." f="958.001" m="1284.78" t="0.215"/>
<eng-data cg="363." f="1092.05" m="1096.45" t="0.529"/>
<eng-data cg="363." f="1220.29" m="860.344" t="0.878"/>
<eng-data cg="363." f="1269.39" m="715.393" t="1.077"/>
<eng-data cg="363." f="1311.47" m="654.232" t="1.158"/>
<eng-data cg="363." f="1293.43" m="595.55" t="1.235"/>
<eng-data cg="363." f="1330.5" m="432.035" t="1.448"/>
<eng-data cg="363." f="1318.48" m="332.06" t="1.577"/>
<eng-data cg="363." f="1319.48" m="258.741" t="1.672"/>
<eng-data cg="363." f="1337.52" m="220.651" t="1.721"/>
<eng-data cg="363." f="1337.52" m="190.911" t="1.759"/>
<eng-data cg="363." f="1337.52" m="154.91" t="1.805"/>
<eng-data cg="363." f="1331.5" m="136.169" t="1.829"/>
<eng-data cg="363." f="1384.67" m="114.714" t="1.856"/>
<eng-data cg="363." f="1277.4" m="89.0121" t="1.889"/>
<eng-data cg="363." f="1216.29" m="76.6094" t="1.906"/>
<eng-data cg="363." f="1052.98" m="55.3642" t="1.938"/>
<eng-data cg="363." f="871.338" m="42.9784" t="1.96"/>
<eng-data cg="363." f="659.239" m="30.4401" t="1.988"/>
<eng-data cg="363." f="453.352" m="17.7453" t="2.027"/>
<eng-data cg="363." f="301.967" m="10.011" t="2.062"/>
<eng-data cg="363." f="138.46" m="3.18168" t="2.115"/>
<eng-data cg="363." f="41.608" m="0.38954" t="2.168"/>
<eng-data cg="363." f="0." m="0." t="2.2"/>
</data>
</engine>
</engine-list>
</engine-database>

18
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AMW_K1130.eng
View File

@ -1,18 +0,0 @@
; Blue Baboon
K1130-BB 54 728 0 1.359 2.574 AMW/ProX
0.01 1000
0.013 1490
0.02 1548
0.04 1500
0.09 1335
0.2 1325
1 1325
1.5 1325
1.63 1345
1.7 1155
1.8 805
1.9 685
2 475
2.1 315
2.2 145
2.3 0

30
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AMW_K1130.rse
View File

@ -1,30 +0,0 @@
<engine-database>
<engine-list>
<engine mfg="AMW-ProX" code="K1130-BB" Type="unspecified" dia="54." len="728."
initWt="2574." propWt="1359." delays="0" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="1109.05" peakThrust="1548." throatDia="0." exitDia="0." Itot="2550.82"
burn-time="2.3" massFrac="52.8" Isp="191.4" tDiv="10" tStep="-1." tFix="1"
FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10"
cgStep="-1." cgFix="1">
<data>
<eng-data t="0." f="0." m="1359." cg="364."/>
<eng-data t="0.01" f="1000." m="1356.34" cg="364."/>
<eng-data t="0.013" f="1490." m="1354.35" cg="364."/>
<eng-data t="0.02" f="1548." m="1348.68" cg="364."/>
<eng-data t="0.04" f="1500." m="1332.44" cg="364."/>
<eng-data t="0.09" f="1335." m="1294.68" cg="364."/>
<eng-data t="0.2" f="1325." m="1216.74" cg="364."/>
<eng-data t="1." f="1325." m="652.003" cg="364."/>
<eng-data t="1.5" f="1325." m="299.043" cg="364."/>
<eng-data t="1.63" f="1345." m="206.581" cg="364."/>
<eng-data t="1.7" f="1155." m="159.964" cg="364."/>
<eng-data t="1.8" f="805." m="107.753" cg="364."/>
<eng-data t="1.9" f="685." m="68.0613" cg="364."/>
<eng-data t="2." f="475." m="37.1607" cg="364."/>
<eng-data t="2.1" f="315." m="16.1163" cg="364."/>
<eng-data t="2.2" f="145." m="3.86258" cg="364."/>
<eng-data t="2.3" f="0." m="0." cg="364."/>
</data>
</engine>
</engine-list>
</engine-database>

18
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AMW_K1250.eng
View File

@ -1,18 +0,0 @@
K1250-WW 54 491 0 0.925 1.815 AMW/ProX
0.01 600
0.02 1400
0.03 1610
0.05 1360
0.07 1410
0.1 1440
0.15 1470
0.2 1480
0.4 1480
0.8 1395
1.28 1185
1.36 985
1.4 680
1.45 570
1.5 210
1.6 60
1.7 0

31
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AMW_K1250.rse
View File

@ -1,31 +0,0 @@
<engine-database>
<engine-list>
<engine mfg="AMW-ProX" code="K1250-WW" Type="unspecified" dia="54." len="491."
initWt="1815." propWt="925." delays="0" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="1148.38" peakThrust="1610." throatDia="0." exitDia="0." Itot="1952.25"
burn-time="1.7" massFrac="50.96" Isp="215.22" tDiv="10" tStep="-1." tFix="1"
FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10"
cgStep="-1." cgFix="1">
<data>
<eng-data t="0." f="0." m="925." cg="245.5"/>
<eng-data t="0.01" f="600." m="923.579" cg="245.5"/>
<eng-data t="0.02" f="1400." m="918.84" cg="245.5"/>
<eng-data t="0.03" f="1610." m="911.71" cg="245.5"/>
<eng-data t="0.05" f="1360." m="897.637" cg="245.5"/>
<eng-data t="0.07" f="1410." m="884.513" cg="245.5"/>
<eng-data t="0.1" f="1440." m="864.257" cg="245.5"/>
<eng-data t="0.15" f="1470." m="829.787" cg="245.5"/>
<eng-data t="0.2" f="1480." m="794.844" cg="245.5"/>
<eng-data t="0.4" f="1480." m="654.595" cg="245.5"/>
<eng-data t="0.8" f="1395." m="382.153" cg="245.5"/>
<eng-data t="1.28" f="1185." m="88.7687" cg="245.5"/>
<eng-data t="1.36" f="985." m="47.6418" cg="245.5"/>
<eng-data t="1.4" f="680." m="31.8639" cg="245.5"/>
<eng-data t="1.45" f="570." m="17.0572" cg="245.5"/>
<eng-data t="1.5" f="210." m="7.8179" cg="245.5"/>
<eng-data t="1.6" f="60." m="1.42144" cg="245.5"/>
<eng-data t="1.7" f="0." m="0." cg="245.5"/>
</data>
</engine>
</engine-list>
</engine-database>

65
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AMW_K1720.rse
View File

@ -1,65 +0,0 @@
<engine-database>
<engine-list>
<engine mfg="Cesaroni Technology Inc." code="K1720ST" Type="reloadable" dia="54."
len="403." initWt="1500." propWt="592." delays="1000" auto-calc-mass="1"
auto-calc-cg="1" avgThrust="1730.35" peakThrust="1928.26" throatDia="0."
exitDia="0." Itot="1183.56" burn-time="0.68" massFrac="39.47" Isp="203.87"
tDiv="10" tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10"
mStep="-1." mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<comments>Input by Tim Van Milligan for RockSim users. Used John Coker's ThrustCruve
Tracer program. Thrust curve from the AMW web site and CAR/NAR/TRA certified
rocket motor list dated 9/28/08. The total weight was estimated based on
similar motors such as the K455TT, K535RR and K665BB.
</comments>
<data>
<eng-data t="0." f="0." m="592." cg="201.5"/>
<eng-data t="0.007" f="1806.44" m="588.838" cg="201.5"/>
<eng-data t="0.011" f="1608.04" m="585.422" cg="201.5"/>
<eng-data t="0.016" f="1702.02" m="581.283" cg="201.5"/>
<eng-data t="0.02" f="1514.07" m="578.065" cg="201.5"/>
<eng-data t="0.024" f="1743.79" m="574.806" cg="201.5"/>
<eng-data t="0.029" f="1541.91" m="570.698" cg="201.5"/>
<eng-data t="0.032" f="1750.75" m="568.227" cg="201.5"/>
<eng-data t="0.039" f="1597.6" m="562.365" cg="201.5"/>
<eng-data t="0.042" f="1736.83" m="559.864" cg="201.5"/>
<eng-data t="0.047" f="1691.58" m="555.577" cg="201.5"/>
<eng-data t="0.05" f="1747.27" m="552.997" cg="201.5"/>
<eng-data t="0.054" f="1715.94" m="549.532" cg="201.5"/>
<eng-data t="0.058" f="1736.83" m="546.078" cg="201.5"/>
<eng-data t="0.065" f="1771.63" m="539.936" cg="201.5"/>
<eng-data t="0.072" f="1764.67" m="533.745" cg="201.5"/>
<eng-data t="0.081" f="1823.84" m="525.668" cg="201.5"/>
<eng-data t="0.09" f="1827.32" m="517.45" cg="201.5"/>
<eng-data t="0.115" f="1858.65" m="494.404" cg="201.5"/>
<eng-data t="0.137" f="1879.53" m="473.836" cg="201.5"/>
<eng-data t="0.144" f="1869.09" m="467.274" cg="201.5"/>
<eng-data t="0.148" f="1823.84" m="463.579" cg="201.5"/>
<eng-data t="0.15" f="1844.72" m="461.744" cg="201.5"/>
<eng-data t="0.17" f="1865.61" m="443.186" cg="201.5"/>
<eng-data t="0.201" f="1886.49" m="414.096" cg="201.5"/>
<eng-data t="0.234" f="1910.86" m="382.757" cg="201.5"/>
<eng-data t="0.276" f="1917.82" m="342.54" cg="201.5"/>
<eng-data t="0.312" f="1928.26" m="307.913" cg="201.5"/>
<eng-data t="0.345" f="1921.3" m="276.142" cg="201.5"/>
<eng-data t="0.384" f="1914.34" m="238.731" cg="201.5"/>
<eng-data t="0.426" f="1886.49" m="198.807" cg="201.5"/>
<eng-data t="0.487" f="1827.32" m="142.151" cg="201.5"/>
<eng-data t="0.526" f="1792.51" m="106.844" cg="201.5"/>
<eng-data t="0.555" f="1757.71" m="81.0954" cg="201.5"/>
<eng-data t="0.575" f="1750.75" m="63.5466" cg="201.5"/>
<eng-data t="0.593" f="1736.83" m="47.8466" cg="201.5"/>
<eng-data t="0.604" f="1736.83" m="38.2905" cg="201.5"/>
<eng-data t="0.615" f="1726.38" m="28.7632" cg="201.5"/>
<eng-data t="0.621" f="1702.02" m="23.6187" cg="201.5"/>
<eng-data t="0.624" f="1649.81" m="21.1038" cg="201.5"/>
<eng-data t="0.628" f="1590.64" m="17.8622" cg="201.5"/>
<eng-data t="0.631" f="1548.87" m="15.5067" cg="201.5"/>
<eng-data t="0.643" f="964.129" m="7.96486" cg="201.5"/>
<eng-data t="0.655" f="518.611" m="3.51499" cg="201.5"/>
<eng-data t="0.666" f="268.007" m="1.35098" cg="201.5"/>
<eng-data t="0.674" f="180.992" m="0.452649" cg="201.5"/>
<eng-data t="0.684" f="0." m="0." cg="201.5"/>
</data>
</engine>
</engine-list>
</engine-database>

