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Merge remote-tracking branch 'upstream/master' into feature/simulationextensions

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Conflicts:
	core/src/net/sf/openrocket/simulation/SimulationStatus.java
This commit is contained in:
Sampo Niskanen 2014-12-23 21:01:48 +02:00
commit 82af205e3e
214 changed files with 10337 additions and 3325 deletions
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core/.releasing.txt.swp Normal file
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core/ChangeLog
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2014-11-02 Kevin Ruland
* Released version 14.11 See Release Notes for changes.
2014-06-26 Kevin Ruland
* Released version 14.06 See Release Notes for changes.
2014-05-21 Kevin Ruland
* Released version 14.05 See Release Notes for changes.
2013-11-07 Kevin Ruland
* Released version 13.11

32
core/ReleaseNotes
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OpenRocket 14.11 (2014-11-02):
------------------------------
New Features:
* Updated thrustcurves
Bug Fixes:
* Fixed a couple of bugs.
OpenRocket 14.06 (2014-06-25):
------------------------------
New Features:
* Klima motor textures
* Added knots to windspeed and velocity units
* Updated thrustcurves
Bug Fixes:
* Fixed annoying IndexOutOfBounds bug in tables.
OpenRocket 14.05 (2014-05-21):
------------------------------
New Features:
* Compute optimimum delay time when simulating
* Display cg/mass overrides using icons in the component tree
Bug Fixes:
* Bug fixes in the motor selection dialog
* Updated thrustcurves
* Updated 3d libraries to 2.1.5
OpenRocket 14.03 (2014-03-20):
------------------------------

27
core/resources-src/datafiles/thrustcurves/manual/Cesaroni_F31.rse Normal file
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<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>

13
core/resources-src/datafiles/thrustcurves/manual/Klima_A6.eng Normal file
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; Raketenmodellbau Klima GmbH
; Official manufacturer thrust data - A6
; Created by Leo Nutz for OpenRocket,
; released into the Public Domain (3/2014)
A6 18 70 4 0.0035 0.0145 Klima
0.088 0.502
0.186 4.601
0.232 7.089
0.314 10.477
0.418 6.713
0.467 3.011
0.501 0.418
0.71 0.0

27
core/resources-src/datafiles/thrustcurves/manual/Klima_B4.eng Normal file
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; Raketenmodellbau Klima GmbH
; Official manufacturer thrust data - B4
; Created by Leo Nutz for OpenRocket,
; released into the Public Domain (3/2014)
B4 18 70 0-4 0.0054 0.0163 Klima
0.049 0.83
0.096 1.745
0.157 2.946
0.209 3.89
0.273 4.977
0.335 6.093
0.380 7.122
0.411 8.001
0.436 7.065
0.465 6.236
0.516 5.063
0.564 4.462
0.607 4.205
0.669 4.09
0.90 4.09
0.966 3.976
1.025 3.719
1.084 3.261
1.145 2.546
1.212 1.745
1.295 0.772
1.364 0.0

24
core/resources-src/datafiles/thrustcurves/manual/Klima_C2.eng Normal file
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; Raketenmodellbau Klima GmbH
; Official manufacturer thrust data - C2
; Created by Leo Nutz for OpenRocket,
; released into the Public Domain (3/2014)
C2 18 70 0-P 0.0113 0.0224 Klima
0.04 0.229
0.12 0.658
0.211 1.144
0.291 1.831
0.385 2.86
0.447 3.833
0.505 5.001
0.567 3.89
0.615 3.146
0.665 2.66
0.735 2.203
0.815 2.088
0.93 1.98
4.589 1.96
4.729 1.888
4.815 1.602
4.873 1.259
4.969 0.658
5.083 0.0

21
core/resources-src/datafiles/thrustcurves/manual/Klima_C6.eng Normal file
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; Raketenmodellbau Klima GmbH
; Official manufacturer thrust data - C6
; Created by Leo Nutz for OpenRocket,
; released into the Public Domain (3/2014)
C6 18 70 0-3-5-7-P 0.0096 0.0205 Klima
0.046 0.953
0.168 5.259
0.235 10.023
0.291 15.00
0.418 9.87
0.505 7.546
0.582 6.631
0.679 6.136
0.786 5.716
1.26 5.678
1.357 5.488
1.423 4.992
1.469 4.116
1.618 1.22
1.701 0.0

28
core/resources-src/datafiles/thrustcurves/manual/Klima_D3.eng Normal file
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; Raketenmodellbau Klima GmbH
; Official manufacturer thrust data - D3
; Created by Leo Nutz for OpenRocket,
; released into the Public Domain (3/2014)
D3 18 70 0-P 0.017 0.0279 Klima
0.073 0.229
0.178 0.686
0.251 1.287
0.313 2.203
0.375 3.633
0.425 5.006
0.473 6.465
0.556 8.181
0.603 9.01
0.655 6.922
0.698 5.463
0.782 4.291
0.873 3.576
1.024 3.146
1.176 2.946
5.282 2.918
5.491 2.832
5.59 2.517
5.782 1.859
5.924 1.287
6.061 0.715
6.17 0.286
6.26 0.0

20
core/resources-src/datafiles/thrustcurves/manual/Klima_D9.eng Normal file
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; Raketenmodellbau Klima GmbH
; Official manufacturer thrust data - D9
; Created by Leo Nutz for OpenRocket,
; released into the Public Domain (3/2014)
D9 18 70 0-3-5-7-P 0.0161 0.0271 Klima
0.04 2.111
0.116 9.685
0.213 25.0
0.286 15.738
0.329 12.472
0.369 10.67
0.42 9.713
0.495 9.178
0.597 8.896
1.711 8.925
1.826 8.699
1.917 8.052
1.975 6.954
2.206 1.07
2.242 0.0

5
core/resources-src/datafiles/thrustcurves/manual/README.txt
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@ -5,7 +5,8 @@ All other thrust curves are from www.thrustcurve.org
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
at130702.eng - preliminary thrustcurve for new AT C3
at130721.eng - preliminary thrustcurve for new AT D2
CTI F31 - Correct diameter to 29mm

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core/resources-src/datafiles/thrustcurves/manual/at130702.eng
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; @File: at130702.asc, @Pts-I: 130, @Pts-O: 31, @Sm: 0, @CO: 5%
; @TI: 8.95946, @TIa: 8.94558, @TIe: +0.07%, @ThMax: 8.26822, @ThAvg: 3.00451, @Tb: 2.982
; Exported using ThrustCurveTool, www.ThrustGear.com
C3 18 70 P 0.0052 0.0211 AT
0.024 0.121145
0.048 2.25634
0.072 6.61759
0.096 7.48075
0.12 8.11675
0.168 8.26822
0.288 7.61706
0.336 7.25359
0.36 6.84475
0.528 5.58781
0.6 5.17897
0.696 4.24012
0.72 4.11897
0.792 3.2255
0.864 2.57434
0.912 2.33203
1.176 2.01403
1.6559 2.02918
1.7999 1.908027
1.9199 1.968656
1.9439 1.862656
1.9679 1.968656
2.0879 1.968656
2.3999 1.802028
2.7359 1.908027
2.7839 1.756656
2.8079 1.847499
2.9279 1.544557
2.9759 0.802587
3.0239 0.287715
3.0959 0.0

35
core/resources-src/datafiles/thrustcurves/manual/at130721.eng
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@ -1,35 +0,0 @@
; @File: at130721.asc, @Pts-I: 538, @Pts-O: 31, @Sm: 0, @CO: 5%
; @TI: 17.10047, @TIa: 17.06124, @TIe: +0.05%, @ThMax: 8.3068, @ThAvg: 2.05042, @Tb: 8.34
; Exported using ThrustCurveTool, www.ThrustGear.com
D2 18 70 P 0.0107 0.0266 AT
0.016 0.0453094
0.064 6.90221
0.08 7.73285
0.096 7.80834
0.112 8.2161
0.144 8.3068
0.16 8.0349
0.176 8.24634
0.192 8.00466
0.24 7.98954
0.48 6.41886
0.736 4.00232
0.784 3.20191
0.864 2.47688
1.024 2.12959
1.6159 2.03889
1.7439 1.827447
1.8719 1.872798
1.8879 2.08424
1.9359 1.827447
2.0639 1.933167
2.0959 1.751961
2.2879 1.721727
2.3199 1.872798
2.7999 1.661358
2.9439 1.827447
3.0559 1.676475
4.4638 1.70671
8.1437 1.162992
8.3677 0.362474
8.5916 0.0

2179
core/resources-src/datafiles/thrustcurves/thrustcurve.org/00INDEX.txt
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16
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AMW_I223.eng Normal file
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; 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 Normal file
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<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>

19
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AMW_I297.eng Normal file
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; 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

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core/resources-src/datafiles/thrustcurves/thrustcurve.org/AMW_I297.rse Normal file
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<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>

49
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AMW_J1365.rse Normal file
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<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>

44
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AMW_J325.rse Normal file
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<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>

67
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@ -0,0 +1,67 @@
<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>

91
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AMW_J400.rse
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@ -1,42 +1,61 @@
<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.
<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 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"/>
<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-list>
</engine-database>

42
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AMW_J400_1.rse Normal file
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@ -0,0 +1,42 @@
<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>

43
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AMW_J440.eng
View File

@ -1,27 +1,16 @@
;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
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

59
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AMW_J440.rse
View File

@ -1,34 +1,29 @@
<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-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
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;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
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@ -0,0 +1,34 @@
<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>

23
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AMW_J475.eng Normal file
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@ -0,0 +1,23 @@
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
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<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 Normal file
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<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>

75
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<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>

80
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@ -1,39 +1,41 @@
;
;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
; 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

97
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AMW_K1075.rse
View File

@ -1,47 +1,54 @@
<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-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 Normal file
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;
;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 Normal file
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<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 Normal file
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; 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 Normal file
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<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 Normal file
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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 Normal file
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<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 Normal file
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<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>

59
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<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>

85
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<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>

48
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;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

21
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AMW_K610.eng Normal file
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@ -0,0 +1,21 @@
; 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 Normal file
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@ -0,0 +1,33 @@
<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>

58
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AMW_K665.rse Normal file
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@ -0,0 +1,58 @@
<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>

117
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@ -1,42 +1,87 @@
<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.
<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 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"/>
<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-list>
</engine-database>

