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Updated thrustcurves.

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kruland2607 2014-05-20 10:43:58 -05:00
parent b1e53e4e6b
commit 49ddd78cbc
19 changed files with 435 additions and 79 deletions
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2
core/resources-src/datafiles/thrustcurves/manual/README.txt
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@ -9,6 +9,4 @@ 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

35
core/resources-src/datafiles/thrustcurves/manual/at130702.eng
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@ -1,35 +0,0 @@
; @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

133
core/resources-src/datafiles/thrustcurves/thrustcurve.org/00INDEX.txt
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@ -1,5 +1,5 @@
Rocket motor simulation data downloaded from ThrustCurve.org.
This ZIP file contains 1600 simulator data files.
This ZIP file contains 1617 simulator data files.
For more info, please see http://www.thrustcurve.org/
AMW_I195.eng
@ -856,6 +856,13 @@ AMW_N4000.rse
Data Source: user
Contributor: John Coker
AeroTech_C3.eng
Manufacturer: AeroTech
Designation: C3.4
Data Format: RASP
Data Source: cert
Contributor: John Coker
AeroTech_D10.eng
Manufacturer: AeroTech
Designation: D10
@ -891,6 +898,13 @@ AeroTech_D15.rse
Data Source: user
Contributor: John Coker
AeroTech_D2.eng
Manufacturer: AeroTech
Designation: D2.3
Data Format: RASP
Data Source: cert
Contributor: John Coker
AeroTech_D21.eng
Manufacturer: AeroTech
Designation: D21
@ -1367,6 +1381,13 @@ AeroTech_F42.rse
Data Source: user
Contributor: John Coker
AeroTech_F44.eng
Manufacturer: AeroTech
Designation: F44W
Data Format: RASP
Data Source: mfr
Contributor: Mark Koelsch
AeroTech_F50.eng
Manufacturer: AeroTech
Designation: F50
@ -1689,6 +1710,13 @@ AeroTech_G71_1.eng
Data Source: mfr
Contributor: Edward K. Chess
AeroTech_G74.eng
Manufacturer: AeroTech
Designation: G74W
Data Format: RASP
Data Source: mfr
Contributor: Mark Koelsch
AeroTech_G75.eng
Manufacturer: AeroTech
Designation: G75J
@ -1955,6 +1983,13 @@ AeroTech_H180.rse
Data Source: user
Contributor: John Coker
AeroTech_H182.eng
Manufacturer: AeroTech
Designation: H182R-14A
Data Format: RASP
Data Source: user
Contributor: Mike Caplinger
AeroTech_H195.eng
Manufacturer: AeroTech
Designation: H195NT-10A
@ -2055,10 +2090,10 @@ AeroTech_H268.rse
AeroTech_H45.eng
Manufacturer: AeroTech
Designation: H45W
Designation: H45W-10A
Data Format: RASP
Data Source: cert
Contributor: John Coker
Data Source: user
Contributor: Mike Caplinger
AeroTech_H45.rse
Manufacturer: AeroTech
@ -2067,6 +2102,13 @@ AeroTech_H45.rse
Data Source: user
Contributor: John Coker
AeroTech_H45_1.eng
Manufacturer: AeroTech
Designation: H45W
Data Format: RASP
Data Source: cert
Contributor: John Coker
AeroTech_H55.eng
Manufacturer: AeroTech
Designation: H55W
@ -2270,6 +2312,13 @@ AeroTech_I200.rse
Data Source: user
Contributor: John Coker
AeroTech_I205.eng
Manufacturer: AeroTech
Designation: I205W-14A
Data Format: RASP
Data Source: user
Contributor: Mike Caplinger
AeroTech_I211.eng
Manufacturer: AeroTech
Designation: I211W
@ -2545,10 +2594,10 @@ AeroTech_I600.rse
AeroTech_I65.eng
Manufacturer: AeroTech
Designation: I65W
Designation: I65W-10A
Data Format: RASP
Data Source: cert
Contributor: John Coker
Data Source: user
Contributor: Mike Caplinger
AeroTech_I65.rse
Manufacturer: AeroTech
@ -2557,6 +2606,13 @@ AeroTech_I65.rse
Data Source: user
Contributor: John Coker
AeroTech_I65_1.eng
Manufacturer: AeroTech
Designation: I65W
Data Format: RASP
Data Source: cert
Contributor: John Coker
AeroTech_J125.eng
Manufacturer: AeroTech
Designation: J125W
@ -2613,6 +2669,13 @@ AeroTech_J145.rse
Data Source: user
Contributor: John Coker
AeroTech_J170.eng
Manufacturer: AeroTech
Designation: J170H 3-jet std.
Data Format: RASP
Data Source: user
Contributor: Jesus Manuel Recuenco
AeroTech_J180.eng
Manufacturer: AeroTech
Designation: J180T
@ -2795,6 +2858,13 @@ AeroTech_J420.rse
Data Source: user
Contributor: John Coker
AeroTech_J425.eng
Manufacturer: AeroTech
Designation: J425R-14A
Data Format: RASP
Data Source: user
Contributor: Mike Caplinger
AeroTech_J460.eng
Manufacturer: AeroTech
Designation: J460T
@ -3117,6 +3187,13 @@ AeroTech_K513.eng
Data Source: user
Contributor: John Coker
AeroTech_K535.eng
Manufacturer: AeroTech
Designation: K535W-14A
Data Format: RASP
Data Source: user
Contributor: Mike Caplinger
AeroTech_K540.rse
Manufacturer: AeroTech
Designation: K540M
@ -3250,6 +3327,13 @@ AeroTech_K828.rse
Data Source: cert
Contributor: Victor Merle Barlow
AeroTech_L1000.eng
Manufacturer: AeroTech
Designation: L1000W-18A
Data Format: RASP
Data Source: user
Contributor: Mike Caplinger
AeroTech_L1040.eng
Manufacturer: AeroTech
Designation: L1040DM
@ -9571,6 +9655,13 @@ GR_M1665.eng
Data Source: mfr
Contributor: John Coker
GR_O2700.eng
Manufacturer: Gorilla Rocket Motors
Designation: O2700BL
Data Format: RASP
Data Source: cert
Contributor: Mark Koelsch
Hypertek_I130.eng
Manufacturer: Hypertek
Designation: 300CC098J - I130
@ -10719,6 +10810,13 @@ PP_J140.eng
Data Source: user
Contributor: John Coker
Quest_A3.eng
Manufacturer: Quest Aerospace
Designation: A3T
Data Format: RASP
Data Source: cert
Contributor: Howard Smart
Quest_A6.eng
Manufacturer: Quest Aerospace
Designation: A6
@ -10971,6 +11069,27 @@ Roadrunner_G80.rse
Data Source: mfr
Contributor: Roadrunner Rocketry
SCR_A3.rse
Manufacturer: Southern Cross Rocketry
Designation: SCR-A8
Data Format: RockSim
Data Source: mfr
Contributor: John Coker
SCR_B4.rse
Manufacturer: Southern Cross Rocketry
Designation: SCR-B6
Data Format: RockSim
Data Source: mfr
Contributor: John Coker
SCR_C3.rse
Manufacturer: Southern Cross Rocketry
Designation: SCR-C6
Data Format: RockSim
Data Source: mfr
Contributor: John Coker
SkyR_G125.eng
Manufacturer: Sky Ripper Systems
Designation: G125