35
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AMW_K365.eng
View File

@ -1,35 +0,0 @@
;
;AMW K365RR RASP.ENG file made from NAR published data
;File produced April 19, 2004
;The total impulse, peak thrust, average thrust and burn time are
;the same as the averaged static test data on the NAR web site in
;the certification file. The curve drawn with these data points is as
;close to the certification curve as can be with such a limited
;number of points (32) allowed with wRASP up to v1.6.
K365RR 75 111 100 0.946 2.3456 Animal_Motor_Works
0.049 138.157
0.068 381.241
0.084 454.75
0.106 481.536
0.164 488.182
0.291 514.867
0.435 545.982
0.666 561.49
0.868 565.73
1.082 565.518
1.296 550.111
1.591 529.871
1.805 509.731
1.828 536.517
1.886 498.554
2.124 467.237
2.501 411.35
2.924 328.677
3.296 241.573
3.638 172.293
3.969 100.798
4.195 56.098
4.265 51.607
4.346 35.959
4.433 15.859
4.51 0

43
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AMW_K365.rse
View File

@ -1,43 +0,0 @@
<engine-database>
<engine-list>
<engine FDiv="10" FFix="1" FStep="-1." Isp="180.58" Itot="1675.27" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="371.456" burn-time="4.51" cgDiv="10" cgFix="1" cgStep="-1." code="K365RR" delays="1000" dia="75." exitDia="0." initWt="2345.6" len="111." mDiv="10" mFix="1" mStep="-1." massFrac="40.33" mfg="Animal Motor Works" peakThrust="565.73" propWt="946." tDiv="10" tFix="1" tStep="-1." throatDia="0.">
<comments>AMW K365RR RASP.ENG file made from NAR published data
File produced April 19, 2004
The total impulse, peak thrust, average thrust and burn time are
the same as the averaged static test data on the NAR web site in
the certification file. The curve drawn with these data points is as
close to the certification curve as can be with such a limited
number of points (32) allowed with wRASP up to v1.6.
</comments>
<data>
<eng-data cg="55.5" f="0." m="946." t="0."/>
<eng-data cg="55.5" f="138.157" m="944.089" t="0.049"/>
<eng-data cg="55.5" f="381.241" m="941.302" t="0.068"/>
<eng-data cg="55.5" f="454.75" m="937.526" t="0.084"/>
<eng-data cg="55.5" f="481.536" m="931.71" t="0.106"/>
<eng-data cg="55.5" f="488.182" m="915.83" t="0.164"/>
<eng-data cg="55.5" f="514.867" m="879.863" t="0.291"/>
<eng-data cg="55.5" f="545.982" m="836.732" t="0.435"/>
<eng-data cg="55.5" f="561.49" m="764.501" t="0.666"/>
<eng-data cg="55.5" f="565.73" m="700.212" t="0.868"/>
<eng-data cg="55.5" f="565.518" m="631.86" t="1.082"/>
<eng-data cg="55.5" f="550.111" m="564.452" t="1.296"/>
<eng-data cg="55.5" f="529.871" m="474.499" t="1.591"/>
<eng-data cg="55.5" f="509.731" m="411.685" t="1.805"/>
<eng-data cg="55.5" f="536.517" m="404.891" t="1.828"/>
<eng-data cg="55.5" f="498.554" m="387.941" t="1.886"/>
<eng-data cg="55.5" f="467.237" m="323.042" t="2.124"/>
<eng-data cg="55.5" f="411.35" m="229.522" t="2.501"/>
<eng-data cg="55.5" f="328.677" m="141.14" t="2.924"/>
<eng-data cg="55.5" f="241.573" m="81.2457" t="3.296"/>
<eng-data cg="55.5" f="172.293" m="41.2823" t="3.638"/>
<eng-data cg="55.5" f="100.798" m="15.7604" t="3.969"/>
<eng-data cg="55.5" f="56.098" m="5.74893" t="4.195"/>
<eng-data cg="55.5" f="51.607" m="3.62025" t="4.265"/>
<eng-data cg="55.5" f="35.959" m="1.61763" t="4.346"/>
<eng-data cg="55.5" f="15.859" m="0.344781" t="4.433"/>
<eng-data cg="55.5" f="0." m="0." t="4.51"/>
</data>
</engine>
</engine-list>
</engine-database>

35
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AMW_K450.eng
View File

@ -1,35 +0,0 @@
;
;AMW K450BB RASP.ENG file made from NAR published data
;File produced Aug 19, 2003
;This file my be used or given away. All I ask is that this header
;is maintained to give credit to NAR S&T. Thank you, Jack Kane.
;The total impulse, peak thrust, average thrust and burn time are
;the same as the averaged static test data on the NAR web site in
;the certification file. The curve drawn with these data points is as
;close to the certification curve as can be with such a limited
;number of points (32) allowed with wRASP up to v1.6.
K450BB 75 302 100 0.8816 2.8349 Animal_Motor_Works
0.03 78.903
0.045 227.9
0.064 449.955
0.069 508.417
0.094 555.187
0.151 563.956
0.362 625.442
0.562 651.85
0.825 660.62
1.134 652.254
1.453 626.147
1.793 594.296
2.113 538.958
2.458 469.106
2.798 384.538
3.165 276.686
3.201 279.609
3.325 232.94
3.51 171.757
3.732 107.65
3.861 58.018
3.959 40.55
4.036 20.149
4.11 0

43
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AMW_K450.rse
View File

@ -1,43 +0,0 @@
<engine-database>
<engine-list>
<engine FDiv="10" FFix="1" FStep="-1." Isp="213.76" Itot="1848.03" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="449.643" burn-time="4.11" cgDiv="10" cgFix="1" cgStep="-1." code="K450BB" delays="1000" dia="75." exitDia="0." initWt="2834.9" len="302." mDiv="10" mFix="1" mStep="-1." massFrac="31.1" mfg="Animal Motor Works" peakThrust="660.62" propWt="881.6" tDiv="10" tFix="1" tStep="-1." throatDia="0.">
<comments><![CDATA[AMW K450BB RASP.ENG file made from NAR published data
File produced Aug 19, 2003
This file my be used or given away. All I ask is that this header
is maintained to give credit to NAR S&T. Thank you, Jack Kane.
The total impulse, peak thrust, average thrust and burn time are
the same as the averaged static test data on the NAR web site in
the certification file. The curve drawn with these data points is as
close to the certification curve as can be with such a limited
number of points (32) allowed with wRASP up to v1.6.
]]></comments>
<data>
<eng-data cg="151." f="0." m="881.6" t="0."/>
<eng-data cg="151." f="78.903" m="881.035" t="0.03"/>
<eng-data cg="151." f="227.9" m="879.938" t="0.045"/>
<eng-data cg="151." f="449.955" m="876.866" t="0.064"/>
<eng-data cg="151." f="508.417" m="875.723" t="0.069"/>
<eng-data cg="151." f="555.187" m="869.38" t="0.094"/>
<eng-data cg="151." f="563.956" m="854.165" t="0.151"/>
<eng-data cg="151." f="625.442" m="794.304" t="0.362"/>
<eng-data cg="151." f="651.85" m="733.371" t="0.562"/>
<eng-data cg="151." f="660.62" m="651.038" t="0.825"/>
<eng-data cg="151." f="652.254" m="554.274" t="1.134"/>
<eng-data cg="151." f="626.147" m="457.001" t="1.453"/>
<eng-data cg="151." f="594.296" m="358.026" t="1.793"/>
<eng-data cg="151." f="538.958" m="271.527" t="2.113"/>
<eng-data cg="151." f="469.106" m="188.573" t="2.458"/>
<eng-data cg="151." f="384.538" m="119.344" t="2.798"/>
<eng-data cg="151." f="276.686" m="61.4618" t="3.165"/>
<eng-data cg="151." f="279.609" m="56.6849" t="3.201"/>
<eng-data cg="151." f="232.94" m="41.5253" t="3.325"/>
<eng-data cg="151." f="171.757" m="23.6673" t="3.51"/>
<eng-data cg="151." f="107.65" m="8.87205" t="3.732"/>
<eng-data cg="151." f="58.018" m="3.77452" t="3.861"/>
<eng-data cg="151." f="40.55" m="1.47046" t="3.959"/>
<eng-data cg="151." f="20.149" m="0.355645" t="4.036"/>
<eng-data cg="151." f="0." m="0." t="4.11"/>
</data>
</engine>
</engine-list>
</engine-database>

59
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AMW_K455.rse
View File

@ -1,59 +0,0 @@
<engine-database>
<engine-list>
<engine mfg="Cesaroni Technology Inc." code="K455TT" Type="reloadable" dia="54."
len="403." initWt="1504." propWt="716." delays="1000" auto-calc-mass="1"
auto-calc-cg="1" avgThrust="457.266" peakThrust="789.038" throatDia="0."
exitDia="0." Itot="1481.54" burn-time="3.24" massFrac="47.61" Isp="211."
tDiv="10" tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10"
mStep="-1." mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<comments>Entered by Tim Van Milligan for RockSim users. Used ThrustCurve Tracer by John
Coker. Data from CAR web site, thrust curve from AMW web site.
</comments>
<data>
<eng-data t="0." f="0." m="716." cg="201.5"/>
<eng-data t="0.021" f="715.739" m="712.368" cg="201.5"/>
<eng-data t="0.035" f="789.038" m="707.277" cg="201.5"/>
<eng-data t="0.052" f="735.861" m="701.013" cg="201.5"/>
<eng-data t="0.069" f="689.869" m="695.157" cg="201.5"/>
<eng-data t="0.09" f="684.12" m="688.184" cg="201.5"/>
<eng-data t="0.114" f="681.246" m="680.266" cg="201.5"/>
<eng-data t="0.138" f="691.307" m="672.306" cg="201.5"/>
<eng-data t="0.19" f="682.683" m="655.042" cg="201.5"/>
<eng-data t="0.345" f="663.999" m="604.603" cg="201.5"/>
<eng-data t="0.528" f="645.315" m="546.705" cg="201.5"/>
<eng-data t="0.583" f="641.004" m="529.609" cg="201.5"/>
<eng-data t="0.735" f="625.194" m="483.103" cg="201.5"/>
<eng-data t="0.835" f="616.571" m="453.097" cg="201.5"/>
<eng-data t="0.983" f="589.263" m="409.973" cg="201.5"/>
<eng-data t="1.163" f="567.705" m="359.65" cg="201.5"/>
<eng-data t="1.304" f="544.709" m="321.749" cg="201.5"/>
<eng-data t="1.598" f="492.969" m="248.03" cg="201.5"/>
<eng-data t="1.663" f="480.034" m="232.747" cg="201.5"/>
<eng-data t="1.932" f="434.043" m="173.331" cg="201.5"/>
<eng-data t="1.984" f="426.857" m="162.514" cg="201.5"/>
<eng-data t="2.019" f="426.857" m="155.293" cg="201.5"/>
<eng-data t="2.077" f="408.173" m="143.59" cg="201.5"/>
<eng-data t="2.119" f="405.298" m="135.334" cg="201.5"/>
<eng-data t="2.157" f="399.549" m="127.944" cg="201.5"/>
<eng-data t="2.205" f="388.052" m="118.809" cg="201.5"/>
<eng-data t="2.232" f="386.614" m="113.755" cg="201.5"/>
<eng-data t="2.315" f="369.368" m="98.5927" cg="201.5"/>
<eng-data t="2.364" f="363.619" m="89.9139" cg="201.5"/>
<eng-data t="2.398" f="360.744" m="83.9627" cg="201.5"/>
<eng-data t="2.433" f="346.372" m="77.9823" cg="201.5"/>
<eng-data t="2.481" f="340.623" m="70.0141" cg="201.5"/>
<eng-data t="2.522" f="333.437" m="63.336" cg="201.5"/>
<eng-data t="2.636" f="306.13" m="45.7179" cg="201.5"/>
<eng-data t="2.705" f="286.008" m="35.845" cg="201.5"/>
<eng-data t="2.753" f="267.324" m="29.4271" cg="201.5"/>
<eng-data t="2.802" f="240.017" m="23.42" cg="201.5"/>
<eng-data t="2.85" f="206.961" m="18.2356" cg="201.5"/>
<eng-data t="2.916" f="159.532" m="12.3907" cg="201.5"/>
<eng-data t="3.012" f="106.355" m="6.22278" cg="201.5"/>
<eng-data t="3.081" f="79.048" m="3.13153" cg="201.5"/>
<eng-data t="3.164" f="40.242" m="0.73903" cg="201.5"/>
<eng-data t="3.24" f="0." m="0." cg="201.5"/>
</data>
</engine>
</engine-list>
</engine-database>