42
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View File

@ -0,0 +1,42 @@
<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>

94
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AMW_K700.rse
View File

@ -1,44 +1,62 @@
<engine-database>
<engine-list>
<engine FDiv="10" FFix="1" FStep="-1." Isp="217.41" Itot="1607.6" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="717.677" burn-time="2.24" cgDiv="10" cgFix="1" cgStep="-1." code="K700BB" delays="1000" dia="54." exitDia="0." initWt="1483.1" len="430." mDiv="10" mFix="1" mStep="-1." massFrac="50.84" mfg="Animal Motor Works" peakThrust="847.06" propWt="754." tDiv="10" tFix="1" tStep="-1." throatDia="0.">
<comments>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.
<engine-list>
<engine mfg="Cesaroni Technology Inc." code="K701BB" Type="reloadable" dia="54."
len="491." initWt="2088." propWt="1205." delays="1000" auto-calc-mass="1"
auto-calc-cg="1" avgThrust="697.011" peakThrust="840.686" throatDia="0."
exitDia="0." Itot="1658.19" burn-time="2.38" massFrac="57.71" Isp="140.32"
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 cg="215." f="0." m="754." t="0."/>
<eng-data cg="215." f="359.559" m="752.82" t="0.014"/>
<eng-data cg="215." f="625.425" m="750.972" t="0.022"/>
<eng-data cg="215." f="737.756" m="748.414" t="0.03"/>
<eng-data cg="215." f="771.505" m="742.397" t="0.047"/>
<eng-data cg="215." f="786.516" m="729.609" t="0.082"/>
<eng-data cg="215." f="771.505" m="720.84" t="0.106"/>
<eng-data cg="215." f="775.233" m="707.056" t="0.144"/>
<eng-data cg="215." f="786.516" m="660.177" t="0.272"/>
<eng-data cg="215." f="812.71" m="583.294" t="0.477"/>
<eng-data cg="215." f="842.632" m="499.444" t="0.693"/>
<eng-data cg="215." f="847.06" m="389.682" t="0.97"/>
<eng-data cg="215." f="838.904" m="265.928" t="1.283"/>
<eng-data cg="215." f="816.438" m="175.479" t="1.516"/>
<eng-data cg="215." f="801.427" m="103.391" t="1.706"/>
<eng-data cg="215." f="793.972" m="76.0788" t="1.779"/>
<eng-data cg="215." f="775.233" m="64.3029" t="1.811"/>
<eng-data cg="215." f="726.573" m="53.7372" t="1.841"/>
<eng-data cg="215." f="625.425" m="43.5913" t="1.873"/>
<eng-data cg="215." f="509.367" m="34.0109" t="1.909"/>
<eng-data cg="215." f="393.208" m="25.3327" t="1.95"/>
<eng-data cg="215." f="337.093" m="19.8523" t="1.982"/>
<eng-data cg="215." f="292.16" m="12.0312" t="2.035"/>
<eng-data cg="215." f="228.489" m="7.39147" t="2.073"/>
<eng-data cg="215." f="153.535" m="3.98709" t="2.111"/>
<eng-data cg="215." f="86.137" m="1.51403" t="2.155"/>
<eng-data cg="215." f="37.446" m="0.412731" t="2.193"/>
<eng-data cg="215." f="0." m="0." t="2.24"/>
<eng-data t="0." f="0." m="1205." cg="245.5"/>
<eng-data t="0.015" f="605.685" m="1201.7" cg="245.5"/>
<eng-data t="0.02" f="693.81" m="1199.34" cg="245.5"/>
<eng-data t="0.037" f="714.793" m="1190.64" cg="245.5"/>
<eng-data t="0.056" f="744.168" m="1180.57" cg="245.5"/>
<eng-data t="0.073" f="711.995" m="1171.57" cg="245.5"/>
<eng-data t="0.1" f="695.209" m="1157.77" cg="245.5"/>
<eng-data t="0.132" f="685.418" m="1141.71" cg="245.5"/>
<eng-data t="0.157" f="691.013" m="1129.21" cg="245.5"/>
<eng-data t="0.235" f="710.596" m="1089.49" cg="245.5"/>
<eng-data t="0.333" f="731.578" m="1038.13" cg="245.5"/>
<eng-data t="0.428" f="749.763" m="987." cg="245.5"/>
<eng-data t="0.531" f="762.352" m="930.409" cg="245.5"/>
<eng-data t="0.617" f="774.941" m="882.372" cg="245.5"/>
<eng-data t="0.69" f="781.936" m="841.077" cg="245.5"/>
<eng-data t="0.764" f="790.328" m="798.802" cg="245.5"/>
<eng-data t="0.876" f="802.918" m="733.965" cg="245.5"/>
<eng-data t="0.957" f="812.709" m="686.415" cg="245.5"/>
<eng-data t="1.023" f="819.703" m="647.268" cg="245.5"/>
<eng-data t="1.084" f="826.697" m="610.777" cg="245.5"/>
<eng-data t="1.192" f="832.293" m="545.675" cg="245.5"/>
<eng-data t="1.246" f="840.686" m="512.85" cg="245.5"/>
<eng-data t="1.307" f="833.692" m="475.739" cg="245.5"/>
<eng-data t="1.393" f="826.697" m="423.855" cg="245.5"/>
<eng-data t="1.444" f="821.102" m="393.32" cg="245.5"/>
<eng-data t="1.508" f="811.311" m="355.359" cg="245.5"/>
<eng-data t="1.574" f="794.525" m="316.85" cg="245.5"/>
<eng-data t="1.633" f="776.34" m="283.174" cg="245.5"/>
<eng-data t="1.713" f="744.168" m="238.976" cg="245.5"/>
<eng-data t="1.777" f="709.197" m="205.179" cg="245.5"/>
<eng-data t="1.853" f="668.632" m="167.131" cg="245.5"/>
<eng-data t="1.916" f="640.656" m="137.161" cg="245.5"/>
<eng-data t="1.956" f="615.477" m="118.904" cg="245.5"/>
<eng-data t="2.012" f="602.888" m="94.1132" cg="245.5"/>
<eng-data t="2.044" f="588.9" m="80.2562" cg="245.5"/>
<eng-data t="2.083" f="553.929" m="64.0616" cg="245.5"/>
<eng-data t="2.115" f="518.959" m="51.587" cg="245.5"/>
<eng-data t="2.146" f="483.989" m="40.29" cg="245.5"/>
<eng-data t="2.169" f="463.007" m="32.3759" cg="245.5"/>
<eng-data t="2.186" f="426.637" m="26.8806" cg="245.5"/>
<eng-data t="2.222" f="328.721" m="17.0001" cg="245.5"/>
<eng-data t="2.249" f="253.185" m="11.2914" cg="245.5"/>
<eng-data t="2.279" f="179.048" m="6.57987" cg="245.5"/>
<eng-data t="2.306" f="123.095" m="3.61572" cg="245.5"/>
<eng-data t="2.352" f="58.75" m="0.576361" cg="245.5"/>
<eng-data t="2.379" f="0." m="0." cg="245.5"/>
</data>
</engine>
</engine-list>
</engine-list>
</engine-database>

44
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AMW_K700_1.rse Normal file
View File

@ -0,0 +1,44 @@
<engine-database>
<engine-list>
<engine FDiv="10" FFix="1" FStep="-1." Isp="217.41" Itot="1607.6" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="717.677" burn-time="2.24" cgDiv="10" cgFix="1" cgStep="-1." code="K700BB" delays="1000" dia="54." exitDia="0." initWt="1483.1" len="430." mDiv="10" mFix="1" mStep="-1." massFrac="50.84" mfg="Animal Motor Works" peakThrust="847.06" propWt="754." tDiv="10" tFix="1" tStep="-1." throatDia="0.">
<comments>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.
</comments>
<data>
<eng-data cg="215." f="0." m="754." t="0."/>
<eng-data cg="215." f="359.559" m="752.82" t="0.014"/>
<eng-data cg="215." f="625.425" m="750.972" t="0.022"/>
<eng-data cg="215." f="737.756" m="748.414" t="0.03"/>
<eng-data cg="215." f="771.505" m="742.397" t="0.047"/>
<eng-data cg="215." f="786.516" m="729.609" t="0.082"/>
<eng-data cg="215." f="771.505" m="720.84" t="0.106"/>
<eng-data cg="215." f="775.233" m="707.056" t="0.144"/>
<eng-data cg="215." f="786.516" m="660.177" t="0.272"/>
<eng-data cg="215." f="812.71" m="583.294" t="0.477"/>
<eng-data cg="215." f="842.632" m="499.444" t="0.693"/>
<eng-data cg="215." f="847.06" m="389.682" t="0.97"/>
<eng-data cg="215." f="838.904" m="265.928" t="1.283"/>
<eng-data cg="215." f="816.438" m="175.479" t="1.516"/>
<eng-data cg="215." f="801.427" m="103.391" t="1.706"/>
<eng-data cg="215." f="793.972" m="76.0788" t="1.779"/>
<eng-data cg="215." f="775.233" m="64.3029" t="1.811"/>
<eng-data cg="215." f="726.573" m="53.7372" t="1.841"/>
<eng-data cg="215." f="625.425" m="43.5913" t="1.873"/>
<eng-data cg="215." f="509.367" m="34.0109" t="1.909"/>
<eng-data cg="215." f="393.208" m="25.3327" t="1.95"/>
<eng-data cg="215." f="337.093" m="19.8523" t="1.982"/>
<eng-data cg="215." f="292.16" m="12.0312" t="2.035"/>
<eng-data cg="215." f="228.489" m="7.39147" t="2.073"/>
<eng-data cg="215." f="153.535" m="3.98709" t="2.111"/>
<eng-data cg="215." f="86.137" m="1.51403" t="2.155"/>
<eng-data cg="215." f="37.446" m="0.412731" t="2.193"/>
<eng-data cg="215." f="0." m="0." t="2.24"/>
</data>
</engine>
</engine-list>
</engine-database>

17
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AMW_K710.eng Normal file
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@ -0,0 +1,17 @@
K710-BB 54 491 0 0.902 1.812 AMW/ProX
0.01 500
0.02 850
0.025 910
0.03 840
0.06 860
0.12 875
0.2 875
0.3 872
1.1 815
1.85 740
1.95 720
2.2 295
2.37 280
2.5 90
2.6 20
2.8 0

30
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AMW_K710.rse Normal file
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<engine-database>
<engine-list>
<engine mfg="AMW-ProX" code="K710-BB" Type="unspecified" dia="54." len="491."
initWt="1812." propWt="902." delays="0" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="639.696" peakThrust="910." throatDia="0." exitDia="0." Itot="1791.15"
burn-time="2.8" massFrac="49.78" Isp="202.49" 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="902." cg="245.5"/>
<eng-data t="0.01" f="500." m="900.741" cg="245.5"/>
<eng-data t="0.02" f="850." m="897.342" cg="245.5"/>
<eng-data t="0.025" f="910." m="895.126" cg="245.5"/>
<eng-data t="0.03" f="840." m="892.923" cg="245.5"/>
<eng-data t="0.06" f="860." m="880.081" cg="245.5"/>
<eng-data t="0.12" f="875." m="853.87" cg="245.5"/>
<eng-data t="0.2" f="875." m="818.619" cg="245.5"/>
<eng-data t="0.3" f="872." m="774.63" cg="245.5"/>
<eng-data t="1.1" f="815." m="434.81" cg="245.5"/>
<eng-data t="1.85" f="740." m="141.155" cg="245.5"/>
<eng-data t="1.95" f="720." m="104.394" cg="245.5"/>
<eng-data t="2.2" f="295." m="40.501" cg="245.5"/>
<eng-data t="2.37" f="280." m="15.8882" cg="245.5"/>
<eng-data t="2.5" f="90." m="3.7769" cg="245.5"/>
<eng-data t="2.6" f="20." m="1.00717" cg="245.5"/>
<eng-data t="2.8" f="0." m="0." cg="245.5"/>
</data>
</engine>
</engine-list>
</engine-database>