36
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AMW_K470.eng
View File

@ -1,36 +0,0 @@
;
;AMW K470ST RASP.ENG file made from Tripoli published data
;File produced May 15, 2004
;This file my be used or given away. All I ask is that this header
;is maintained to give credit to the people who produced the data.
;The total impulse, peak thrust, average thrust and burn time are
;the same as the averaged static test data on the NAR web site in
;the certification file. The curve drawn with these data points is as
;close to the certification curve as can be with such a limited
;number of points (32) allowed with wRASP up to v1.6.
K470ST 75 302 100 0.826 2.779 Animal_Motor_Works
0.028 699.309
0.039 799.337
0.09 765.845
0.157 770.311
0.258 785.941
0.41 804
0.572 794.425
0.707 794.425
0.886 792.192
0.998 783.261
1.15 752.002
1.318 709.579
1.447 655.992
1.593 595.707
1.728 522.025
1.885 444.101
2.092 354.923
2.356 270.167
2.664 187.554
2.945 131.734
3.27 78.058
3.433 55.686
3.478 48.987
3.556 28.909
3.7 0

44
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AMW_K470.rse
View File

@ -1,44 +0,0 @@
<engine-database>
<engine-list>
<engine FDiv="10" FFix="1" FStep="-1." Isp="207.28" Itot="1679." Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="453.784" burn-time="3.7" cgDiv="10" cgFix="1" cgStep="-1." code="K470ST" delays="1000" dia="75." exitDia="0." initWt="2779." len="302." mDiv="10" mFix="1" mStep="-1." massFrac="29.72" mfg="Animal Motor Works" peakThrust="804." propWt="826." tDiv="10" tFix="1" tStep="-1." throatDia="0.">
<comments>AMW K470ST RASP.ENG file made from Tripoli published data
File produced May 15, 2004
This file my be used or given away. All I ask is that this header
is maintained to give credit to the people who produced the data.
The total impulse, peak thrust, average thrust and burn time are
the same as the averaged static test data on the NAR web site in
the certification file. The curve drawn with these data points is as
close to the certification curve as can be with such a limited
number of points (32) allowed with wRASP up to v1.6.
</comments>
<data>
<eng-data cg="151." f="0." m="826." t="0."/>
<eng-data cg="151." f="699.309" m="821.184" t="0.028"/>
<eng-data cg="151." f="799.337" m="817.129" t="0.039"/>
<eng-data cg="151." f="765.845" m="797.493" t="0.09"/>
<eng-data cg="151." f="770.311" m="772.177" t="0.157"/>
<eng-data cg="151." f="785.941" m="733.513" t="0.258"/>
<eng-data cg="151." f="804." m="674.067" t="0.41"/>
<eng-data cg="151." f="794.425" m="610.372" t="0.572"/>
<eng-data cg="151." f="794.425" m="557.61" t="0.707"/>
<eng-data cg="151." f="792.192" m="487.751" t="0.886"/>
<eng-data cg="151." f="783.261" m="444.348" t="0.998"/>
<eng-data cg="151." f="752.002" m="386.946" t="1.15"/>
<eng-data cg="151." f="709.579" m="326.547" t="1.318"/>
<eng-data cg="151." f="655.992" m="283.215" t="1.447"/>
<eng-data cg="151." f="595.707" m="238.263" t="1.593"/>
<eng-data cg="151." f="522.025" m="201.146" t="1.728"/>
<eng-data cg="151." f="444.101" m="163.835" t="1.885"/>
<eng-data cg="151." f="354.923" m="123.151" t="2.092"/>
<eng-data cg="151." f="270.167" m="82.5581" t="2.356"/>
<eng-data cg="151." f="187.554" m="47.8804" t="2.664"/>
<eng-data cg="151." f="131.734" m="25.8111" t="2.945"/>
<eng-data cg="151." f="78.058" m="9.0396" t="3.27"/>
<eng-data cg="151." f="55.686" m="3.67717" t="3.433"/>
<eng-data cg="151." f="48.987" m="2.51853" t="3.478"/>
<eng-data cg="151." f="28.909" m="1.02399" t="3.556"/>
<eng-data cg="151." f="0." m="0." t="3.7"/>
</data>
</engine>
</engine-list>
</engine-database>

38
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AMW_K475.eng
View File

@ -1,38 +0,0 @@
;
;Animal Motor Works K475 RASP.ENG file made from NAR data
;File produced Feb 22, 2003
;The total impulse, peak thrust, average thrust and burn time are
;the same as the averaged static test data on the NAR web site in
;the certification file. The curve drawn with these data points is as
;close to the certification curve as can be with such a limited
;number of points (32) allowed with wRASP up to v1.6.
K475WW 54 403 100 0.7286 1.4925 Animal_Motor_Works
0.022 127.831
0.041 386.016
0.063 548.326
0.096 521.308
0.134 499.129
0.18 486.83
0.285 486.83
0.478 501.649
0.731 523.727
1.096 553.266
1.433 577.962
1.601 588.29
1.756 582.704
1.895 580.284
1.958 575.344
2.063 550.746
2.209 518.788
2.344 477.051
2.495 417.974
2.561 354.058
2.582 334.399
2.599 331.98
2.62 297.501
2.67 226.226
2.707 157.37
2.74 98.353
2.799 49.176
2.853 17.208
2.94 0

46
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AMW_K475.rse
View File

@ -1,46 +0,0 @@
<engine-database>
<engine-list>
<engine FDiv="10" FFix="1" FStep="-1." Isp="195.08" Itot="1393.88" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="474.108" burn-time="2.94" cgDiv="10" cgFix="1" cgStep="-1." code="K475WW" delays="1000" dia="54." exitDia="0." initWt="1492.5" len="403." mDiv="10" mFix="1" mStep="-1." massFrac="48.82" mfg="Animal Motor Works" peakThrust="588.29" propWt="728.6" tDiv="10" tFix="1" tStep="-1." throatDia="0.">
<comments>Animal Motor Works K475 RASP.ENG file made from NAR data
File produced Feb 22, 2003
The total impulse, peak thrust, average thrust and burn time are
the same as the averaged static test data on the NAR web site in
the certification file. The curve drawn with these data points is as
close to the certification curve as can be with such a limited
number of points (32) allowed with wRASP up to v1.6.
</comments>
<data>
<eng-data cg="201.5" f="0." m="728.6" t="0."/>
<eng-data cg="201.5" f="127.831" m="727.865" t="0.022"/>
<eng-data cg="201.5" f="386.016" m="725.313" t="0.041"/>
<eng-data cg="201.5" f="548.326" m="719.941" t="0.063"/>
<eng-data cg="201.5" f="521.308" m="710.716" t="0.096"/>
<eng-data cg="201.5" f="499.129" m="700.581" t="0.134"/>
<eng-data cg="201.5" f="486.83" m="688.727" t="0.18"/>
<eng-data cg="201.5" f="486.83" m="662.008" t="0.285"/>
<eng-data cg="201.5" f="501.649" m="612.147" t="0.478"/>
<eng-data cg="201.5" f="523.727" m="544.346" t="0.731"/>
<eng-data cg="201.5" f="553.266" m="441.605" t="1.096"/>
<eng-data cg="201.5" f="577.962" m="341.97" t="1.433"/>
<eng-data cg="201.5" f="588.29" m="290.762" t="1.601"/>
<eng-data cg="201.5" f="582.704" m="243.324" t="1.756"/>
<eng-data cg="201.5" f="580.284" m="201.074" t="1.895"/>
<eng-data cg="201.5" f="575.344" m="182.046" t="1.958"/>
<eng-data cg="201.5" f="550.746" m="151.144" t="2.063"/>
<eng-data cg="201.5" f="518.788" m="110.332" t="2.209"/>
<eng-data cg="201.5" f="477.051" m="75.1958" t="2.344"/>
<eng-data cg="201.5" f="417.974" m="39.8736" t="2.495"/>
<eng-data cg="201.5" f="354.058" m="26.5564" t="2.561"/>
<eng-data cg="201.5" f="334.399" m="22.7778" t="2.582"/>
<eng-data cg="201.5" f="331.98" m="19.817" t="2.599"/>
<eng-data cg="201.5" f="297.501" m="16.3621" t="2.62"/>
<eng-data cg="201.5" f="226.226" m="9.5181" t="2.67"/>
<eng-data cg="201.5" f="157.37" m="5.80864" t="2.707"/>
<eng-data cg="201.5" f="98.353" m="3.60308" t="2.74"/>
<eng-data cg="201.5" f="49.176" m="1.32817" t="2.799"/>
<eng-data cg="201.5" f="17.208" m="0.391277" t="2.853"/>
<eng-data cg="201.5" f="0." m="0." t="2.94"/>
</data>
</engine>
</engine-list>
</engine-database>

36
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AMW_K500.eng
View File

@ -1,36 +0,0 @@
; Entered by Tim Van Milligan. Used John Coker's ThrustCurve Tracer software and
; data from NAR certification dated May 7, 2007
K500SK 75 368 100 1.1235 2.713 Animal
0.018 194.373
0.031 207.161
0.036 268.542
0.103 319.693
0.138 322.251
0.17 314.578
0.67 309.463
0.692 322.251
0.902 319.693
0.929 332.481
1.263 355.499
1.585 383.632
1.969 411.765
2.112 416.88
2.272 447.57
2.415 488.491
2.46 485.934
2.634 534.527
2.83 618.926
3.018 710.997
3.143 767.263
3.228 815.857
3.339 841.432
3.402 826.087
3.504 785.166
3.585 718.67
3.661 631.714
3.728 519.182
3.772 365.729
3.826 181.586
3.862 99.744
3.893 43.478
3.946 0.0