61
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AMW_K855.rse Normal file
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<engine-database>
<engine-list>
<engine mfg="Cesaroni Technology Inc." code="K855BB" Type="reloadable" dia="54."
len="491." initWt="2121." propWt="1205." delays="1000" auto-calc-mass="1"
auto-calc-cg="1" avgThrust="857.905" peakThrust="1021.66" throatDia="0."
exitDia="0." Itot="1731.25" burn-time="2.02" massFrac="56.81" Isp="146.51"
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="1205." cg="245.5"/>
<eng-data t="0.008" f="863.997" m="1202.59" cg="245.5"/>
<eng-data t="0.023" f="756.786" m="1194.13" cg="245.5"/>
<eng-data t="0.027" f="899.734" m="1191.83" cg="245.5"/>
<eng-data t="0.042" f="857.691" m="1182.65" cg="245.5"/>
<eng-data t="0.046" f="916.552" m="1180.18" cg="245.5"/>
<eng-data t="0.058" f="880.815" m="1172.68" cg="245.5"/>
<eng-data t="0.073" f="868.202" m="1163.55" cg="245.5"/>
<eng-data t="0.088" f="851.384" m="1154.57" cg="245.5"/>
<eng-data t="0.098" f="855.589" m="1148.63" cg="245.5"/>
<eng-data t="0.123" f="872.406" m="1133.6" cg="245.5"/>
<eng-data t="0.177" f="889.224" m="1100.49" cg="245.5"/>
<eng-data t="0.281" f="920.756" m="1034.98" cg="245.5"/>
<eng-data t="0.402" f="943.88" m="956.462" cg="245.5"/>
<eng-data t="0.494" f="962.8" m="895.415" cg="245.5"/>
<eng-data t="0.559" f="973.311" m="851.618" cg="245.5"/>
<eng-data t="0.636" f="985.924" m="799.117" cg="245.5"/>
<eng-data t="0.711" f="990.128" m="747.54" cg="245.5"/>
<eng-data t="0.784" f="1002.74" m="696.911" cg="245.5"/>
<eng-data t="0.859" f="1011.15" m="644.346" cg="245.5"/>
<eng-data t="0.932" f="1013.25" m="592.916" cg="245.5"/>
<eng-data t="1.017" f="1021.66" m="532.721" cg="245.5"/>
<eng-data t="1.08" f="1011.15" m="488.152" cg="245.5"/>
<eng-data t="1.136" f="1000.64" m="448.945" cg="245.5"/>
<eng-data t="1.246" f="977.515" m="373.218" cg="245.5"/>
<eng-data t="1.303" f="967.004" m="334.645" cg="245.5"/>
<eng-data t="1.374" f="935.472" m="287.637" cg="245.5"/>
<eng-data t="1.455" f="891.326" m="236.141" cg="245.5"/>
<eng-data t="1.505" f="855.589" m="205.743" cg="245.5"/>
<eng-data t="1.584" f="798.83" m="160.258" cg="245.5"/>
<eng-data t="1.64" f="750.479" m="130.064" cg="245.5"/>
<eng-data t="1.688" f="727.355" m="105.377" cg="245.5"/>
<eng-data t="1.726" f="714.742" m="86.3063" cg="245.5"/>
<eng-data t="1.745" f="712.64" m="76.8681" cg="245.5"/>
<eng-data t="1.757" f="689.516" m="71.0124" cg="245.5"/>
<eng-data t="1.782" f="668.494" m="59.1973" cg="245.5"/>
<eng-data t="1.826" f="626.451" m="39.3683" cg="245.5"/>
<eng-data t="1.845" f="590.714" m="31.3201" cg="245.5"/>
<eng-data t="1.87" f="498.217" m="21.846" cg="245.5"/>
<eng-data t="1.901" f="353.167" m="12.6609" cg="245.5"/>
<eng-data t="1.928" f="239.649" m="7.09056" cg="245.5"/>
<eng-data t="1.951" f="159.766" m="3.89352" cg="245.5"/>
<eng-data t="1.972" f="100.905" m="1.98846" cg="245.5"/>
<eng-data t="1.997" f="69.372" m="0.506991" cg="245.5"/>
<eng-data t="2.018" f="0." m="0." cg="245.5"/>
</data>
</engine>
</engine-list>
</engine-database>

48
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AMW_K935.eng Normal file
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@ -0,0 +1,48 @@
;Created by Jesus Manuel Recuenco Andres 2011
;with Tctracer v1.0
K935 54.0 403.00 1000 0.73200 1.50800 Cesaroni
0.01 1072.70
0.02 1043.71
0.04 974.21
0.07 1015.94
0.10 1029.21
0.14 1040.97
0.17 1049.51
0.22 1059.74
0.25 1064.00
0.29 1070.18
0.34 1072.70
0.39 1072.26
0.42 1069.80
0.45 1072.70
0.49 1069.80
0.52 1070.18
0.58 1064.00
0.64 1059.74
0.70 1055.30
0.76 1045.14
0.81 1035.01
0.85 1029.21
0.88 1022.20
0.91 1017.62
0.94 1014.72
0.97 1008.92
1.00 1003.42
1.06 985.72
1.12 965.87
1.16 950.93
1.21 936.66
1.26 919.04
1.30 903.29
1.34 890.05
1.38 876.17
1.43 861.06
1.48 846.96
1.51 719.71
1.54 619.58
1.56 510.26
1.58 415.14
1.60 295.72
1.63 181.49
1.66 66.76
1.70 0.00

24
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AMW_L1276.eng Normal file
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; AMX/ProX 2729L1276 RR
L1276RR 54 728 P 1.475 2.96 AMW
0.015 76.924
0.017 692.317
0.026 1495.003
0.037 1244.164
0.052 1401.357
0.084 1307.71
0.127 1307.71
0.181 1367.911
0.289 1401.357
0.384 1408.046
0.807 1421.424
0.993 1461.558
1.215 1491.659
1.673 1474.936
1.727 1384.634
1.798 1083.627
1.947 531.78
1.986 351.175
2.047 177.26
2.092 93.647
2.144 33.445
2.185 0.0

37
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AMW_L1276.rse Normal file
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@ -0,0 +1,37 @@
<engine-database>
<engine-list>
<engine mfg="AMW" code="L1276RR" Type="unspecified" dia="54." len="728." initWt="2960."
propWt="1475." delays="0" auto-calc-mass="1" auto-calc-cg="1" avgThrust="1237.17"
peakThrust="1495." throatDia="0." exitDia="0." Itot="2703.21" burn-time="2.19"
massFrac="49.83" Isp="186.88" 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>AMX/ProX 2729L1276 RR</comments>
<data>
<eng-data t="0." f="0." m="1475." cg="364."/>
<eng-data t="0.015" f="76.924" m="1474.69" cg="364."/>
<eng-data t="0.017" f="692.317" m="1474.27" cg="364."/>
<eng-data t="0.026" f="1495." m="1468.89" cg="364."/>
<eng-data t="0.037" f="1244.16" m="1460.67" cg="364."/>
<eng-data t="0.052" f="1401.36" m="1449.85" cg="364."/>
<eng-data t="0.084" f="1307.71" m="1426.2" cg="364."/>
<eng-data t="0.127" f="1307.71" m="1395.51" cg="364."/>
<eng-data t="0.181" f="1367.91" m="1356.1" cg="364."/>
<eng-data t="0.289" f="1401.36" m="1274.5" cg="364."/>
<eng-data t="0.384" f="1408.05" m="1201.68" cg="364."/>
<eng-data t="0.807" f="1421.42" m="875.151" cg="364."/>
<eng-data t="0.993" f="1461.56" m="728.853" cg="364."/>
<eng-data t="1.215" f="1491.66" m="549.986" cg="364."/>
<eng-data t="1.673" f="1474.94" m="179.3" cg="364."/>
<eng-data t="1.727" f="1384.63" m="137.171" cg="364."/>
<eng-data t="1.798" f="1083.63" m="89.3597" cg="364."/>
<eng-data t="1.947" f="531.78" m="23.6922" cg="364."/>
<eng-data t="1.986" f="351.175" m="14.2974" cg="364."/>
<eng-data t="2.047" f="177.26" m="5.50309" cg="364."/>
<eng-data t="2.092" f="93.647" m="2.17714" cg="364."/>
<eng-data t="2.144" f="33.445" m="0.374108" cg="364."/>
<eng-data t="2.185" f="0." m="0." cg="364."/>
</data>
</engine>
</engine-list>
</engine-database>

21
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AMW_L1290.eng Normal file
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@ -0,0 +1,21 @@
; ABC-76-6000 4701L1290-SK P
L1290-SK 76 785 P 3.047 5.399 CTI
0.022 117.623
0.081 786.023
0.11 797.226
0.176 1226.645
0.691 1357.337
1.231 1461.891
1.761 1476.828
2.008 1467.493
2.311 1417.082
2.835 1299.459
3.101 1235.98
3.167 1230.379
3.34 1321.863
3.373 1286.39
3.532 365.94
3.602 201.64
3.734 91.485
3.782 69.08
3.8 0.0

34
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AMW_L1290.rse Normal file
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@ -0,0 +1,34 @@
<engine-database>
<engine-list>
<engine mfg="CTI" code="L1290-SK" Type="unspecified" dia="76." len="785." initWt="5399."
propWt="3047." delays="0" auto-calc-mass="1" auto-calc-cg="1" avgThrust="1234.96"
peakThrust="1476.83" throatDia="0." exitDia="0." Itot="4692.85" burn-time="3.8"
massFrac="56.44" Isp="157.05" 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>ABC-76-6000 4701L1290-SK P</comments>
<data>
<eng-data t="0." f="0." m="3047." cg="392.5"/>
<eng-data t="0.022" f="117.623" m="3046.16" cg="392.5"/>
<eng-data t="0.081" f="786.023" m="3028.85" cg="392.5"/>
<eng-data t="0.11" f="797.226" m="3013.95" cg="392.5"/>
<eng-data t="0.176" f="1226.64" m="2970.58" cg="392.5"/>
<eng-data t="0.691" f="1357.34" m="2538.56" cg="392.5"/>
<eng-data t="1.231" f="1461.89" m="2044.33" cg="392.5"/>
<eng-data t="1.761" f="1476.83" m="1538.69" cg="392.5"/>
<eng-data t="2.008" f="1467.49" m="1302.6" cg="392.5"/>
<eng-data t="2.311" f="1417.08" m="1018.85" cg="392.5"/>
<eng-data t="2.835" f="1299.46" m="556.734" cg="392.5"/>
<eng-data t="3.101" f="1235.98" m="337.786" cg="392.5"/>
<eng-data t="3.167" f="1230.38" m="284.94" cg="392.5"/>
<eng-data t="3.34" f="1321.86" m="141.598" cg="392.5"/>
<eng-data t="3.373" f="1286.39" m="113.656" cg="392.5"/>
<eng-data t="3.532" f="365.94" m="28.3652" cg="392.5"/>
<eng-data t="3.602" f="201.64" m="15.467" cg="392.5"/>
<eng-data t="3.734" f="91.485" m="2.90574" cg="392.5"/>
<eng-data t="3.782" f="69.08" m="0.403674" cg="392.5"/>
<eng-data t="3.8" f="0." m="0." cg="392.5"/>
</data>
</engine>
</engine-list>
</engine-database>