50
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AMW_K500.rse
View File

@ -1,50 +0,0 @@
<engine-database>
<engine-list>
<engine mfg="Animal" code="K500SK" Type="reloadable" dia="75." len="368." initWt="2713."
propWt="1123.5" delays="1000" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="455.234" peakThrust="841.432" throatDia="0." exitDia="0."
Itot="1796.35" burn-time="3.95" massFrac="41.41" Isp="163.04" tDiv="10"
tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."
mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<comments>Entered by Tim Van Milligan. Used John Coker's ThrustCurve Tracer software and
data from NAR certification dated May 7, 2007
</comments>
<data>
<eng-data t="0." f="0." m="1123.5" cg="184."/>
<eng-data t="0.018" f="194.373" m="1122.41" cg="184."/>
<eng-data t="0.031" f="207.161" m="1120.77" cg="184."/>
<eng-data t="0.036" f="268.542" m="1120.03" cg="184."/>
<eng-data t="0.103" f="319.693" m="1107.71" cg="184."/>
<eng-data t="0.138" f="322.251" m="1100.68" cg="184."/>
<eng-data t="0.17" f="314.578" m="1094.31" cg="184."/>
<eng-data t="0.67" f="309.463" m="996.732" cg="184."/>
<eng-data t="0.692" f="322.251" m="992.386" cg="184."/>
<eng-data t="0.902" f="319.693" m="950.229" cg="184."/>
<eng-data t="0.929" f="332.481" m="944.723" cg="184."/>
<eng-data t="1.263" f="355.499" m="872.865" cg="184."/>
<eng-data t="1.585" f="383.632" m="798.438" cg="184."/>
<eng-data t="1.969" f="411.765" m="702.924" cg="184."/>
<eng-data t="2.112" f="416.88" m="665.869" cg="184."/>
<eng-data t="2.272" f="447.57" m="622.616" cg="184."/>
<eng-data t="2.415" f="488.491" m="580.757" cg="184."/>
<eng-data t="2.46" f="485.934" m="567.044" cg="184."/>
<eng-data t="2.634" f="534.527" m="511.518" cg="184."/>
<eng-data t="2.83" f="618.926" m="440.82" cg="184."/>
<eng-data t="3.018" f="710.997" m="362.633" cg="184."/>
<eng-data t="3.143" f="767.263" m="304.849" cg="184."/>
<eng-data t="3.228" f="815.857" m="262.768" cg="184."/>
<eng-data t="3.339" f="841.432" m="205.241" cg="184."/>
<eng-data t="3.402" f="826.087" m="172.389" cg="184."/>
<eng-data t="3.504" f="785.166" m="120.994" cg="184."/>
<eng-data t="3.585" f="718.67" m="82.902" cg="184."/>
<eng-data t="3.661" f="631.714" m="50.8081" cg="184."/>
<eng-data t="3.728" f="519.182" m="26.6945" cg="184."/>
<eng-data t="3.772" f="365.729" m="14.5185" cg="184."/>
<eng-data t="3.826" f="181.586" m="5.27619" cg="184."/>
<eng-data t="3.862" f="99.744" m="2.10903" cg="184."/>
<eng-data t="3.893" f="43.478" m="0.720604" cg="184."/>
<eng-data t="3.946" f="0." m="0." cg="184."/>
</data>
</engine>
</engine-list>
</engine-database>

43
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AMW_K530.eng
View File

@ -1,43 +0,0 @@
;
;Animal Motor Works 54-1400
;AMW K530GG RASP.ENG file made from NAR data
;File produced Feb 25, 2003
;This file my be used or given away. All I ask is that this header
;is maintained to give credit to NAR S&T. Thank you, Jack Kane
;The total impulse, peak thrust, average thrust and burn time are
;the same as the averaged static test data on the NAR web site in
;the certification file. The curve drawn with these data points is as
;close to the certification curve as can be with such a limited
;number of points (32) allowed with wRASP up to v1.6.
K530GG 54 403 1000 0.7967 1.616 Animal_Motor_Works
0.013 129.764
0.054 171.852
0.096 284.122
0.138 392.892
0.171 455.975
0.217 501.662
0.238 498.063
0.326 508.66
0.542 564.745
0.755 613.831
1.01 645.423
1.17 657.23
1.273 648.922
1.51 638.425
1.656 634.925
1.702 606.833
1.803 606.833
1.857 585.839
1.936 589.338
1.974 575.242
2.015 589.338
2.04 564.745
2.132 536.652
2.207 540.251
2.291 522.656
2.357 487.566
2.42 375.297
2.478 242.033
2.529 140.361
2.583 66.651
2.66 0

51
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AMW_K530.rse
View File

@ -1,51 +0,0 @@
<engine-database>
<engine-list>
<engine FDiv="10" FFix="1" FStep="-1." Isp="179.39" Itot="1401.55" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="526.897" burn-time="2.66" cgDiv="10" cgFix="1" cgStep="-1." code="K530GG" delays="1000" dia="54." exitDia="0." initWt="1616." len="403." mDiv="10" mFix="1" mStep="-1." massFrac="49.3" mfg="Animal Motor Works" peakThrust="657.23" propWt="796.7" tDiv="10" tFix="1" tStep="-1." throatDia="0.">
<comments><![CDATA[Animal Motor Works 54-1400
AMW K530GG RASP.ENG file made from NAR data
File produced Feb 25, 2003
This file my be used or given away. All I ask is that this header
is maintained to give credit to NAR S&T. Thank you, Jack Kane
The total impulse, peak thrust, average thrust and burn time are
the same as the averaged static test data on the NAR web site in
the certification file. The curve drawn with these data points is as
close to the certification curve as can be with such a limited
number of points (32) allowed with wRASP up to v1.6.
]]></comments>
<data>
<eng-data cg="201.5" f="0." m="796.7" t="0."/>
<eng-data cg="201.5" f="129.764" m="796.221" t="0.013"/>
<eng-data cg="201.5" f="171.852" m="792.706" t="0.054"/>
<eng-data cg="201.5" f="284.122" m="787.263" t="0.096"/>
<eng-data cg="201.5" f="392.892" m="779.181" t="0.138"/>
<eng-data cg="201.5" f="455.975" m="771.219" t="0.171"/>
<eng-data cg="201.5" f="501.662" m="758.699" t="0.217"/>
<eng-data cg="201.5" f="498.063" m="752.732" t="0.238"/>
<eng-data cg="201.5" f="508.66" m="727.552" t="0.326"/>
<eng-data cg="201.5" f="564.745" m="661.654" t="0.542"/>
<eng-data cg="201.5" f="613.831" m="590.303" t="0.755"/>
<eng-data cg="201.5" f="645.423" m="499.037" t="1.01"/>
<eng-data cg="201.5" f="657.23" m="439.798" t="1.17"/>
<eng-data cg="201.5" f="648.922" m="401.561" t="1.273"/>
<eng-data cg="201.5" f="638.425" m="314.844" t="1.51"/>
<eng-data cg="201.5" f="634.925" m="262.005" t="1.656"/>
<eng-data cg="201.5" f="606.833" m="245.77" t="1.702"/>
<eng-data cg="201.5" f="606.833" m="210.93" t="1.803"/>
<eng-data cg="201.5" f="585.839" m="192.625" t="1.857"/>
<eng-data cg="201.5" f="589.338" m="166.238" t="1.936"/>
<eng-data cg="201.5" f="575.242" m="153.66" t="1.974"/>
<eng-data cg="201.5" f="589.338" m="140.089" t="2.015"/>
<eng-data cg="201.5" f="564.745" m="131.889" t="2.04"/>
<eng-data cg="201.5" f="536.652" m="103.089" t="2.132"/>
<eng-data cg="201.5" f="540.251" m="80.1328" t="2.207"/>
<eng-data cg="201.5" f="522.656" m="54.7562" t="2.291"/>
<eng-data cg="201.5" f="487.566" m="35.8058" t="2.357"/>
<eng-data cg="201.5" f="375.297" m="20.3554" t="2.42"/>
<eng-data cg="201.5" f="242.033" m="10.1788" t="2.478"/>
<eng-data cg="201.5" f="140.361" m="4.63588" t="2.529"/>
<eng-data cg="201.5" f="66.651" m="1.45866" t="2.583"/>
<eng-data cg="201.5" f="0." m="0." t="2.66"/>
</data>
</engine>
</engine-list>
</engine-database>

85
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AMW_K535.rse
View File

@ -1,85 +0,0 @@
<engine-database>
<engine-list>
<engine mfg="Cesaroni Technology Inc." code="K535RR" Type="reloadable" dia="54."
len="403." initWt="1559." propWt="764." delays="1000" auto-calc-mass="1"
auto-calc-cg="1" avgThrust="529.945" peakThrust="629.683" throatDia="0."
exitDia="0." Itot="1436.15" burn-time="2.71" massFrac="49.01" Isp="191.68"
tDiv="10" tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10"
mStep="-1." mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<comments>Entered by Tim Van Milligan for RockSim users. Used ThrustCurve Tracer by John
Coker. Data from CAR web site, thrust curve from AMW web site.
</comments>
<data>
<eng-data t="0." f="0." m="764." cg="201.5"/>
<eng-data t="0.023" f="447.71" m="761.261" cg="201.5"/>
<eng-data t="0.04" f="534.364" m="756.82" cg="201.5"/>
<eng-data t="0.049" f="547.362" m="754.231" cg="201.5"/>
<eng-data t="0.078" f="569.026" m="745.619" cg="201.5"/>
<eng-data t="0.092" f="564.693" m="741.397" cg="201.5"/>
<eng-data t="0.116" f="553.139" m="734.262" cg="201.5"/>
<eng-data t="0.139" f="574.802" m="727.361" cg="201.5"/>
<eng-data t="0.173" f="589.245" m="716.834" cg="201.5"/>
<eng-data t="0.199" f="606.575" m="708.564" cg="201.5"/>
<eng-data t="0.222" f="605.131" m="701.151" cg="201.5"/>
<eng-data t="0.246" f="616.685" m="693.351" cg="201.5"/>
<eng-data t="0.277" f="619.574" m="683.158" cg="201.5"/>
<eng-data t="0.298" f="625.35" m="676.204" cg="201.5"/>
<eng-data t="0.318" f="621.018" m="669.573" cg="201.5"/>
<eng-data t="0.35" f="623.906" m="658.977" cg="201.5"/>
<eng-data t="0.378" f="626.795" m="649.662" cg="201.5"/>
<eng-data t="0.402" f="623.906" m="641.678" cg="201.5"/>
<eng-data t="0.439" f="626.795" m="629.369" cg="201.5"/>
<eng-data t="0.462" f="628.239" m="621.691" cg="201.5"/>
<eng-data t="0.517" f="623.906" m="603.373" cg="201.5"/>
<eng-data t="0.572" f="623.906" m="585.118" cg="201.5"/>
<eng-data t="0.592" f="629.683" m="578.45" cg="201.5"/>
<eng-data t="0.612" f="622.462" m="571.788" cg="201.5"/>
<eng-data t="0.647" f="625.35" m="560.172" cg="201.5"/>
<eng-data t="0.691" f="618.129" m="545.619" cg="201.5"/>
<eng-data t="0.722" f="613.797" m="535.461" cg="201.5"/>
<eng-data t="0.743" f="621.018" m="528.563" cg="201.5"/>
<eng-data t="0.771" f="621.018" m="519.313" cg="201.5"/>
<eng-data t="0.826" f="613.797" m="501.248" cg="201.5"/>
<eng-data t="0.861" f="608.02" m="489.874" cg="201.5"/>
<eng-data t="0.919" f="602.243" m="471.203" cg="201.5"/>
<eng-data t="0.988" f="603.687" m="449.07" cg="201.5"/>
<eng-data t="1.034" f="596.466" m="434.386" cg="201.5"/>
<eng-data t="1.101" f="599.354" m="413.075" cg="201.5"/>
<eng-data t="1.147" f="584.912" m="398.584" cg="201.5"/>
<eng-data t="1.19" f="583.468" m="385.221" cg="201.5"/>
<eng-data t="1.219" f="586.356" m="376.197" cg="201.5"/>
<eng-data t="1.265" f="576.247" m="361.972" cg="201.5"/>
<eng-data t="1.326" f="576.247" m="343.273" cg="201.5"/>
<eng-data t="1.346" f="570.47" m="337.173" cg="201.5"/>
<eng-data t="1.375" f="569.026" m="328.383" cg="201.5"/>
<eng-data t="1.416" f="566.137" m="316.003" cg="201.5"/>
<eng-data t="1.485" f="571.914" m="295.116" cg="201.5"/>
<eng-data t="1.531" f="567.581" m="281.174" cg="201.5"/>
<eng-data t="1.56" f="550.251" m="272.552" cg="201.5"/>
<eng-data t="1.58" f="557.472" m="266.659" cg="201.5"/>
<eng-data t="1.673" f="547.362" m="239.329" cg="201.5"/>
<eng-data t="1.725" f="554.583" m="224.087" cg="201.5"/>
<eng-data t="1.754" f="547.362" m="215.587" cg="201.5"/>
<eng-data t="1.783" f="540.141" m="207.198" cg="201.5"/>
<eng-data t="1.811" f="543.029" m="199.131" cg="201.5"/>
<eng-data t="1.936" f="532.92" m="163.357" cg="201.5"/>
<eng-data t="2.109" f="519.922" m="114.91" cg="201.5"/>
<eng-data t="2.184" f="511.256" m="94.3387" cg="201.5"/>
<eng-data t="2.236" f="502.591" m="80.3158" cg="201.5"/>
<eng-data t="2.262" f="501.147" m="73.3742" cg="201.5"/>
<eng-data t="2.288" f="502.591" m="66.4327" cg="201.5"/>
<eng-data t="2.317" f="491.037" m="58.7681" cg="201.5"/>
<eng-data t="2.355" f="467.93" m="49.0753" cg="201.5"/>
<eng-data t="2.395" f="447.71" m="39.3333" cg="201.5"/>
<eng-data t="2.444" f="407.272" m="28.19" cg="201.5"/>
<eng-data t="2.473" f="382.72" m="22.0962" cg="201.5"/>
<eng-data t="2.511" f="322.063" m="14.9726" cg="201.5"/>
<eng-data t="2.542" f="252.74" m="10.2329" cg="201.5"/>
<eng-data t="2.574" f="194.971" m="6.42219" cg="201.5"/>
<eng-data t="2.612" f="125.648" m="3.18151" cg="201.5"/>
<eng-data t="2.652" f="70.767" m="1.09175" cg="201.5"/>
<eng-data t="2.71" f="0." m="0." cg="201.5"/>
</data>
</engine>
</engine-list>
</engine-database>