56
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AMW_L985.rse Normal file
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@ -0,0 +1,56 @@
<engine-database>
<engine-list>
<engine mfg="Cesaroni Technology Inc." code="L985TT" Type="reloadable" dia="54."
len="491." initWt="2572." propWt="1295." delays="1000" auto-calc-mass="1"
auto-calc-cg="1" avgThrust="996.381" peakThrust="1483.94" throatDia="0."
exitDia="0." Itot="2678.27" burn-time="2.69" massFrac="50.35" Isp="210.89"
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="1295." cg="245.5"/>
<eng-data t="0.017" f="1483.94" m="1288.9" cg="245.5"/>
<eng-data t="0.033" f="1394.18" m="1277.77" cg="245.5"/>
<eng-data t="0.061" f="1315.63" m="1259.42" cg="245.5"/>
<eng-data t="0.081" f="1251.11" m="1247.01" cg="245.5"/>
<eng-data t="0.103" f="1290.38" m="1233.5" cg="245.5"/>
<eng-data t="0.134" f="1307.22" m="1214.03" cg="245.5"/>
<eng-data t="0.17" f="1310.02" m="1191.25" cg="245.5"/>
<eng-data t="0.27" f="1287.58" m="1128.45" cg="245.5"/>
<eng-data t="0.396" f="1270.75" m="1050.52" cg="245.5"/>
<eng-data t="0.485" f="1262.33" m="996.015" cg="245.5"/>
<eng-data t="0.56" f="1231.48" m="950.798" cg="245.5"/>
<eng-data t="0.618" f="1253.92" m="915.947" cg="245.5"/>
<eng-data t="0.699" f="1242.7" m="867.057" cg="245.5"/>
<eng-data t="0.827" f="1220.26" m="790.84" cg="245.5"/>
<eng-data t="1.087" f="1178.18" m="640.08" cg="245.5"/>
<eng-data t="1.273" f="1158.54" m="535.004" cg="245.5"/>
<eng-data t="1.443" f="1136.1" m="440.696" cg="245.5"/>
<eng-data t="1.619" f="1119.27" m="344.731" cg="245.5"/>
<eng-data t="1.755" f="1096.83" m="271.867" cg="245.5"/>
<eng-data t="1.83" f="1091.22" m="232.193" cg="245.5"/>
<eng-data t="1.878" f="1085.61" m="206.932" cg="245.5"/>
<eng-data t="1.917" f="1082.8" m="186.487" cg="245.5"/>
<eng-data t="1.942" f="1060.36" m="173.534" cg="245.5"/>
<eng-data t="1.972" f="1021.09" m="158.438" cg="245.5"/>
<eng-data t="2.034" f="906.074" m="129.551" cg="245.5"/>
<eng-data t="2.07" f="813.503" m="114.585" cg="245.5"/>
<eng-data t="2.12" f="701.296" m="96.2741" cg="245.5"/>
<eng-data t="2.162" f="633.972" m="82.7159" cg="245.5"/>
<eng-data t="2.195" f="594.699" m="72.9134" cg="245.5"/>
<eng-data t="2.246" f="530.18" m="59.0439" cg="245.5"/>
<eng-data t="2.298" f="451.635" m="46.701" cg="245.5"/>
<eng-data t="2.34" f="395.531" m="38.0989" cg="245.5"/>
<eng-data t="2.407" f="328.207" m="26.3759" cg="245.5"/>
<eng-data t="2.454" f="272.103" m="19.5547" cg="245.5"/>
<eng-data t="2.53" f="210.389" m="10.6895" cg="245.5"/>
<eng-data t="2.56" f="187.947" m="7.80046" cg="245.5"/>
<eng-data t="2.602" f="162.701" m="4.24001" cg="245.5"/>
<eng-data t="2.649" f="115.013" m="1.08442" cg="245.5"/>
<eng-data t="2.688" f="0." m="0." cg="245.5"/>
</data>
</engine>
</engine-list>
</engine-database>

19
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AMW_M1630.eng Normal file
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@ -0,0 +1,19 @@
; AMW75-7600 8212M1630-TT/DT P
M1630-TT 75 1039 P 4.349 7.237 CTI
0.0030 147.481
0.032 2040.948
0.078 3235.069
0.158 3368.278
0.463 3258.856
0.647 2992.439
0.949 2697.477
1.052 2040.948
1.101 1883.952
1.392 1907.739
1.786 1812.59
3.6 1327.33
3.899 875.372
4.595 347.294
4.857 195.056
4.891 166.511
4.9 0.0

32
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AMW_M1630.rse Normal file
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@ -0,0 +1,32 @@
<engine-database>
<engine-list>
<engine mfg="CTI" code="M1630-TT" Type="unspecified" dia="75." len="1039."
initWt="7237." propWt="4349." delays="0" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="1666.9" peakThrust="3368.28" throatDia="0." exitDia="0." Itot="8167.8"
burn-time="4.9" massFrac="60.09" Isp="191.51" 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>AMW75-7600 8212M1630-TT/DT P</comments>
<data>
<eng-data t="0." f="0." m="4349." cg="519.5"/>
<eng-data t="0.003" f="147.481" m="4348.88" cg="519.5"/>
<eng-data t="0.032" f="2040.95" m="4331.99" cg="519.5"/>
<eng-data t="0.078" f="3235.07" m="4267.37" cg="519.5"/>
<eng-data t="0.158" f="3368.28" m="4126.73" cg="519.5"/>
<eng-data t="0.463" f="3258.86" m="3588.61" cg="519.5"/>
<eng-data t="0.647" f="2992.44" m="3282.39" cg="519.5"/>
<eng-data t="0.949" f="2697.48" m="2824.91" cg="519.5"/>
<eng-data t="1.052" f="2040.95" m="2694.98" cg="519.5"/>
<eng-data t="1.101" f="1883.95" m="2643.78" cg="519.5"/>
<eng-data t="1.392" f="1907.74" m="2350.02" cg="519.5"/>
<eng-data t="1.786" f="1812.59" m="1959.78" cg="519.5"/>
<eng-data t="3.6" f="1327.33" m="443.396" cg="519.5"/>
<eng-data t="3.899" f="875.372" m="268.056" cg="519.5"/>
<eng-data t="4.595" f="347.294" m="41.5017" cg="519.5"/>
<eng-data t="4.857" f="195.056" m="3.67179" cg="519.5"/>
<eng-data t="4.891" f="166.511" m="0.39897" cg="519.5"/>
<eng-data t="4.9" f="0." m="0." cg="519.5"/>
</data>
</engine>
</engine-list>
</engine-database>

16
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AMW_M2050.eng Normal file
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@ -0,0 +1,16 @@
; AMX75-7600 6774-M2050-SK P
M2050-BS 75 1039 P 4.172 7.1290000000000004 ABC
0.038 2152.81
0.833 2506.091
1.189 2539.211
1.546 2500.571
1.775 2415.011
1.907 2279.77
2.168 2086.569
2.401 1973.409
2.616 1909.929
2.776 1871.288
2.918 1203.365
3.056 706.563
3.309 135.241
3.4 0.0

29
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AMW_M2050.rse Normal file
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@ -0,0 +1,29 @@
<engine-database>
<engine-list>
<engine mfg="ABC" code="M2050-BS" Type="unspecified" dia="75." len="1039."
initWt="7129." propWt="4172." delays="0" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="1996.66" peakThrust="2539.21" throatDia="0." exitDia="0."
Itot="6788.65" burn-time="3.4" massFrac="58.52" Isp="165.93" 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>AMX75-7600 6774-M2050-SK P</comments>
<data>
<eng-data t="0." f="0." m="4172." cg="519.5"/>
<eng-data t="0.038" f="2152.81" m="4146.86" cg="519.5"/>
<eng-data t="0.833" f="2506.09" m="3008.76" cg="519.5"/>
<eng-data t="1.189" f="2539.21" m="2456.85" cg="519.5"/>
<eng-data t="1.546" f="2500.57" m="1904." cg="519.5"/>
<eng-data t="1.775" f="2415.01" m="1558.1" cg="519.5"/>
<eng-data t="1.907" f="2279.77" m="1367.68" cg="519.5"/>
<eng-data t="2.168" f="2086.57" m="1017.5" cg="519.5"/>
<eng-data t="2.401" f="1973.41" m="726.824" cg="519.5"/>
<eng-data t="2.616" f="1909.93" m="470.273" cg="519.5"/>
<eng-data t="2.776" f="1871.29" m="284.371" cg="519.5"/>
<eng-data t="2.918" f="1203.37" m="150.214" cg="519.5"/>
<eng-data t="3.056" f="706.563" m="69.2245" cg="519.5"/>
<eng-data t="3.309" f="135.241" m="3.78164" cg="519.5"/>
<eng-data t="3.4" f="0." m="0." cg="519.5"/>
</data>
</engine>
</engine-list>
</engine-database>

31
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AeroTech_C3.eng Normal file
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@ -0,0 +1,31 @@
; Aerotech C3.4-PT RASP.ENG file made from NAR published data
; File produced, 2013
; 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.
C3.4 18 72 0, .0052 .0239 A
0.023 3.188
0.028 5.669
0.093 9.080
0.235 8.208
0.427 6.881
0.513 6.188
0.600 5.438
0.666 4.803
0.762 3.649
0.838 2.668
0.970 2.149
1.228 1.918
1.522 1.918
1.800 1.860
2.013 1.745
2.068 2.034
2.134 1.803
2.326 1.803
2.509 1.745
2.645 1.687
2.721 1.457
2.807 0.879
2.860 0.000

34
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AeroTech_D2.eng Normal file
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@ -0,0 +1,34 @@
; Aerotech D2.3-PT RASP.ENG file made from NAR published data
; File produced, 2013
; 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.
D2.3 18 72 0, .0107 .0293 A
0.020 5.071
0.039 9.478
0.093 10.140
0.184 9.478
0.275 8.429
0.438 6.820
0.657 4.372
0.747 3.392
0.838 2.413
1.056 2.064
1.365 1.923
1.892 1.783
2.528 1.713
2.946 1.713
3.219 1.643
4.091 1.573
4.727 1.573
5.218 1.573
5.636 1.573
6.217 1.573
6.726 1.433
7.199 1.503
7.635 1.363
7.907 1.224
8.016 0.734
8.140 0.000

74
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AeroTech_F20.eng
View File

@ -1,35 +1,39 @@
;
;
F20EJ 29 83 4-7 0.03 0.0746 AeroTech
0.01 52.08
0.03 49.81
0.06 46.98
0.1 45.56
0.15 44.49
0.18 45.55
0.21 43.42
0.24 43.78
0.32 43.77
0.36 44.11
0.44 43.04
0.45 40.58
0.53 39.86
0.62 38.08
0.76 36.3
0.8 37.35
0.84 34.88
0.89 36.99
0.9 33.46
1.03 30.61
1.06 32.02
1.09 29.55
1.23 26
1.32 22.45
1.35 23.16
1.36 21.39
1.58 16.42
1.8 11.1
2.01 6.48
2.19 3.63
2.39 1.13
2.68 0
; Aerotech F20 RASP.ENG file made from NAR published data
; File produced July 4, 2007
; 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.
F20 29 83 4-7 .0300 .0801 A
0.023 16.431
0.043 28.538
0.062 36.691
0.078 40.330
0.120 37.677
0.167 36.933
0.213 36.931
0.298 36.432
0.318 37.173
0.333 35.689
0.368 36.182
0.395 35.192
0.430 36.426
0.446 37.166
0.481 34.447
0.554 34.443
0.946 30.964
0.965 29.481
1.008 29.726
1.062 27.746
1.097 27.497
1.136 26.260
1.310 20.568
1.360 19.824
1.438 17.349
1.465 17.348
1.527 15.121
1.597 13.882
1.810 9.176
1.969 6.203
2.490 0.000

35
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AeroTech_F20_1.eng Normal file
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@ -0,0 +1,35 @@
;
;
F20EJ 29 83 4-7 0.03 0.0746 AeroTech
0.01 52.08
0.03 49.81
0.06 46.98
0.1 45.56
0.15 44.49
0.18 45.55
0.21 43.42
0.24 43.78
0.32 43.77
0.36 44.11
0.44 43.04
0.45 40.58
0.53 39.86
0.62 38.08
0.76 36.3
0.8 37.35
0.84 34.88
0.89 36.99
0.9 33.46
1.03 30.61
1.06 32.02
1.09 29.55
1.23 26
1.32 22.45
1.35 23.16
1.36 21.39
1.58 16.42
1.8 11.1
2.01 6.48
2.19 3.63
2.39 1.13
2.68 0