33
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AMW_K555.eng
View File

@ -1,33 +0,0 @@
;Animal Motor Works 54-1750 K555 skidmark
;File provide by Joel Rogers of AMW
K555SK 54 492 0 0.8707 1.7343 AMW
0.063 507.328
0.144 535.181
0.226 559.826
0.308 585.793
0.389 607.239
0.471 629.034
0.553 664.586
0.634 683.688
0.716 697.625
0.798 719.618
0.879 756.521
0.961 777.700
1.043 789.004
1.124 797.934
1.206 801.689
1.288 804.331
1.369 799.414
1.451 768.014
1.533 704.469
1.614 641.709
1.696 568.727
1.778 481.013
1.859 401.614
1.941 333.897
2.023 277.226
2.104 205.009
2.186 129.425
2.268 73.717
2.349 22.380
2.368 0.000

45
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AMW_K555.rse
View File

@ -1,45 +0,0 @@
<engine-database>
<engine-list>
<engine mfg="Animal Motor Works" code="K555SK" Type="reloadable" dia="54." len="492."
initWt="1737." propWt="878.4" delays="1000" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="560.673" peakThrust="936.468" throatDia="0." exitDia="0."
Itot="1309.73" burn-time="2.34" massFrac="50.57" Isp="152.04" tDiv="10"
tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."
mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<comments>AMW K555 RASP.ENG file from Robert at AMW.</comments>
<data>
<eng-data t="0." f="0." m="878.4" cg="246."/>
<eng-data t="0.061" f="508.351" m="868.001" cg="246."/>
<eng-data t="0.141" f="538.032" m="839.93" cg="246."/>
<eng-data t="0.222" f="573.058" m="809.751" cg="246."/>
<eng-data t="0.302" f="604.249" m="778.167" cg="246."/>
<eng-data t="0.383" f="631.13" m="744.612" cg="246."/>
<eng-data t="0.463" f="666.503" m="709.8" cg="246."/>
<eng-data t="0.544" f="696.284" m="672.784" cg="246."/>
<eng-data t="0.624" f="741.988" m="634.2" cg="246."/>
<eng-data t="0.705" f="787.186" m="592.664" cg="246."/>
<eng-data t="0.786" f="832.036" m="548.682" cg="246."/>
<eng-data t="0.866" f="869.416" m="503.038" cg="246."/>
<eng-data t="0.947" f="880.989" m="455.493" cg="246."/>
<eng-data t="1.027" f="912.349" m="407.383" cg="246."/>
<eng-data t="1.108" f="933.915" m="357.235" cg="246."/>
<eng-data t="1.188" f="936.468" m="307.058" cg="246."/>
<eng-data t="1.269" f="880.77" m="257.698" cg="246."/>
<eng-data t="1.349" f="784.951" m="213.012" cg="246."/>
<eng-data t="1.43" f="679.973" m="173.222" cg="246."/>
<eng-data t="1.511" f="572.224" m="139.209" cg="246."/>
<eng-data t="1.591" f="482.275" m="110.92" cg="246."/>
<eng-data t="1.672" f="407.793" m="86.7442" cg="246."/>
<eng-data t="1.752" f="347.675" m="66.4774" cg="246."/>
<eng-data t="1.833" f="286.395" m="49.2547" cg="246."/>
<eng-data t="1.913" f="235.942" m="35.242" cg="246."/>
<eng-data t="1.994" f="189.94" m="23.6742" cg="246."/>
<eng-data t="2.074" f="145.318" m="14.6802" cg="246."/>
<eng-data t="2.155" f="107.471" m="7.81394" cg="246."/>
<eng-data t="2.236" f="70.697" m="2.97451" cg="246."/>
<eng-data t="2.316" f="32.145" m="0.215587" cg="246."/>
<eng-data t="2.336" f="0." m="0." cg="246."/>
</data>
</engine>
</engine-list>
</engine-database>

37
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AMW_K560.eng
View File

@ -1,37 +0,0 @@
;
;AMW K560 RASP.ENG file made from NAR published data
;File produced April 19, 2004
;The total impulse, peak thrust, average thrust and burn time are
;the same as the averaged static test data on the NAR web site in
;the certification file. The curve drawn with these data points is as
;close to the certification curve as can be with such a limited
;number of points (32) allowed with wRASP up to v1.6.
K560RR 54 430 100 0.75 1.5866 Animal_Motor_Works
0.023 229.13
0.046 415.135
0.059 485.264
0.078 512.268
0.106 525.67
0.154 523.05
0.211 528.39
0.261 536.451
0.369 560.734
0.511 587.738
0.657 603.86
0.77 612.022
1.096 625.75
1.358 620.083
1.627 612.022
1.839 603.86
2.057 590.459
2.218 598.52
2.335 609.301
2.385 601.24
2.407 585.018
2.426 533.831
2.467 385.511
2.507 283.037
2.542 164.441
2.576 67.399
2.595 29.653
2.62 0

45
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AMW_K560.rse
View File

@ -1,45 +0,0 @@
<engine-database>
<engine-list>
<engine FDiv="10" FFix="1" FStep="-1." Isp="200.34" Itot="1473.47" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="562.394" burn-time="2.62" cgDiv="10" cgFix="1" cgStep="-1." code="K560RR" delays="1000" dia="54." exitDia="0." initWt="1586.6" len="430." mDiv="10" mFix="1" mStep="-1." massFrac="47.27" mfg="Animal Motor Works" peakThrust="625.75" propWt="750." tDiv="10" tFix="1" tStep="-1." throatDia="0.">
<comments>AMW K560 RASP.ENG file made from NAR published data
File produced April 19, 2004
The total impulse, peak thrust, average thrust and burn time are
the same as the averaged static test data on the NAR web site in
the certification file. The curve drawn with these data points is as
close to the certification curve as can be with such a limited
number of points (32) allowed with wRASP up to v1.6.
</comments>
<data>
<eng-data cg="215." f="0." m="750." t="0."/>
<eng-data cg="215." f="229.13" m="748.659" t="0.023"/>
<eng-data cg="215." f="415.135" m="744.888" t="0.046"/>
<eng-data cg="215." f="485.264" m="741.909" t="0.059"/>
<eng-data cg="215." f="512.268" m="737.085" t="0.078"/>
<eng-data cg="215." f="525.67" m="729.689" t="0.106"/>
<eng-data cg="215." f="523.05" m="716.877" t="0.154"/>
<eng-data cg="215." f="528.39" m="701.625" t="0.211"/>
<eng-data cg="215." f="536.451" m="688.074" t="0.261"/>
<eng-data cg="215." f="560.734" m="657.917" t="0.369"/>
<eng-data cg="215." f="587.738" m="616.412" t="0.511"/>
<eng-data cg="215." f="603.86" m="572.136" t="0.657"/>
<eng-data cg="215." f="612.022" m="537.169" t="0.77"/>
<eng-data cg="215." f="625.75" m="434.474" t="1.096"/>
<eng-data cg="215." f="620.083" m="351.403" t="1.358"/>
<eng-data cg="215." f="612.022" m="267.052" t="1.627"/>
<eng-data cg="215." f="603.86" m="201.45" t="1.839"/>
<eng-data cg="215." f="590.459" m="135.188" t="2.057"/>
<eng-data cg="215." f="598.52" m="86.4699" t="2.218"/>
<eng-data cg="215." f="609.301" m="50.5051" t="2.335"/>
<eng-data cg="215." f="601.24" m="35.1009" t="2.385"/>
<eng-data cg="215." f="585.018" m="28.459" t="2.407"/>
<eng-data cg="215." f="533.831" m="23.0488" t="2.426"/>
<eng-data cg="215." f="385.511" m="13.4559" t="2.467"/>
<eng-data cg="215." f="283.037" m="6.65001" t="2.507"/>
<eng-data cg="215." f="164.441" m="2.66408" t="2.542"/>
<eng-data cg="215." f="67.399" m="0.657965" t="2.576"/>
<eng-data cg="215." f="29.653" m="0.188668" t="2.595"/>
<eng-data cg="215." f="0." m="0." t="2.62"/>
</data>
</engine>
</engine-list>
</engine-database>

28
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AMW_K570.eng
View File

@ -1,28 +0,0 @@
;
;Animal Motor Works K570 White Wolf
K570WW 54 492 0 0.9146 1.8151 AMW
0.020 364.42
0.030 664.79
0.051 751.47
0.071 745.81
0.096 705.25
0.137 674.93
0.284 661.38
0.528 651.24
0.913 644.51
1.192 651.24
1.430 651.24
1.649 651.24
1.872 644.51
2.176 624.23
2.318 600.64
2.394 597.33
2.455 546.63
2.501 485.89
2.562 421.84
2.597 340.83
2.638 266.54
2.734 175.48
2.836 97.86
2.927 47.24
3.040 0.00

42
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AMW_K570.rse
View File

@ -1,42 +0,0 @@
<engine-database>
<engine-list>
<engine FDiv="10" FFix="1" FStep="-1." Isp="189.27" Itot="1697.59" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="558.419" burn-time="3.04" cgDiv="10" cgFix="1" cgStep="-1." code="K570WW" delays="1000" dia="54." exitDia="0." initWt="1815.1" len="492." mDiv="10" mFix="1" mStep="-1." massFrac="50.39" mfg="Animal Motor Works" peakThrust="751.47" propWt="914.6" tDiv="10" tFix="1" tStep="-1." throatDia="0.">
<comments>AMW K570 RASP.ENG file made from NAR published data
File produced December 25, 2002
The total impulse, peak thrust, average thrust and burn time are
the same as the averaged static test data on the NAR web site in
the certification file. The curve drawn with these data points is as
close to the certification curve as can be with such a limited
number of points (32) allowed with wRASP up to v1.6.
</comments>
<data>
<eng-data cg="246." f="0." m="914.6" t="0."/>
<eng-data cg="246." f="364.42" m="912.637" t="0.02"/>
<eng-data cg="246." f="664.79" m="909.864" t="0.03"/>
<eng-data cg="246." f="751.47" m="901.852" t="0.051"/>
<eng-data cg="246." f="745.81" m="893.786" t="0.071"/>
<eng-data cg="246." f="705.25" m="884.013" t="0.096"/>
<eng-data cg="246." f="674.93" m="868.77" t="0.137"/>
<eng-data cg="246." f="661.38" m="815.853" t="0.284"/>
<eng-data cg="246." f="651.24" m="729.576" t="0.528"/>
<eng-data cg="246." f="644.51" m="595.191" t="0.913"/>
<eng-data cg="246." f="651.24" m="497.806" t="1.192"/>
<eng-data cg="246." f="651.24" m="414.301" t="1.43"/>
<eng-data cg="246." f="651.24" m="337.461" t="1.649"/>
<eng-data cg="246." f="644.51" m="259.623" t="1.872"/>
<eng-data cg="246." f="624.23" m="155.724" t="2.176"/>
<eng-data cg="246." f="600.64" m="108.87" t="2.318"/>
<eng-data cg="246." f="597.33" m="84.3437" t="2.394"/>
<eng-data cg="246." f="546.63" m="65.5458" t="2.455"/>
<eng-data cg="246." f="485.89" m="52.7513" t="2.501"/>
<eng-data cg="246." f="421.84" m="37.8353" t="2.562"/>
<eng-data cg="246." f="340.83" m="30.6445" t="2.597"/>
<eng-data cg="246." f="266.54" m="23.9364" t="2.638"/>
<eng-data cg="246." f="175.48" m="12.5055" t="2.734"/>
<eng-data cg="246." f="97.86" m="4.99493" t="2.836"/>
<eng-data cg="246." f="47.24" m="1.43799" t="2.927"/>
<eng-data cg="246." f="0." m="0." t="3.04"/>
</data>
</engine>
</engine-list>
</engine-database>

48
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AMW_K580.eng
View File

@ -1,48 +0,0 @@
;Created by Jesus Manuel Recuenco Andres 2011
;with Tctracer v1.0
K580 54.0 491.00 1000 0.89500 1.82300 Cesaroni
0.02 624.92
0.03 1076.60
0.07 846.73
0.12 884.56
0.20 855.46
0.29 840.91
0.39 835.09
0.48 822.58
0.56 808.60
0.66 800.62
0.74 784.64
0.83 776.66
0.90 762.68
0.96 760.68
1.03 748.71
1.10 734.32
1.14 713.24
1.18 720.75
1.27 704.78
1.35 682.82
1.43 666.85
1.51 650.87
1.59 632.91
1.67 622.92
1.73 604.95
1.79 598.96
1.86 579.00
1.94 561.03
1.99 559.03
2.03 539.07
2.09 533.08
2.16 517.11
2.24 507.12
2.31 491.15
2.39 477.18
2.45 463.20
2.51 442.28
2.55 407.36
2.60 360.81
2.65 320.07
2.69 276.42
2.76 232.78
2.82 194.95
2.96 122.21
3.20 0.00

40
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AMW_K600.eng
View File

@ -1,40 +0,0 @@
;
; Animal Motor Works K600 RASP.ENG file made from NAR data
; File produced August 22, 2002
; The total impulse, peak thrust, average thrust and burn time are
; the same as the averaged static test data on the NAR web site in
; the certification file. The curve drawn with these data points is as
; close to the certification curve as can be with such a limited
; number of points (32) allowed with wRASP up to v1.6.
K600 75 368 P 1.2233 2.9129 AMW
0.010 412.229
0.029 522.21
0.059 547.215
0.083 524.8
0.122 497.305
0.181 484.852
0.333 495.113
0.690 560.464
1.195 643.548
1.400 673.833
1.420 708.799
1.508 701.427
1.591 721.551
1.782 731.712
2.017 752.035
2.174 756.816
2.257 765.2
2.502 766.44
2.727 752.931
2.918 738.187
3.143 705.91
3.408 643.847
3.603 569.131
3.692 526.793
3.745 439.426
3.799 289.596
3.883 112.272
3.922 64.862
3.971 37.437
3.995 22.474
4.070 0

48
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AMW_K600.rse
View File

@ -1,48 +0,0 @@
<engine-database>
<engine-list>
<engine FDiv="10" FFix="1" FStep="-1." Isp="208.34" Itot="2499.34" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="614.088" burn-time="4.07" cgDiv="10" cgFix="1" cgStep="-1." code="K600WW" delays="1000" dia="75." exitDia="0." initWt="2912.9" len="368." mDiv="10" mFix="1" mStep="-1." massFrac="42." mfg="Animal Motor Works" peakThrust="766.44" propWt="1223.3" tDiv="10" tFix="1" tStep="-1." throatDia="0.">
<comments>Animal Motor Works K600 RASP.ENG file made from NAR data
File produced August 22, 2002
The total impulse, peak thrust, average thrust and burn time are
the same as the averaged static test data on the NAR web site in
the certification file. The curve drawn with these data points is as
close to the certification curve as can be with such a limited
number of points (32) allowed with wRASP up to v1.6.
</comments>
<data>
<eng-data cg="184." f="0." m="1223.3" t="0."/>
<eng-data cg="184." f="412.229" m="1222.29" t="0.01"/>
<eng-data cg="184." f="522.21" m="1217.95" t="0.029"/>
<eng-data cg="184." f="547.215" m="1210.09" t="0.059"/>
<eng-data cg="184." f="524.8" m="1203.8" t="0.083"/>
<eng-data cg="184." f="497.305" m="1194.04" t="0.122"/>
<eng-data cg="184." f="484.852" m="1179.86" t="0.181"/>
<eng-data cg="184." f="495.113" m="1143.41" t="0.333"/>
<eng-data cg="184." f="560.464" m="1051.19" t="0.69"/>
<eng-data cg="184." f="643.548" m="902.388" t="1.195"/>
<eng-data cg="184." f="673.833" m="836.297" t="1.4"/>
<eng-data cg="184." f="708.799" m="829.53" t="1.42"/>
<eng-data cg="184." f="701.427" m="799.159" t="1.508"/>
<eng-data cg="184." f="721.551" m="770.256" t="1.591"/>
<eng-data cg="184." f="731.712" m="702.327" t="1.782"/>
<eng-data cg="184." f="752.035" m="616.996" t="2.017"/>
<eng-data cg="184." f="756.816" m="559.023" t="2.174"/>
<eng-data cg="184." f="765.2" m="528.108" t="2.257"/>
<eng-data cg="184." f="766.44" m="436.274" t="2.502"/>
<eng-data cg="184." f="752.931" m="352.613" t="2.727"/>
<eng-data cg="184." f="738.187" m="282.915" t="2.918"/>
<eng-data cg="184." f="705.91" m="203.398" t="3.143"/>
<eng-data cg="184." f="643.847" m="115.864" t="3.408"/>
<eng-data cg="184." f="569.131" m="57.979" t="3.603"/>
<eng-data cg="184." f="526.793" m="34.1092" t="3.692"/>
<eng-data cg="184." f="439.426" m="21.577" t="3.745"/>
<eng-data cg="184." f="289.596" m="11.9429" t="3.799"/>
<eng-data cg="184." f="112.272" m="3.68171" t="3.883"/>
<eng-data cg="184." f="64.862" m="1.9911" t="3.922"/>
<eng-data cg="184." f="37.437" m="0.764376" t="3.971"/>
<eng-data cg="184." f="22.474" m="0.412496" t="3.995"/>
<eng-data cg="184." f="0." m="0." t="4.07"/>
</data>
</engine>
</engine-list>
</engine-database>

34
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AMW_K600_1.eng
View File

@ -1,34 +0,0 @@
;
;Animal Motor Works K600 White Wolf
K600WW 75 368 0 1.2233 2.9129 AMW
0.010 412.229
0.029 522.21
0.059 547.215
0.083 524.8
0.122 497.305
0.181 484.852
0.333 495.113
0.690 560.464
1.195 643.548
1.400 673.833
1.420 708.799
1.508 701.427
1.591 721.551
1.782 731.712
2.017 752.035
2.174 756.816
2.257 765.2
2.502 766.44
2.727 752.931
2.918 738.187
3.143 705.91
3.408 643.847
3.603 569.131
3.692 526.793
3.745 439.426
3.799 289.596
3.883 112.272
3.922 64.862
3.971 37.437
3.995 22.474
4.070 0

31
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AMW_K605.eng
View File

@ -1,31 +0,0 @@
;
;AMW K605 RASP.ENG file made from NAR published data
;File produced April 19, 2004
;The total impulse, peak thrust, average thrust and burn time are
;the same as the averaged static test data on the NAR web site in
;the certification file. The curve drawn with these data points is as
;close to the certification curve as can be with such a limited
;number of points (32) allowed with wRASP up to v1.6.
K605RR 75 368 100 1.231 2.7688 Animal_Motor_Works
0.03 165.845
0.053 309.12
0.077 361.916
0.142 392.042
0.527 501.412
0.988 606.905
1.515 682.37
2.101 730.593
2.355 737.58
2.692 731.289
3 712.497
3.361 671.036
3.503 663.479
3.586 659.701
3.645 633.353
3.692 573
3.734 444.838
3.775 297.785
3.828 162.066
3.864 98.015
3.905 41.471
3.95 0

39
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AMW_K605.rse
View File

@ -1,39 +0,0 @@
<engine-database>
<engine-list>
<engine FDiv="10" FFix="1" FStep="-1." Isp="198.9" Itot="2401.13" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="607.882" burn-time="3.95" cgDiv="10" cgFix="1" cgStep="-1." code="K605RR" delays="1000" dia="75." exitDia="0." initWt="2768.8" len="368." mDiv="10" mFix="1" mStep="-1." massFrac="44.46" mfg="Animal Motor Works" peakThrust="737.58" propWt="1231." tDiv="10" tFix="1" tStep="-1." throatDia="0.">
<comments>AMW K605 RASP.ENG file made from NAR published data
File produced April 19, 2004
The total impulse, peak thrust, average thrust and burn time are
the same as the averaged static test data on the NAR web site in
the certification file. The curve drawn with these data points is as
close to the certification curve as can be with such a limited
number of points (32) allowed with wRASP up to v1.6.
</comments>
<data>
<eng-data cg="184." f="0." m="1231." t="0."/>
<eng-data cg="184." f="165.845" m="1229.72" t="0.03"/>
<eng-data cg="184." f="309.12" m="1226.92" t="0.053"/>
<eng-data cg="184." f="361.916" m="1222.8" t="0.077"/>
<eng-data cg="184." f="392.042" m="1210.23" t="0.142"/>
<eng-data cg="184." f="501.412" m="1122.06" t="0.527"/>
<eng-data cg="184." f="606.905" m="991.087" t="0.988"/>
<eng-data cg="184." f="682.37" m="816.92" t="1.515"/>
<eng-data cg="184." f="730.593" m="604.673" t="2.101"/>
<eng-data cg="184." f="737.58" m="509.081" t="2.355"/>
<eng-data cg="184." f="731.289" m="382.192" t="2.692"/>
<eng-data cg="184." f="712.497" m="268.202" t="3."/>
<eng-data cg="184." f="671.036" m="140.173" t="3.361"/>
<eng-data cg="184." f="663.479" m="91.5969" t="3.503"/>
<eng-data cg="184." f="659.701" m="63.4449" t="3.586"/>
<eng-data cg="184." f="633.353" m="43.8889" t="3.645"/>
<eng-data cg="184." f="573." m="29.3549" t="3.692"/>
<eng-data cg="184." f="444.838" m="18.3967" t="3.734"/>
<eng-data cg="184." f="297.785" m="10.5919" t="3.775"/>
<eng-data cg="184." f="162.066" m="4.34441" t="3.828"/>
<eng-data cg="184." f="98.015" m="1.94435" t="3.864"/>
<eng-data cg="184." f="41.471" m="0.478375" t="3.905"/>
<eng-data cg="184." f="0." m="0." t="3.95"/>
</data>
</engine>
</engine-list>
</engine-database>