70
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AeroTech_G64.eng
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@ -1,38 +1,32 @@
;
;Aerotech G64 RASP.ENG file made from NAR published data
;File produced July 4, 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.
G64 29 124 4-8-10 0.0625 0.1512 AT
0.014 54.325
0.032 81.488
0.059 98.31
0.101 85.021
0.165 83.847
0.274 85.614
0.37 87.39
0.476 86.798
0.503 91.516
0.517 85.614
0.585 83.847
0.723 80.896
0.745 82.07
0.773 77.945
0.883 75.576
0.988 74.401
1.093 69.673
1.262 61.412
1.28 61.994
1.326 58.451
1.372 54.907
1.422 47.238
1.505 34.841
1.591 23.027
1.701 13.581
1.829 7.085
1.902 4.133
1.966 1.771
2.09 0
; Aerotech G64 Bifurcated RASP.ENG file made from data Supplied by Aerotech
; File produced August 10 by Tim Barr
; The curve drawn with these data points is as
; close to the test curve as can be with such a limited
; number of points (32) allowed with wRASP up to v1.6.
G64BF 29 124 4-8-10 0.0625 0.1512 AERO
0.01 9.5637
0.02 60.0510
0.03 77.4880
0.04 90.3211
0.05 98.8061
0.06 102.9986
0.07 105.9789
0.08 108.1140
0.09 108.0695
0.10 106.4237
0.15 104.0773
0.25 103.3222
0.35 100.4053
0.45 95.4399
0.55 90.4957
0.65 85.0522
0.75 79.2640
0.95 67.6591
1.15 53.0840
1.35 38.1535
1.55 23.7201
1.75 11.4636
1.95 4.6295
2.15 1.4518
2.35 0.1101
2.44 0

15
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AeroTech_H182.eng Normal file
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@ -0,0 +1,15 @@
; From AT DMS announcement May 2014.
H182 29 203.2 14 0.115 0.20700000000000002 AT
0.007 82.404
0.031 159.208
0.091 158.408
0.186 182.409
0.5 192.009
0.904 188.809
1.054 175.209
1.106 180.809
1.144 200.81
1.163 162.408
1.201 36.802
1.212 16.801
1.235 0.0

13
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AeroTech_H45_1.eng Normal file
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@ -0,0 +1,13 @@
; From AT DMS announcement May 2014.
H45 38 202.7 10 0.18 0.364 AT
0.04 84.004
0.854 86.004
1.377 84.804
2.046 79.204
2.69 66.003
3.286 51.603
4.414 28.401
5.042 16.001
5.429 9.2
6.113 6.4
6.186 0.0

41
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AeroTech_H550.eng Normal file
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@ -0,0 +1,41 @@
; AT H550 ST DMS
H550 38 206 14 0.176 0.316 AT
0.008 445.411
0.009 533.786
0.01 565.601
0.013 586.812
0.015 623.34
0.021 639.837
0.036 606.843
0.045 629.232
0.057 615.092
0.061 635.123
0.067 619.805
0.101 637.48
0.116 622.162
0.157 643.372
0.174 623.34
0.196 623.34
0.205 639.837
0.231 631.588
0.234 618.627
0.255 611.557
0.268 628.053
0.314 595.06
0.334 600.952
0.362 571.493
0.386 565.601
0.401 556.175
0.426 518.468
0.445 503.15
0.493 447.768
0.505 447.768
0.511 456.016
0.519 451.303
0.535 357.036
0.545 266.304
0.551 179.107
0.559 91.91
0.565 42.42
0.572 12.962
0.579 0.0

17
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AeroTech_I205.eng Normal file
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@ -0,0 +1,17 @@
; From AT DMS announcement May 2014.
I205 29 304.8 14 0.188 0.315 AT
0.008 377.299
0.028 241.932
0.36 256.333
0.711 246.252
0.861 233.292
1.121 230.411
1.146 214.571
1.242 211.69
1.349 141.127
1.404 125.286
1.489 72.004
1.602 41.762
1.712 11.521
1.787 12.961
1.892 0.0

15
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AeroTech_I65_1.eng Normal file
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@ -0,0 +1,15 @@
; From AT DMS announcement May 2014.
I65 54 218 10 0.377 0.752 AT
0.023 148.274
0.211 196.341
0.398 167.827
0.797 149.903
1.395 135.239
2.238 122.204
3.199 99.392
4.711 69.249
5.367 48.882
6.246 29.329
6.926 15.479
7.395 11.406
8.496 0.0

37
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AeroTech_J1799.eng Normal file
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@ -0,0 +1,37 @@
;
; AT 54-1280
; Greg Gardner - 09/15/06
J1999N 54 314 0 0.5574 1.111 AT
0.01 830
0.02 1716
0.03 1787
0.04 1873
0.05 1896
0.06 1918
0.07 1984
0.08 2007
0.09 2051
0.10 2058
0.12 2090
0.14 2098
0.16 2135
0.18 2138
0.20 2142
0.25 2146
0.30 2150
0.35 2146
0.40 2138
0.45 2096
0.50 1974
0.55 1864
0.57 1829
0.59 1815
0.60 1762
0.61 1673
0.62 1085
0.63 490
0.64 190
0.65 81
0.66 31
0.67 0
;

44
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AeroTech_J1799.rse Normal file
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@ -0,0 +1,44 @@
<engine-database>
<engine-list>
<engine FDiv="10" FFix="1" FStep="-1." Isp="228.74" Itot="1250.35" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="1866.19" burn-time="0.67" cgDiv="10" cgFix="1" cgStep="-1." code="J1999N" delays="1000" dia="54." exitDia="0." initWt="1111." len="314." mDiv="10" mFix="1" mStep="-1." massFrac="50.17" mfg="Aerotech" peakThrust="2150." propWt="557.4" tDiv="10" tFix="1" tStep="-1." throatDia="0.">
<comments>AT 54-852
Greg Gardner - 09/15/06
</comments>
<data>
<eng-data cg="157." f="0." m="557.4" t="0."/>
<eng-data cg="157." f="830." m="555.55" t="0.01"/>
<eng-data cg="157." f="1716." m="549.875" t="0.02"/>
<eng-data cg="157." f="1787." m="542.067" t="0.03"/>
<eng-data cg="157." f="1873." m="533.909" t="0.04"/>
<eng-data cg="157." f="1896." m="525.508" t="0.05"/>
<eng-data cg="157." f="1918." m="517.006" t="0.06"/>
<eng-data cg="157." f="1984." m="508.309" t="0.07"/>
<eng-data cg="157." f="2007." m="499.413" t="0.08"/>
<eng-data cg="157." f="2051." m="490.368" t="0.09"/>
<eng-data cg="157." f="2058." m="481.209" t="0.1"/>
<eng-data cg="157." f="2090." m="462.717" t="0.12"/>
<eng-data cg="157." f="2098." m="444.047" t="0.14"/>
<eng-data cg="157." f="2135." m="425.177" t="0.16"/>
<eng-data cg="157." f="2138." m="406.128" t="0.18"/>
<eng-data cg="157." f="2142." m="387.048" t="0.2"/>
<eng-data cg="157." f="2146." m="339.258" t="0.25"/>
<eng-data cg="157." f="2150." m="291.38" t="0.3"/>
<eng-data cg="157." f="2146." m="243.501" t="0.35"/>
<eng-data cg="157." f="2138." m="195.756" t="0.4"/>
<eng-data cg="157." f="2096." m="148.569" t="0.45"/>
<eng-data cg="157." f="1974." m="103.209" t="0.5"/>
<eng-data cg="157." f="1864." m="60.4345" t="0.55"/>
<eng-data cg="157." f="1829." m="43.9712" t="0.57"/>
<eng-data cg="157." f="1815." m="27.7263" t="0.59"/>
<eng-data cg="157." f="1762." m="19.7533" t="0.6"/>
<eng-data cg="157." f="1673." m="12.0967" t="0.61"/>
<eng-data cg="157." f="1085." m="5.94916" t="0.62"/>
<eng-data cg="157." f="490." m="2.43851" t="0.63"/>
<eng-data cg="157." f="190." m="0.9228" t="0.64"/>
<eng-data cg="157." f="81." m="0.318745" t="0.65"/>
<eng-data cg="157." f="31." m="0.0690985" t="0.66"/>
<eng-data cg="157." f="0." m="0." t="0.67"/>
</data>
</engine>
</engine-list>
</engine-database>

15
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AeroTech_J425.eng Normal file
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@ -0,0 +1,15 @@
; From AT DMS announcement May 2014.
J425 38 356.4 14 0.364 0.631 AT
0.018 267.857
0.062 368.062
0.242 420.092
0.524 443.216
0.902 452.851
1.225 448.997
1.389 433.581
1.502 452.851
1.53 420.092
1.542 356.5
1.599 67.446
1.618 28.905
1.648 0.0

21
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AeroTech_K535.eng Normal file
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@ -0,0 +1,21 @@
; revised per AT post on TRF 5/19/14
K535 54 358.1 14 0.745 1.264 AT
0.015 467.288
0.063 642.221
0.104 613.465
0.23 627.843
0.419 620.654
0.883 623.05
1.335 599.087
1.646 555.953
1.843 500.837
2.017 450.513
2.258 404.983
2.488 366.641
2.6 230.049
2.611 172.537
2.648 124.61
2.696 81.476
2.789 40.738
2.837 9.585
2.952 0.0

26
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AeroTech_L1000.eng Normal file
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@ -0,0 +1,26 @@
; per AT announcement 5/8/14
L1000 54 635 18 1.4000000000000001 2.194 AT
0.004 10.664
0.011 1268.961
0.04 1322.279
0.195 1226.307
0.249 1268.961
0.296 1242.303
0.372 1252.966
0.416 1215.644
0.6 1226.307
0.788 1215.644
1.066 1183.653
1.261 1167.658
1.507 1125.004
1.746 1087.681
1.865 1050.359
1.995 1045.027
2.093 911.733
2.158 746.448
2.263 554.504
2.389 405.215
2.577 191.944
2.693 85.308
2.761 42.654
3.0 0.0

26
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AeroTech_M1350.eng Normal file
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@ -0,0 +1,26 @@
; AT M1350W DMS
M1350W 75 622 p 1.97 4.808 AT
0.03 1428.886
0.044 1724.734
0.056 1548.484
0.078 1620.873
0.115 1589.399
0.178 1642.904
0.455 1749.913
0.496 1724.734
0.54 1737.324
1.132 1746.766
1.499 1731.029
1.639 1715.292
2.505 1334.466
3.086 1051.207
3.179 985.113
3.227 928.461
3.315 670.38
3.419 446.92
3.46 396.563
3.545 298.996
3.697 173.103
3.737 173.103
3.845 81.83
3.996 0.0

19
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AeroTech_M1350_1.eng Normal file
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@ -0,0 +1,19 @@
; from TMT cert letter 22 Jun 2014
M1350 75 622 P 1.97 4.808 AT
0.058 1591.743
0.45 1758.762
0.501 1723.334
0.717 1756.231
1.022 1758.762
1.651 1723.334
2.03 1561.376
2.213 1467.744
2.707 1245.052
3.029 1090.686
3.171 997.054
3.255 908.483
3.343 640.24
3.448 412.487
3.702 169.55
3.915 43.02
4.0 0.0