21
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AMW_K610.eng
View File

@ -1,21 +0,0 @@
; Skidmark
K610-SK 54 491 0 0.866 1.765 AMW/ProX
0.01 300
0.02 745
0.035 650
0.06 560
0.12 635
0.21 670
0.4 695
0.7 700
1 690
1.35 665
1.7 630
2.05 585
2.19 590
2.24 500
2.3 350
2.4 205
2.5 60
2.6 15
2.7 0

33
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AMW_K610.rse
View File

@ -1,33 +0,0 @@
<engine-database>
<engine-list>
<engine mfg="AMW-ProX" code="K610-SK" Type="unspecified" dia="54." len="491."
initWt="1765." propWt="866." delays="0" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="567.106" peakThrust="745." throatDia="0." exitDia="0." Itot="1531.19"
burn-time="2.7" massFrac="49.07" Isp="180.3" tDiv="10" tStep="-1." tFix="1"
FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10"
cgStep="-1." cgFix="1">
<data>
<eng-data t="0." f="0." m="866." cg="245.5"/>
<eng-data t="0.01" f="300." m="865.152" cg="245.5"/>
<eng-data t="0.02" f="745." m="862.197" cg="245.5"/>
<eng-data t="0.035" f="650." m="856.279" cg="245.5"/>
<eng-data t="0.06" f="560." m="847.725" cg="245.5"/>
<eng-data t="0.12" f="635." m="827.449" cg="245.5"/>
<eng-data t="0.21" f="670." m="794.236" cg="245.5"/>
<eng-data t="0.4" f="695." m="720.895" cg="245.5"/>
<eng-data t="0.7" f="700." m="602.549" cg="245.5"/>
<eng-data t="1." f="690." m="484.626" cg="245.5"/>
<eng-data t="1.35" f="665." m="350.515" cg="245.5"/>
<eng-data t="1.7" f="630." m="222.341" cg="245.5"/>
<eng-data t="2.05" f="585." m="102.086" cg="245.5"/>
<eng-data t="2.19" f="590." m="55.5677" cg="245.5"/>
<eng-data t="2.24" f="500." m="40.1558" cg="245.5"/>
<eng-data t="2.3" f="350." m="25.7336" cg="245.5"/>
<eng-data t="2.4" f="205." m="10.0389" cg="245.5"/>
<eng-data t="2.5" f="60." m="2.54508" cg="245.5"/>
<eng-data t="2.6" f="15." m="0.424181" cg="245.5"/>
<eng-data t="2.7" f="0." m="0." cg="245.5"/>
</data>
</engine>
</engine-list>
</engine-database>

38
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AMW_K650.eng
View File

@ -1,38 +0,0 @@
; Animal Motor Works 54-1750
; AMW K650RR RASP.ENG file made from NAR published data
; File produced April 19, 2004
; This file my be used or given away. All I ask is that this header
; is maintained to give credit to NAR S&T. Thank you, Jack Kane
; The total impulse, peak thrust, average thrust and burn time are
; the same as the averaged static test data on the NAR web site in
; the certification file. The curve drawn with these data points is as
; close to the certification curve as can be with such a limited
; number of points (32) allowed with wRASP up to v1.6.
K650RR 54 492 0 0.931 1.8087 AMW
0.022 308.257
0.045 566.480
0.058 620.440
0.081 639.668
0.135 639.668
0.229 643.494
0.351 662.823
0.594 701.380
0.810 724.434
0.999 743.763
1.151 751.220
1.381 747.588
1.610 736.001
1.835 709.031
2.073 685.876
2.244 674.400
2.334 682.051
2.429 685.876
2.469 666.648
2.528 597.285
2.573 481.714
2.609 358.391
2.631 250.471
2.681 146.477
2.721 65.507
2.748 23.124
2.770 0.000

44
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AMW_K650.rse
View File

@ -1,44 +0,0 @@
<engine-database>
<engine-list>
<engine FDiv="10" FFix="1" FStep="-1." Isp="199.5" Itot="1821.46" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="657.565" burn-time="2.77" cgDiv="10" cgFix="1" cgStep="-1." code="K650RR" delays="1000" dia="54." exitDia="0." initWt="1808.7" len="492." mDiv="10" mFix="1" mStep="-1." massFrac="51.47" mfg="Animal Motor Works" peakThrust="751.22" propWt="931." tDiv="10" tFix="1" tStep="-1." throatDia="0.">
<comments>AMW K650 RASP.ENG file made from NAR published data
File produced April 19, 2004
The total impulse, peak thrust, average thrust and burn time are
the same as the averaged static test data on the NAR web site in
the certification file. The curve drawn with these data points is as
close to the certification curve as can be with such a limited
number of points (32) allowed with wRASP up to v1.6.
</comments>
<data>
<eng-data cg="246." f="0." m="931." t="0."/>
<eng-data cg="246." f="308.257" m="929.267" t="0.022"/>
<eng-data cg="246." f="566.48" m="924.125" t="0.045"/>
<eng-data cg="246." f="620.44" m="920.182" t="0.058"/>
<eng-data cg="246." f="639.668" m="912.775" t="0.081"/>
<eng-data cg="246." f="639.668" m="895.119" t="0.135"/>
<eng-data cg="246." f="643.494" m="864.294" t="0.229"/>
<eng-data cg="246." f="662.823" m="823.564" t="0.351"/>
<eng-data cg="246." f="701.38" m="738.844" t="0.594"/>
<eng-data cg="246." f="724.434" m="660.137" t="0.81"/>
<eng-data cg="246." f="743.763" m="589.22" t="0.999"/>
<eng-data cg="246." f="751.22" m="531.146" t="1.151"/>
<eng-data cg="246." f="747.588" m="443.047" t="1.381"/>
<eng-data cg="246." f="736.001" m="356.22" t="1.61"/>
<eng-data cg="246." f="709.031" m="273.128" t="1.835"/>
<eng-data cg="246." f="685.876" m="188.284" t="2.073"/>
<eng-data cg="246." f="674.4" m="128.838" t="2.244"/>
<eng-data cg="246." f="682.051" m="97.6381" t="2.334"/>
<eng-data cg="246." f="685.876" m="64.4266" t="2.429"/>
<eng-data cg="246." f="666.648" m="50.6004" t="2.469"/>
<eng-data cg="246." f="597.285" m="31.5424" t="2.528"/>
<eng-data cg="246." f="481.714" m="19.1334" t="2.573"/>
<eng-data cg="246." f="358.391" m="11.4042" t="2.609"/>
<eng-data cg="246." f="250.471" m="7.98091" t="2.631"/>
<eng-data cg="246." f="146.477" m="2.90861" t="2.681"/>
<eng-data cg="246." f="65.507" m="0.741589" t="2.721"/>
<eng-data cg="246." f="23.124" m="0.130013" t="2.748"/>
<eng-data cg="246." f="0." m="0." t="2.77"/>
</data>
</engine>
</engine-list>
</engine-database>

58
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AMW_K665.rse
View File

@ -1,58 +0,0 @@
<engine-database>
<engine-list>
<engine mfg="Cesaroni Technology Inc." code="K665BB" Type="reloadable" dia="54."
len="403." initWt="1737." propWt="964." delays="1000" auto-calc-mass="1"
auto-calc-cg="1" avgThrust="661.106" peakThrust="819.841" throatDia="0."
exitDia="0." Itot="1352.62" burn-time="2.05" massFrac="55.5" Isp="143.08"
tDiv="10" tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10"
mStep="-1." mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<comments>Entered by Tim Van Milligan for RockSim users. Used ThrustCurve Tracer by John
Coker. Data from CAR web site, thrust curve from AMW web site.
</comments>
<data>
<eng-data t="0." f="0." m="964." cg="201.5"/>
<eng-data t="0.011" f="429.766" m="962.315" cg="201.5"/>
<eng-data t="0.036" f="591.271" m="953.219" cg="201.5"/>
<eng-data t="0.042" f="620.013" m="950.63" cg="201.5"/>
<eng-data t="0.063" f="636.438" m="941.227" cg="201.5"/>
<eng-data t="0.076" f="636.438" m="935.331" cg="201.5"/>
<eng-data t="0.097" f="624.119" m="925.898" cg="201.5"/>
<eng-data t="0.109" f="624.119" m="920.56" cg="201.5"/>
<eng-data t="0.137" f="635.069" m="907.996" cg="201.5"/>
<eng-data t="0.21" f="658.337" m="874.351" cg="201.5"/>
<eng-data t="0.341" f="695.291" m="811.162" cg="201.5"/>
<eng-data t="0.413" f="724.033" m="774.746" cg="201.5"/>
<eng-data t="0.497" f="740.458" m="730.91" cg="201.5"/>
<eng-data t="0.714" f="781.518" m="613.22" cg="201.5"/>
<eng-data t="0.825" f="803.417" m="550.529" cg="201.5"/>
<eng-data t="0.937" f="810.26" m="486.127" cg="201.5"/>
<eng-data t="0.972" f="818.472" m="465.813" cg="201.5"/>
<eng-data t="1.029" f="819.841" m="432.536" cg="201.5"/>
<eng-data t="1.101" f="817.104" m="390.537" cg="201.5"/>
<eng-data t="1.16" f="808.892" m="356.352" cg="201.5"/>
<eng-data t="1.273" f="773.306" m="292.642" cg="201.5"/>
<eng-data t="1.337" f="755.513" m="257.775" cg="201.5"/>
<eng-data t="1.396" f="729.508" m="226.554" cg="201.5"/>
<eng-data t="1.469" f="689.816" m="189.633" cg="201.5"/>
<eng-data t="1.551" f="636.438" m="150.879" cg="201.5"/>
<eng-data t="1.625" f="589.902" m="118.541" cg="201.5"/>
<eng-data t="1.694" f="548.842" m="90.5419" cg="201.5"/>
<eng-data t="1.745" f="521.468" m="71.0905" cg="201.5"/>
<eng-data t="1.77" f="509.15" m="61.9091" cg="201.5"/>
<eng-data t="1.791" f="509.15" m="54.289" cg="201.5"/>
<eng-data t="1.806" f="506.413" m="48.8606" cg="201.5"/>
<eng-data t="1.829" f="494.095" m="40.6605" cg="201.5"/>
<eng-data t="1.863" f="446.191" m="29.2683" cg="201.5"/>
<eng-data t="1.89" f="396.918" m="21.1565" cg="201.5"/>
<eng-data t="1.913" f="342.171" m="15.0989" cg="201.5"/>
<eng-data t="1.928" f="290.161" m="11.719" cg="201.5"/>
<eng-data t="1.947" f="231.307" m="8.18839" cg="201.5"/>
<eng-data t="1.972" f="164.242" m="4.66459" cg="201.5"/>
<eng-data t="1.985" f="131.394" m="3.29507" cg="201.5"/>
<eng-data t="2.006" f="95.808" m="1.59486" cg="201.5"/>
<eng-data t="2.027" f="61.591" m="0.417005" cg="201.5"/>
<eng-data t="2.046" f="0." m="0." cg="201.5"/>
</data>
</engine>
</engine-list>
</engine-database>

34
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AMW_K670.eng
View File

@ -1,34 +0,0 @@
;
; AMW K670 RASP.ENG file made from NAR published data
; File produced SEPT 4, 2002
; The total impulse, peak thrust, average thrust and burn time are
; the same as the averaged static test data on the NAR web site in
; the certification file. The curve drawn with these data points is as
; close to the certification curve as can be with such a limited
; number of points (32) allowed with wRASP up to v1.6.
K670 54 492 P- 1.0140 1.9145 AMW
0.016 294.05
0.035 398.577
0.086 506.292
0.153 496.428
0.264 506.093
0.461 558.108
0.722 629.553
0.983 688.044
1.116 714.051
1.193 785.795
1.409 788.784
1.737 804.56
2.074 781.41
2.195 764.87
2.226 781.211
2.277 764.77
2.398 751.517
2.440 744.941
2.468 718.834
2.484 666.521
2.525 418.107
2.551 218.818
2.573 120.768
2.595 52.143
2.620 0

87
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AMW_K670.rse
View File

@ -1,87 +0,0 @@
<engine-database>
<engine-list>
<engine mfg="Cesaroni Technology Inc." code="K671RR" Type="reloadable" dia="54."
len="491." initWt="1885." propWt="955." delays="1000" auto-calc-mass="1"
auto-calc-cg="1" avgThrust="681.307" peakThrust="825.096" throatDia="0."
exitDia="0." Itot="1802.06" burn-time="2.65" massFrac="50.66" Isp="192.42"
tDiv="10" tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10"
mStep="-1." mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<comments>Entered by Tim Van Milligan for RockSim users. Used ThrustCurve Tracer by John
Coker. Data from CAR web site, thrust curve from AMW web site.
</comments>
<data>
<eng-data t="0." f="0." m="955." cg="245.5"/>
<eng-data t="0.033" f="610.402" m="949.663" cg="245.5"/>
<eng-data t="0.052" f="752.128" m="942.803" cg="245.5"/>
<eng-data t="0.06" f="775.983" m="939.564" cg="245.5"/>
<eng-data t="0.076" f="785.805" m="932.942" cg="245.5"/>
<eng-data t="0.098" f="813.87" m="923.617" cg="245.5"/>
<eng-data t="0.109" f="822.289" m="918.848" cg="245.5"/>
<eng-data t="0.133" f="818.08" m="908.416" cg="245.5"/>
<eng-data t="0.166" f="825.096" m="894.048" cg="245.5"/>
<eng-data t="0.185" f="820.886" m="885.761" cg="245.5"/>
<eng-data t="0.21" f="813.87" m="874.932" cg="245.5"/>
<eng-data t="0.226" f="825.096" m="867.984" cg="245.5"/>
<eng-data t="0.253" f="818.08" m="856.228" cg="245.5"/>
<eng-data t="0.286" f="820.886" m="841.896" cg="245.5"/>
<eng-data t="0.321" f="818.08" m="826.696" cg="245.5"/>
<eng-data t="0.457" f="809.66" m="768.038" cg="245.5"/>
<eng-data t="0.593" f="805.451" m="709.835" cg="245.5"/>
<eng-data t="0.688" f="802.644" m="669.355" cg="245.5"/>
<eng-data t="0.729" f="791.418" m="652.037" cg="245.5"/>
<eng-data t="0.803" f="792.822" m="620.973" cg="245.5"/>
<eng-data t="0.86" f="780.193" m="597.215" cg="245.5"/>
<eng-data t="0.925" f="778.789" m="570.364" cg="245.5"/>
<eng-data t="0.988" f="770.37" m="544.503" cg="245.5"/>
<eng-data t="1.061" f="760.547" m="514.89" cg="245.5"/>
<eng-data t="1.116" f="759.144" m="492.743" cg="245.5"/>
<eng-data t="1.176" f="752.128" m="468.716" cg="245.5"/>
<eng-data t="1.271" f="735.289" m="431.274" cg="245.5"/>
<eng-data t="1.309" f="738.096" m="416.438" cg="245.5"/>
<eng-data t="1.344" f="735.289" m="402.774" cg="245.5"/>
<eng-data t="1.363" f="731.08" m="395.392" cg="245.5"/>
<eng-data t="1.41" f="735.289" m="377.13" cg="245.5"/>
<eng-data t="1.448" f="735.289" m="362.322" cg="245.5"/>
<eng-data t="1.494" f="731.08" m="344.449" cg="245.5"/>
<eng-data t="1.524" f="735.289" m="332.792" cg="245.5"/>
<eng-data t="1.557" f="731.08" m="319.97" cg="245.5"/>
<eng-data t="1.616" f="721.257" m="297.265" cg="245.5"/>
<eng-data t="1.654" f="714.241" m="282.811" cg="245.5"/>
<eng-data t="1.682" f="721.257" m="272.161" cg="245.5"/>
<eng-data t="1.728" f="705.822" m="254.766" cg="245.5"/>
<eng-data t="1.766" f="705.822" m="240.552" cg="245.5"/>
<eng-data t="1.799" f="705.822" m="228.209" cg="245.5"/>
<eng-data t="1.826" f="698.806" m="218.159" cg="245.5"/>
<eng-data t="1.856" f="690.386" m="207.116" cg="245.5"/>
<eng-data t="1.889" f="687.58" m="195.067" cg="245.5"/>
<eng-data t="1.921" f="688.983" m="183.395" cg="245.5"/>
<eng-data t="1.946" f="684.773" m="174.295" cg="245.5"/>
<eng-data t="1.976" f="684.773" m="163.408" cg="245.5"/>
<eng-data t="2." f="674.951" m="154.761" cg="245.5"/>
<eng-data t="2.014" f="681.967" m="149.727" cg="245.5"/>
<eng-data t="2.049" f="669.338" m="137.195" cg="245.5"/>
<eng-data t="2.063" f="659.515" m="132.265" cg="245.5"/>
<eng-data t="2.106" f="649.693" m="117.348" cg="245.5"/>
<eng-data t="2.136" f="651.096" m="107.008" cg="245.5"/>
<eng-data t="2.163" f="655.306" m="97.6617" cg="245.5"/>
<eng-data t="2.177" f="648.289" m="92.8258" cg="245.5"/>
<eng-data t="2.199" f="651.096" m="85.2511" cg="245.5"/>
<eng-data t="2.212" f="646.886" m="80.78" cg="245.5"/>
<eng-data t="2.22" f="638.467" m="78.0553" cg="245.5"/>
<eng-data t="2.248" f="617.419" m="68.7375" cg="245.5"/>
<eng-data t="2.267" f="600.58" m="62.6054" cg="245.5"/>
<eng-data t="2.283" f="599.177" m="57.5189" cg="245.5"/>
<eng-data t="2.316" f="568.306" m="47.3103" cg="245.5"/>
<eng-data t="2.359" f="516.386" m="34.9514" cg="245.5"/>
<eng-data t="2.384" f="464.467" m="28.4538" cg="245.5"/>
<eng-data t="2.4" f="425.177" m="24.6821" cg="245.5"/>
<eng-data t="2.444" f="326.951" m="15.9131" cg="245.5"/>
<eng-data t="2.474" f="259.596" m="11.2505" cg="245.5"/>
<eng-data t="2.52" f="171.193" m="5.99967" cg="245.5"/>
<eng-data t="2.563" f="112.258" m="2.77005" cg="245.5"/>
<eng-data t="2.61" f="63.145" m="0.585615" cg="245.5"/>
<eng-data t="2.645" f="0." m="0." cg="245.5"/>
</data>
</engine>
</engine-list>
</engine-database>

28
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AMW_K670_1.eng
View File

@ -1,28 +0,0 @@
;
;Animal Motor Works K670 Green Gorilla
K670GG 54 492 0 1.0140 1.9145 AMW
0.016 294.05
0.035 398.577
0.086 506.292
0.153 496.428
0.264 506.093
0.461 558.108
0.722 629.553
0.983 688.044
1.116 714.051
1.193 785.795
1.409 788.784
1.737 804.56
2.074 781.41
2.195 764.87
2.226 781.211
2.277 764.77
2.398 751.517
2.440 744.941
2.468 718.834
2.484 666.521
2.525 418.107
2.551 218.818
2.573 120.768
2.595 52.143
2.620 0

42
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AMW_K670_1.rse
View File

@ -1,42 +0,0 @@
<engine-database>
<engine-list>
<engine FDiv="10" FFix="1" FStep="-1." Isp="176.09" Itot="1751.06" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="668.342" burn-time="2.62" cgDiv="10" cgFix="1" cgStep="-1." code="K670GG" delays="1000" dia="54." exitDia="0." initWt="1914.5" len="492." mDiv="10" mFix="1" mStep="-1." massFrac="52.96" mfg="Animal Motor Works" peakThrust="804.56" propWt="1014." tDiv="10" tFix="1" tStep="-1." throatDia="0.">
<comments>AMW K670 RASP.ENG file made from NAR published data
File produced SEPT 4, 2002
The total impulse, peak thrust, average thrust and burn time are
the same as the averaged static test data on the NAR web site in
the certification file. The curve drawn with these data points is as
close to the certification curve as can be with such a limited
number of points (32) allowed with wRASP up to v1.6.
</comments>
<data>
<eng-data cg="246." f="0." m="1014." t="0."/>
<eng-data cg="246." f="294.05" m="1012.64" t="0.016"/>
<eng-data cg="246." f="398.577" m="1008.83" t="0.035"/>
<eng-data cg="246." f="506.292" m="995.466" t="0.086"/>
<eng-data cg="246." f="496.428" m="976.014" t="0.153"/>
<eng-data cg="246." f="506.093" m="943.794" t="0.264"/>
<eng-data cg="246." f="558.108" m="883.093" t="0.461"/>
<eng-data cg="246." f="629.553" m="793.341" t="0.722"/>
<eng-data cg="246." f="688.044" m="693.771" t="0.983"/>
<eng-data cg="246." f="714.051" m="639.778" t="1.116"/>
<eng-data cg="246." f="785.795" m="606.34" t="1.193"/>
<eng-data cg="246." f="788.784" m="507.865" t="1.409"/>
<eng-data cg="246." f="804.56" m="356.547" t="1.737"/>
<eng-data cg="246." f="781.41" m="201.796" t="2.074"/>
<eng-data cg="246." f="764.87" m="147.623" t="2.195"/>
<eng-data cg="246." f="781.211" m="133.746" t="2.226"/>
<eng-data cg="246." f="764.77" m="110.917" t="2.277"/>
<eng-data cg="246." f="751.517" m="57.7952" t="2.398"/>
<eng-data cg="246." f="744.941" m="39.5973" t="2.44"/>
<eng-data cg="246." f="718.834" m="27.7303" t="2.468"/>
<eng-data cg="246." f="666.521" m="21.3125" t="2.484"/>
<eng-data cg="246." f="418.107" m="8.43676" t="2.525"/>
<eng-data cg="246." f="218.818" m="3.64197" t="2.551"/>
<eng-data cg="246." f="120.768" m="1.47886" t="2.573"/>
<eng-data cg="246." f="52.143" m="0.377436" t="2.595"/>
<eng-data cg="246." f="0." m="0." t="2.62"/>
</data>
</engine>
</engine-list>
</engine-database>

36
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AMW_K700.eng
View File

@ -1,36 +0,0 @@
;
;AMW K700 RASP.ENG file made from NAR published data
;File produced April 19, 2004
;The total impulse, peak thrust, average thrust and burn time are
;the same as the averaged static test data on the NAR web site in
;the certification file. The curve drawn with these data points is as
;close to the certification curve as can be with such a limited
;number of points (32) allowed with wRASP up to v1.6.
K700BB 54 430 100 0.754 1.4831 Animal_Motor_Works
0.014 359.559
0.022 625.425
0.03 737.756
0.047 771.505
0.082 786.516
0.106 771.505
0.144 775.233
0.272 786.516
0.477 812.71
0.693 842.632
0.97 847.06
1.283 838.904
1.516 816.438
1.706 801.427
1.779 793.972
1.811 775.233
1.841 726.573
1.873 625.425
1.909 509.367
1.95 393.208
1.982 337.093
2.035 292.16
2.073 228.489
2.111 153.535
2.155 86.137
2.193 37.446
2.24 0

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