34
core/resources-src/datafiles/thrustcurves/thrustcurve.org/Cesarioni_G69.rse Normal file
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<engine-database>
<engine-list>
<engine mfg="CTI" code="G69SK" Type="unspecified" dia="38." len="126." initWt="198."
propWt="67." delays="14,11,9,7,5" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="59.043" peakThrust="91.872" throatDia="0." exitDia="0." Itot="116.255"
burn-time="1.97" massFrac="33.84" Isp="176.94" 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 Pro38-1G 117 G69SK - 14A</comments>
<data>
<eng-data t="0." f="0." m="67." cg="63."/>
<eng-data t="0.015" f="49.371" m="66.7866" cg="63."/>
<eng-data t="0.023" f="79.41" m="66.4897" cg="63."/>
<eng-data t="0.035" f="91.872" m="65.8974" cg="63."/>
<eng-data t="0.064" f="82.605" m="64.4394" cg="63."/>
<eng-data t="0.099" f="52.407" m="63.0777" cg="63."/>
<eng-data t="0.166" f="57.041" m="60.9647" cg="63."/>
<eng-data t="0.228" f="59.278" m="58.8865" cg="63."/>
<eng-data t="0.375" f="64.231" m="53.6548" cg="63."/>
<eng-data t="1.297" f="69.024" m="18.2513" cg="63."/>
<eng-data t="1.453" f="68.864" m="12.0528" cg="63."/>
<eng-data t="1.533" f="67.746" m="8.90358" cg="63."/>
<eng-data t="1.589" f="65.189" m="6.75842" cg="63."/>
<eng-data t="1.686" f="58.639" m="3.29726" cg="63."/>
<eng-data t="1.735" f="42.821" m="1.86466" cg="63."/>
<eng-data t="1.781" f="26.363" m="0.947608" cg="63."/>
<eng-data t="1.816" f="13.901" m="0.541523" cg="63."/>
<eng-data t="1.89" f="5.432" m="0.129271" cg="63."/>
<eng-data t="1.954" f="1.278" m="0.005524" cg="63."/>
<eng-data t="1.969" f="0." m="0." cg="63."/>
</data>
</engine>
</engine-list>
</engine-database>

29
core/resources-src/datafiles/thrustcurves/thrustcurve.org/Cesaroni_F32.rse Normal file
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<engine-database>
<engine-list>
<engine mfg="CTI" code="53-F32-WH-12A" Type="unspecified" dia="29." len="98.0008"
initWt="107." propWt="37." delays="12,9,7,5,3" auto-calc-mass="1"
auto-calc-cg="1" avgThrust="30.663" peakThrust="48.044" throatDia="0."
exitDia="0." Itot="52.925" burn-time="1.73" massFrac="34.58" Isp="145.86"
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 53-F32-WH-12A</comments>
<data>
<eng-data t="0." f="0." m="37." cg="49."/>
<eng-data t="0.002" f="2.999" m="36.9979" cg="49."/>
<eng-data t="0.035" f="48.044" m="36.4091" cg="49."/>
<eng-data t="0.065" f="24.055" m="35.653" cg="49."/>
<eng-data t="0.111" f="31.03" m="34.7673" cg="49."/>
<eng-data t="0.162" f="32.79" m="33.6296" cg="49."/>
<eng-data t="0.36" f="34.811" m="28.9508" cg="49."/>
<eng-data t="0.521" f="35.593" m="24.9886" cg="49."/>
<eng-data t="0.665" f="36.701" m="21.3496" cg="49."/>
<eng-data t="0.787" f="35.984" m="18.2499" cg="49."/>
<eng-data t="1.436" f="29.205" m="3.46104" cg="49."/>
<eng-data t="1.513" f="27.249" m="1.94154" cg="49."/>
<eng-data t="1.576" f="21.578" m="0.866273" cg="49."/>
<eng-data t="1.641" f="7.171" m="0.213066" cg="49."/>
<eng-data t="1.726" f="0." m="0." cg="49."/>
</data>
</engine>
</engine-list>
</engine-database>

44
core/resources-src/datafiles/thrustcurves/thrustcurve.org/Cesaroni_F51.rse
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@ -1,25 +1,31 @@
<engine-database>
<engine-list>
<engine mfg="CTI" code="75-F51-CL-12A" Type="unspecified" dia="24." len="133."
initWt="95." propWt="40." delays="12,9,7,5" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="47.72" peakThrust="84.148" throatDia="0." exitDia="0." Itot="75.254"
burn-time="1.58" massFrac="42.11" Isp="191.85" 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>Classic 24mm 3G
75-F51-CL-12A
</comments>
<engine mfg="CTI" code="50-F51-BS-13A" Type="unspecified" dia="24." len="101.001"
initWt="73." propWt="28." delays="13,10,8,6,4" auto-calc-mass="1"
auto-calc-cg="1" avgThrust="47.645" peakThrust="67.976" throatDia="0."
exitDia="0." Itot="49.789" burn-time="1.04" massFrac="38.36" Isp="181.32"
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 50-F51-BS-13A</comments>
<data>
<eng-data t="0." f="0." m="40." cg="66.5"/>
<eng-data t="0.02" f="75.924" m="39.5964" cg="66.5"/>
<eng-data t="0.031" f="84.148" m="39.1285" cg="66.5"/>
<eng-data t="0.062" f="70.441" m="37.8549" cg="66.5"/>
<eng-data t="0.117" f="73.659" m="35.7485" cg="66.5"/>
<eng-data t="1.211" f="38.737" m="3.06972" cg="66.5"/>
<eng-data t="1.376" f="14.779" m="0.722981" cg="66.5"/>
<eng-data t="1.456" f="7.271" m="0.254171" cg="66.5"/>
<eng-data t="1.532" f="3.337" m="0.0399086" cg="66.5"/>
<eng-data t="1.577" f="0." m="0." cg="66.5"/>
<eng-data t="0." f="0." m="28." cg="50.5"/>
<eng-data t="0.001" f="5.145" m="27.9986" cg="50.5"/>
<eng-data t="0.027" f="67.976" m="27.464" cg="50.5"/>
<eng-data t="0.051" f="53.807" m="26.6421" cg="50.5"/>
<eng-data t="0.06" f="52.88" m="26.3721" cg="50.5"/>
<eng-data t="0.092" f="55.916" m="25.3932" cg="50.5"/>
<eng-data t="0.119" f="57.94" m="24.5288" cg="50.5"/>
<eng-data t="0.17" f="59.711" m="22.8416" cg="50.5"/>
<eng-data t="0.3" f="61.145" m="18.4238" cg="50.5"/>
<eng-data t="0.462" f="58.952" m="12.9531" cg="50.5"/>
<eng-data t="0.569" f="55.578" m="9.50718" cg="50.5"/>
<eng-data t="0.675" f="52.205" m="6.29461" cg="50.5"/>
<eng-data t="0.778" f="46.386" m="3.43918" cg="50.5"/>
<eng-data t="0.846" f="38.12" m="1.82336" cg="50.5"/>
<eng-data t="0.917" f="20.325" m="0.656546" cg="50.5"/>
<eng-data t="1.009" f="3.542" m="0.0391239" cg="50.5"/>
<eng-data t="1.032" f="1.602" m="0.00585602" cg="50.5"/>
<eng-data t="1.045" f="0." m="0." cg="50.5"/>
</data>
</engine>
</engine-list>

26
core/resources-src/datafiles/thrustcurves/thrustcurve.org/Cesaroni_F51_1.rse Normal file
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<engine-database>
<engine-list>
<engine mfg="CTI" code="75-F51-CL-12A" Type="unspecified" dia="24." len="133."
initWt="95." propWt="40." delays="12,9,7,5" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="47.72" peakThrust="84.148" throatDia="0." exitDia="0." Itot="75.254"
burn-time="1.58" massFrac="42.11" Isp="191.85" 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>Classic 24mm 3G
75-F51-CL-12A
</comments>
<data>
<eng-data t="0." f="0." m="40." cg="66.5"/>
<eng-data t="0.02" f="75.924" m="39.5964" cg="66.5"/>
<eng-data t="0.031" f="84.148" m="39.1285" cg="66.5"/>
<eng-data t="0.062" f="70.441" m="37.8549" cg="66.5"/>
<eng-data t="0.117" f="73.659" m="35.7485" cg="66.5"/>
<eng-data t="1.211" f="38.737" m="3.06972" cg="66.5"/>
<eng-data t="1.376" f="14.779" m="0.722981" cg="66.5"/>
<eng-data t="1.456" f="7.271" m="0.254171" cg="66.5"/>
<eng-data t="1.532" f="3.337" m="0.0399086" cg="66.5"/>
<eng-data t="1.577" f="0." m="0." cg="66.5"/>
</data>
</engine>
</engine-list>
</engine-database>

27
core/resources-src/datafiles/thrustcurves/thrustcurve.org/Cesaroni_F70.rse Normal file
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@ -0,0 +1,27 @@
<engine-database>
<engine-list>
<engine mfg="CTI" code="53-F70-WT-14A" Type="unspecified" dia="24." len="101.001"
initWt="73." propWt="29." delays="14,11,9,7,5" auto-calc-mass="1"
auto-calc-cg="1" avgThrust="64.725" peakThrust="96.149" throatDia="0."
exitDia="0." Itot="52.816" burn-time="0.82" massFrac="39.73" Isp="185.71"
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 53-F70-WT-14A</comments>
<data>
<eng-data t="0." f="0." m="29." cg="50.5"/>
<eng-data t="0.001" f="8.303" m="28.9977" cg="50.5"/>
<eng-data t="0.013" f="85.68" m="28.6881" cg="50.5"/>
<eng-data t="0.023" f="96.149" m="28.1889" cg="50.5"/>
<eng-data t="0.052" f="78.821" m="26.7959" cg="50.5"/>
<eng-data t="0.1" f="83.634" m="24.655" cg="50.5"/>
<eng-data t="0.379" f="77.858" m="12.2853" cg="50.5"/>
<eng-data t="0.641" f="62.575" m="2.18404" cg="50.5"/>
<eng-data t="0.665" f="55.716" m="1.40463" cg="50.5"/>
<eng-data t="0.706" f="23.947" m="0.507928" cg="50.5"/>
<eng-data t="0.744" f="9.146" m="0.162685" cg="50.5"/>
<eng-data t="0.787" f="2.768" m="0.0220379" cg="50.5"/>
<eng-data t="0.816" f="0." m="0." cg="50.5"/>
</data>
</engine>
</engine-list>
</engine-database>

27
core/resources-src/datafiles/thrustcurves/thrustcurve.org/Cesaroni_G33.rse Normal file
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<engine-database>
<engine-list>
<engine mfg="CTI" code="143-G33-MY-9A" Type="unspecified" dia="29." len="187."
initWt="197." propWt="89." delays="9,6,4,2" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="32.122" peakThrust="62.823" throatDia="0." exitDia="0." Itot="143.298"
burn-time="4.46" massFrac="45.18" Isp="164.18" 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 143-G33-MY-9A</comments>
<data>
<eng-data t="0." f="0." m="89." cg="93.5"/>
<eng-data t="0.009" f="5.657" m="88.9842" cg="93.5"/>
<eng-data t="0.035" f="62.823" m="88.4313" cg="93.5"/>
<eng-data t="0.07" f="27.443" m="87.4502" cg="93.5"/>
<eng-data t="0.143" f="34.789" m="86.0394" cg="93.5"/>
<eng-data t="0.228" f="38.589" m="84.1025" cg="93.5"/>
<eng-data t="0.568" f="39.771" m="75.829" cg="93.5"/>
<eng-data t="1.358" f="37.66" m="56.833" cg="93.5"/>
<eng-data t="3.126" f="36.14" m="16.3141" cg="93.5"/>
<eng-data t="3.405" f="31.58" m="10.4468" cg="93.5"/>
<eng-data t="3.762" f="21.616" m="4.54931" cg="93.5"/>
<eng-data t="4.224" f="6.671" m="0.490974" cg="93.5"/>
<eng-data t="4.461" f="0." m="0." cg="93.5"/>
</data>
</engine>
</engine-list>
</engine-database>

53
core/resources-src/datafiles/thrustcurves/thrustcurve.org/Cesaroni_G69.rse
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@ -1,34 +1,27 @@
<engine-database>
<engine-list>
<engine mfg="CTI" code="G69SK" Type="unspecified" dia="38." len="126." initWt="198."
propWt="67." delays="14,11,9,7,5" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="59.043" peakThrust="91.872" throatDia="0." exitDia="0." Itot="116.255"
burn-time="1.97" massFrac="33.84" Isp="176.94" 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 Pro38-1G 117 G69SK - 14A</comments>
<data>
<eng-data t="0." f="0." m="67." cg="63."/>
<eng-data t="0.015" f="49.371" m="66.7866" cg="63."/>
<eng-data t="0.023" f="79.41" m="66.4897" cg="63."/>
<eng-data t="0.035" f="91.872" m="65.8974" cg="63."/>
<eng-data t="0.064" f="82.605" m="64.4394" cg="63."/>
<eng-data t="0.099" f="52.407" m="63.0777" cg="63."/>
<eng-data t="0.166" f="57.041" m="60.9647" cg="63."/>
<eng-data t="0.228" f="59.278" m="58.8865" cg="63."/>
<eng-data t="0.375" f="64.231" m="53.6548" cg="63."/>
<eng-data t="1.297" f="69.024" m="18.2513" cg="63."/>
<eng-data t="1.453" f="68.864" m="12.0528" cg="63."/>
<eng-data t="1.533" f="67.746" m="8.90358" cg="63."/>
<eng-data t="1.589" f="65.189" m="6.75842" cg="63."/>
<eng-data t="1.686" f="58.639" m="3.29726" cg="63."/>
<eng-data t="1.735" f="42.821" m="1.86466" cg="63."/>
<eng-data t="1.781" f="26.363" m="0.947608" cg="63."/>
<eng-data t="1.816" f="13.901" m="0.541523" cg="63."/>
<eng-data t="1.89" f="5.432" m="0.129271" cg="63."/>
<eng-data t="1.954" f="1.278" m="0.005524" cg="63."/>
<eng-data t="1.969" f="0." m="0." cg="63."/>
</data>
</engine>
<engine mfg="Cesaroni Technology Inc." code="G69-Classic" Type="reloadable" dia="38."
len="127." initWt="205.1" propWt="84." delays="3,5,7,9,12" auto-calc-mass="1"
auto-calc-cg="1" avgThrust="68.911" peakThrust="84.5" throatDia="0." exitDia="0."
Itot="132.997" burn-time="1.93" massFrac="40.96" Isp="161.45" 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>Replaced by G46-Classic</comments>
<data>
<eng-data t="0." f="0." m="84." cg="63.5"/>
<eng-data t="0.06" f="80.77" m="82.4696" cg="63.5"/>
<eng-data t="0.2" f="84.5" m="75.1628" cg="63.5"/>
<eng-data t="0.41" f="82.74" m="64.0719" cg="63.5"/>
<eng-data t="0.59" f="80.11" m="54.815" cg="63.5"/>
<eng-data t="0.81" f="76.82" m="43.9122" cg="63.5"/>
<eng-data t="1." f="72.87" m="34.9307" cg="63.5"/>
<eng-data t="1.2" f="68.92" m="25.9753" cg="63.5"/>
<eng-data t="1.4" f="64.31" m="17.5606" cg="63.5"/>
<eng-data t="1.61" f="59.48" m="9.35122" cg="63.5"/>
<eng-data t="1.82" f="50.92" m="2.02981" cg="63.5"/>
<eng-data t="1.9" f="21.4" m="0.202741" cg="63.5"/>
<eng-data t="1.93" f="0." m="0." cg="63.5"/>
</data>
</engine>
</engine-list>
</engine-database>

34
core/resources-src/datafiles/thrustcurves/thrustcurve.org/Cesaroni_G69SK.rse Normal file
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<engine-database>
<engine-list>
<engine mfg="CTI" code="G69SK" Type="unspecified" dia="38." len="126." initWt="198."
propWt="67." delays="14,11,9,7,5" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="59.043" peakThrust="91.872" throatDia="0." exitDia="0." Itot="116.255"
burn-time="1.97" massFrac="33.84" Isp="176.94" 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 Pro38-1G 117 G69SK - 14A</comments>
<data>
<eng-data t="0." f="0." m="67." cg="63."/>
<eng-data t="0.015" f="49.371" m="66.7866" cg="63."/>
<eng-data t="0.023" f="79.41" m="66.4897" cg="63."/>
<eng-data t="0.035" f="91.872" m="65.8974" cg="63."/>
<eng-data t="0.064" f="82.605" m="64.4394" cg="63."/>
<eng-data t="0.099" f="52.407" m="63.0777" cg="63."/>
<eng-data t="0.166" f="57.041" m="60.9647" cg="63."/>
<eng-data t="0.228" f="59.278" m="58.8865" cg="63."/>
<eng-data t="0.375" f="64.231" m="53.6548" cg="63."/>
<eng-data t="1.297" f="69.024" m="18.2513" cg="63."/>
<eng-data t="1.453" f="68.864" m="12.0528" cg="63."/>
<eng-data t="1.533" f="67.746" m="8.90358" cg="63."/>
<eng-data t="1.589" f="65.189" m="6.75842" cg="63."/>
<eng-data t="1.686" f="58.639" m="3.29726" cg="63."/>
<eng-data t="1.735" f="42.821" m="1.86466" cg="63."/>
<eng-data t="1.781" f="26.363" m="0.947608" cg="63."/>
<eng-data t="1.816" f="13.901" m="0.541523" cg="63."/>
<eng-data t="1.89" f="5.432" m="0.129271" cg="63."/>
<eng-data t="1.954" f="1.278" m="0.005524" cg="63."/>
<eng-data t="1.969" f="0." m="0." cg="63."/>
</data>
</engine>
</engine-list>
</engine-database>

27
core/resources-src/datafiles/thrustcurves/thrustcurve.org/Cesaroni_H42.rse Normal file
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<engine-database>
<engine-list>
<engine mfg="CTI" code="186-H42-MY-10A" Type="unspecified" dia="29." len="231."
initWt="242." propWt="117." delays="10,7,5,3,1" auto-calc-mass="1"
auto-calc-cg="1" avgThrust="41.861" peakThrust="82.796" throatDia="0."
exitDia="0." Itot="186.196" burn-time="4.45" massFrac="48.35" Isp="162.28"
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 186-H42-MY-10A</comments>
<data>
<eng-data t="0." f="0." m="117." cg="115.5"/>
<eng-data t="0.015" f="8.71" m="116.959" cg="115.5"/>
<eng-data t="0.035" f="82.796" m="116.384" cg="115.5"/>
<eng-data t="0.059" f="43.548" m="115.431" cg="115.5"/>
<eng-data t="0.118" f="48.387" m="113.727" cg="115.5"/>
<eng-data t="0.261" f="54.946" m="109.084" cg="115.5"/>
<eng-data t="0.391" f="55.484" m="104.574" cg="115.5"/>
<eng-data t="1.21" f="51.29" m="77.0991" cg="115.5"/>
<eng-data t="2.797" f="49.462" m="26.8629" cg="115.5"/>
<eng-data t="3.029" f="45.161" m="19.9657" cg="115.5"/>
<eng-data t="3.757" f="20.538" m="4.93855" cg="115.5"/>
<eng-data t="4.374" f="4.409" m="0.102508" cg="115.5"/>
<eng-data t="4.448" f="0." m="0." cg="115.5"/>
</data>
</engine>
</engine-list>
</engine-database>

28
core/resources-src/datafiles/thrustcurves/thrustcurve.org/Cesaroni_H53.rse Normal file
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<engine-database>
<engine-list>
<engine mfg="CTI" code="234-H53-MY-12A" Type="unspecified" dia="29." len="275.999"
initWt="286." propWt="145." delays="12,9,7,5,3" auto-calc-mass="1"
auto-calc-cg="1" avgThrust="52.43" peakThrust="101.042" throatDia="0."
exitDia="0." Itot="233.156" burn-time="4.45" massFrac="50.7" Isp="163.97"
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>CTI 234-H53-MY-12A</comments>
<data>
<eng-data t="0." f="0." m="145." cg="138."/>
<eng-data t="0.006" f="8.958" m="144.983" cg="138."/>
<eng-data t="0.027" f="101.042" m="144.265" cg="138."/>
<eng-data t="0.042" f="63.234" m="143.499" cg="138."/>
<eng-data t="0.102" f="71.006" m="140.994" cg="138."/>
<eng-data t="0.2" f="77.988" m="136.454" cg="138."/>
<eng-data t="0.362" f="79.832" m="128.504" cg="138."/>
<eng-data t="0.98" f="71.138" m="99.4923" cg="138."/>
<eng-data t="2.561" f="65.341" m="32.3973" cg="138."/>
<eng-data t="2.663" f="60.862" m="28.3946" cg="138."/>
<eng-data t="3.661" f="16.731" m="4.31518" cg="138."/>
<eng-data t="4.011" f="9.353" m="1.47638" cg="138."/>
<eng-data t="4.316" f="4.347" m="0.177073" cg="138."/>
<eng-data t="4.447" f="0." m="0." cg="138."/>
</data>
</engine>
</engine-list>
</engine-database>

29
core/resources-src/datafiles/thrustcurves/thrustcurve.org/Cesaroni_I55.rse Normal file
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<engine-database>
<engine-list>
<engine mfg="CTI" code="395-I55-MY-9A" Type="unspecified" dia="38." len="245.001"
initWt="437." propWt="243." delays="9,6,4,2" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="54.545" peakThrust="92.296" throatDia="0." exitDia="0." Itot="395.236"
burn-time="7.25" massFrac="55.61" Isp="165.86" 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 395-I55-MY-9A</comments>
<data>
<eng-data t="0." f="0." m="243." cg="122.5"/>
<eng-data t="0.009" f="10.024" m="242.972" cg="122.5"/>
<eng-data t="0.033" f="92.296" m="242.217" cg="122.5"/>
<eng-data t="0.066" f="57.669" m="240.696" cg="122.5"/>
<eng-data t="0.094" f="55.325" m="239.723" cg="122.5"/>
<eng-data t="0.222" f="64.308" m="235.016" cg="122.5"/>
<eng-data t="0.471" f="67.953" m="224.892" cg="122.5"/>
<eng-data t="2.088" f="63.266" m="159.665" cg="122.5"/>
<eng-data t="3.753" f="61.704" m="95.7005" cg="122.5"/>
<eng-data t="5.195" f="62.225" m="40.7643" cg="122.5"/>
<eng-data t="5.789" f="43.87" m="21.3911" cg="122.5"/>
<eng-data t="6.105" f="40.095" m="13.2346" cg="122.5"/>
<eng-data t="6.765" f="13.669" m="2.32632" cg="122.5"/>
<eng-data t="7.085" f="6.639" m="0.328586" cg="122.5"/>
<eng-data t="7.246" f="0." m="0." cg="122.5"/>
</data>
</engine>
</engine-list>
</engine-database>

25
core/resources-src/datafiles/thrustcurves/thrustcurve.org/Cesaroni_J145.rse Normal file
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<engine-database>
<engine-list>
<engine mfg="CTI" code="699-J145-SK-LB-19A" Type="unspecified" dia="54." len="235.999"
initWt="837." propWt="416." delays="19,17,15,13,11,9" auto-calc-mass="1"
auto-calc-cg="1" avgThrust="141.729" peakThrust="498.166" throatDia="0."
exitDia="0." Itot="700.708" burn-time="4.94" massFrac="49.7" Isp="171.76"
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 699-J145-SK-LB-19A</comments>
<data>
<eng-data t="0." f="0." m="416." cg="118."/>
<eng-data t="0.011" f="39.12" m="415.872" cg="118."/>
<eng-data t="0.018" f="498.166" m="414.756" cg="118."/>
<eng-data t="0.059" f="224.939" m="405.955" cg="118."/>
<eng-data t="0.154" f="257.335" m="392.355" cg="118."/>
<eng-data t="0.488" f="235.33" m="343.51" cg="118."/>
<eng-data t="1.881" f="180.318" m="171.638" cg="118."/>
<eng-data t="3.612" f="78.851" m="38.4685" cg="118."/>
<eng-data t="4.669" f="31.174" m="3.94679" cg="118."/>
<eng-data t="4.896" f="22.616" m="0.322243" cg="118."/>
<eng-data t="4.944" f="0." m="0." cg="118."/>
</data>
</engine>
</engine-list>
</engine-database>

27
core/resources-src/datafiles/thrustcurves/thrustcurve.org/Cesaroni_J150.rse Normal file
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<engine-database>
<engine-list>
<engine mfg="CTI" code="949-J150-MY-P" Type="unspecified" dia="38." len="499.999"
initWt="951." propWt="596." delays="0" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="146.606" peakThrust="324.576" throatDia="0." exitDia="0."
Itot="943.266" burn-time="6.43" massFrac="62.67" Isp="161.39" 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 949-J150-MY-P</comments>
<data>
<eng-data t="0." f="0." m="596." cg="250."/>
<eng-data t="0.004" f="33.051" m="595.958" cg="250."/>
<eng-data t="0.03" f="324.576" m="593.021" cg="250."/>
<eng-data t="0.12" f="248.729" m="576.72" cg="250."/>
<eng-data t="0.617" f="225." m="502.338" cg="250."/>
<eng-data t="1.385" f="201.271" m="398.912" cg="250."/>
<eng-data t="2.306" f="183.475" m="286.964" cg="250."/>
<eng-data t="3.425" f="177.119" m="159.487" cg="250."/>
<eng-data t="4.149" f="123.729" m="90.6746" cg="250."/>
<eng-data t="4.934" f="79.661" m="40.2339" cg="250."/>
<eng-data t="5.59" f="42.373" m="14.9428" cg="250."/>
<eng-data t="6.318" f="19.492" m="0.714326" cg="250."/>
<eng-data t="6.434" f="0." m="0." cg="250."/>
</data>
</engine>
</engine-list>
</engine-database>

29
core/resources-src/datafiles/thrustcurves/thrustcurve.org/Cesaroni_J94.rse Normal file
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<engine-database>
<engine-list>
<engine mfg="CTI" code="644-J94-MY-P" Type="unspecified" dia="38." len="367."
initWt="660." propWt="393." delays="0" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="93.043" peakThrust="168.646" throatDia="0." exitDia="0."
Itot="644.603" burn-time="6.93" massFrac="59.55" Isp="167.25" 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 644-J94-MY-P</comments>
<data>
<eng-data t="0." f="0." m="393." cg="183.5"/>
<eng-data t="0.005" f="19.477" m="392.97" cg="183.5"/>
<eng-data t="0.014" f="168.646" m="392.454" cg="183.5"/>
<eng-data t="0.05" f="133.967" m="389.133" cg="183.5"/>
<eng-data t="0.113" f="133.967" m="383.988" cg="183.5"/>
<eng-data t="0.203" f="146.081" m="376.304" cg="183.5"/>
<eng-data t="0.752" f="133.967" m="329.436" cg="183.5"/>
<eng-data t="1.787" f="116.865" m="250.297" cg="183.5"/>
<eng-data t="3.075" f="110.451" m="161.045" cg="183.5"/>
<eng-data t="4.236" f="108.314" m="83.6203" cg="183.5"/>
<eng-data t="4.803" f="77.672" m="51.4738" cg="183.5"/>
<eng-data t="5.474" f="56.295" m="24.0713" cg="183.5"/>
<eng-data t="6.375" f="17.577" m="3.78159" cg="183.5"/>
<eng-data t="6.879" f="6.413" m="0.0957917" cg="183.5"/>
<eng-data t="6.928" f="0." m="0." cg="183.5"/>
</data>
</engine>
</engine-list>
</engine-database>

25
core/resources-src/datafiles/thrustcurves/thrustcurve.org/Cesaroni_K520.rse Normal file
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@ -0,0 +1,25 @@
<engine-database>
<engine-list>
<engine mfg="CTI" code="1711-K520-WH-17A" Type="unspecified" dia="54." len="404."
initWt="1576." propWt="988." delays="17,15,13,11,9,7" auto-calc-mass="1"
auto-calc-cg="1" avgThrust="512.036" peakThrust="615.459" throatDia="0."
exitDia="0." Itot="1710.2" burn-time="3.34" massFrac="62.69" Isp="176.51"
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 1711-K520-WH-17A</comments>
<data>
<eng-data t="0." f="0." m="988." cg="202."/>
<eng-data t="0.007" f="121.739" m="987.754" cg="202."/>
<eng-data t="0.023" f="591.787" m="984.456" cg="202."/>
<eng-data t="0.075" f="615.459" m="966.323" cg="202."/>
<eng-data t="0.151" f="580.797" m="940.061" cg="202."/>
<eng-data t="1.629" f="568.116" m="449.559" cg="202."/>
<eng-data t="2.177" f="535.145" m="274.921" cg="202."/>
<eng-data t="2.903" f="476.812" m="62.7047" cg="202."/>
<eng-data t="2.993" f="414.251" m="39.5398" cg="202."/>
<eng-data t="3.242" f="97.222" m="2.75214" cg="202."/>
<eng-data t="3.34" f="0." m="0." cg="202."/>
</data>
</engine>
</engine-list>
</engine-database>

27
core/resources-src/datafiles/thrustcurves/thrustcurve.org/Cesaroni_K600.rse Normal file
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<engine-database>
<engine-list>
<engine mfg="CTI" code="2130-K600-WH-17A" Type="unspecified" dia="54." len="488."
initWt="1892." propWt="1238." delays="17,15,13,11,9,7" auto-calc-mass="1"
auto-calc-cg="1" avgThrust="599.274" peakThrust="785.114" throatDia="0."
exitDia="0." Itot="2118.43" burn-time="3.54" massFrac="65.43" Isp="174.49"
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 2130-K600-WH-17A</comments>
<data>
<eng-data t="0." f="0." m="1238." cg="244."/>
<eng-data t="0.002" f="97.239" m="1237.94" cg="244."/>
<eng-data t="0.007" f="785.114" m="1236.65" cg="244."/>
<eng-data t="0.03" f="741.897" m="1226.39" cg="244."/>
<eng-data t="0.101" f="745.498" m="1195.53" cg="244."/>
<eng-data t="0.148" f="731.092" m="1175.26" cg="244."/>
<eng-data t="0.455" f="699.88" m="1046.89" cg="244."/>
<eng-data t="1.711" f="669.868" m="544.194" cg="244."/>
<eng-data t="2.313" f="619.448" m="317.4" cg="244."/>
<eng-data t="2.911" f="559.424" m="111.411" cg="244."/>
<eng-data t="3.093" f="420.168" m="59.3164" cg="244."/>
<eng-data t="3.513" f="60.024" m="0.385855" cg="244."/>
<eng-data t="3.535" f="0." m="0." cg="244."/>
</data>
</engine>
</engine-list>
</engine-database>

26
core/resources-src/datafiles/thrustcurves/thrustcurve.org/Cesaroni_K711.rse Normal file
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<engine-database>
<engine-list>
<engine mfg="CTI" code="2377-K711-WH-18A" Type="unspecified" dia="54." len="572."
initWt="2198." propWt="1464." delays="18,16,14,12,10,8" auto-calc-mass="1"
auto-calc-cg="1" avgThrust="706.798" peakThrust="1702.76" throatDia="0."
exitDia="0." Itot="2374.14" burn-time="3.36" massFrac="66.61" Isp="165.37"
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 2377-K711-WH-18A</comments>
<data>
<eng-data t="0." f="0." m="1464." cg="286."/>
<eng-data t="0.002" f="239.856" m="1463.85" cg="286."/>
<eng-data t="0.003" f="1702.76" m="1463.25" cg="286."/>
<eng-data t="0.03" f="976.711" m="1440.95" cg="286."/>
<eng-data t="0.149" f="903.241" m="1371.97" cg="286."/>
<eng-data t="0.474" f="855.702" m="1195.72" cg="286."/>
<eng-data t="1.791" f="780.072" m="531.492" cg="286."/>
<eng-data t="2.397" f="721.729" m="250.891" cg="286."/>
<eng-data t="2.65" f="546.699" m="151.946" cg="286."/>
<eng-data t="2.976" f="395.438" m="57.2489" cg="286."/>
<eng-data t="3.343" f="105.882" m="0.522333" cg="286."/>
<eng-data t="3.359" f="0." m="0." cg="286."/>
</data>
</engine>
</engine-list>
</engine-database>

30
core/resources-src/datafiles/thrustcurves/thrustcurve.org/Cesaroni_L265.eng Normal file
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@ -0,0 +1,30 @@
L265 54 649 P 1.603 2.481 CTI
0.056 471
0.149 421.196
0.28 426.63
0.644 391.304
0.961 375.906
1.408 350.543
1.837 335.145
2.266 332.428
3.227 318.841
4.663 313.406
5.82 317.029
6.072 312.5
6.333 279.891
6.529 257.246
6.79 248.188
7.163 223.732
7.527 189.312
7.909 141.304
8.002 145.833
8.198 122.283
8.441 97.826
8.637 81.522
8.954 79.71
9.373 59.783
9.672 36.232
10.017 17.21
10.549 15.399
11.015 10.87
11.472 0.0

27
core/resources-src/datafiles/thrustcurves/thrustcurve.org/Cesaroni_L265.rse Normal file
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@ -0,0 +1,27 @@
<engine-database>
<engine-list>
<engine mfg="CTI" code="2645-L265-MY-P" Type="unspecified" dia="54." len="649."
initWt="2481." propWt="1644." delays="0" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="266.487" peakThrust="461.131" throatDia="0." exitDia="0."
Itot="2633.43" burn-time="9.88" massFrac="66.26" Isp="163.34" 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 2645-L265-MY-P</comments>
<data>
<eng-data t="0." f="0." m="1644." cg="324.5"/>
<eng-data t="0.007" f="30.035" m="1643.93" cg="324.5"/>
<eng-data t="0.021" f="461.131" m="1641.79" cg="324.5"/>
<eng-data t="0.188" f="425.206" m="1595.59" cg="324.5"/>
<eng-data t="0.607" f="399.882" m="1487.67" cg="324.5"/>
<eng-data t="1.353" f="354.535" m="1312." cg="324.5"/>
<eng-data t="1.939" f="336.278" m="1185.64" cg="324.5"/>
<eng-data t="3.592" f="319.199" m="847.438" cg="324.5"/>
<eng-data t="6.053" f="312.132" m="362.463" cg="324.5"/>
<eng-data t="8.09" f="133.098" m="79.372" cg="324.5"/>
<eng-data t="8.508" f="95.995" m="49.4811" cg="324.5"/>
<eng-data t="9.485" f="47.114" m="5.83836" cg="324.5"/>
<eng-data t="9.882" f="0." m="0." cg="324.5"/>
</data>
</engine>
</engine-list>
</engine-database>

16
core/resources-src/datafiles/thrustcurves/thrustcurve.org/Cesaroni_L395.eng Normal file
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@ -0,0 +1,16 @@
; CTI L395 long burn Mellow Propellant
; Not many data points.
; Made from the data in the Rocksim file below
L395 75 757 P 2.218 5.706 CTI
0.04 484.229
0.129 484.229
0.209 578.734
0.547 553.644
2.043 511.828
7.329 439.068
8.632 424.014
9.573 297.73
11.399 100.358
12.445 30.108
12.501 0
;

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