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

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

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

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

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

27
core/resources-src/datafiles/thrustcurves/thrustcurve.org/Quest_A3.eng Normal file
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@ -0,0 +1,27 @@
;Quest A3T
;File produced by Howard Smart from NAR certification thrust curve
;9 May 2014
A3T 13 55 2-4 0.0036 0.009 Q
0.0925926 0.494186
0.123457 0.988372
0.192901 2.73256
0.243056 1.51163
0.25463 1.2936
0.281636 1.13372
0.320216 1.03198
0.37037 0.901163
0.401235 0.799419
0.455247 0.843023
0.505401 0.799419
0.748457 0.784884
0.841049 0.799419
0.914352 0.65407
1.00309 0.712209
1.25386 0.625
1.50077 0.697674
1.7554 0.741279
2.00231 0.770349
2.05633 0.741279
2.07562 0.56686
2.1 0
;

22
core/resources-src/datafiles/thrustcurves/thrustcurve.org/SCR_A3.rse Normal file
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@ -0,0 +1,22 @@
<engine-database>
<engine-list>
<engine mfg="Southern Cross Rocketry" code="A8" Type="single-use" dia="18." len="70."
initWt="11.5" propWt="3." delays="3,5" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="3.338" peakThrust="8.706" throatDia="0." exitDia="0." Itot="2.46"
burn-time="0.74" massFrac="0." Isp="0." 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="0." cg="0."/>
<eng-data t="0.0806184" f="0.403361" m="0." cg="0."/>
<eng-data t="0.13915" f="1.31092" m="0." cg="0."/>
<eng-data t="0.213694" f="3.04202" m="0." cg="0."/>
<eng-data t="0.399779" f="8.70588" m="0." cg="0."/>
<eng-data t="0.581999" f="2.30252" m="0." cg="0."/>
<eng-data t="0.631143" f="1.15966" m="0." cg="0."/>
<eng-data t="0.685257" f="0.352941" m="0." cg="0."/>
<eng-data t="0.737162" f="0.0168067" m="0." cg="0."/>
</data>
</engine>
</engine-list>
</engine-database>

22
core/resources-src/datafiles/thrustcurves/thrustcurve.org/SCR_B4.rse Normal file
View File

@ -0,0 +1,22 @@
<engine-database>
<engine-list>
<engine mfg="Southern Cross Rocketry" code="B6" Type="single-use" dia="18." len="70."
initWt="14.8" propWt="6." delays="4" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="3.886" peakThrust="12.202" throatDia="0." exitDia="0." Itot="4.69"
burn-time="1.21" massFrac="40.54" Isp="79.71" tDiv="10" tStep="-1." tFix="1"
FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10"
cgStep="-1." cgFix="1">
<data>
<eng-data t="0." f="0." m="6." cg="35."/>
<eng-data t="0.3545" f="12.2017" m="3.2334" cg="35."/>
<eng-data t="0.478189" f="3.63025" m="1.98092" cg="35."/>
<eng-data t="0.51132" f="2.78992" m="1.84487" cg="35."/>
<eng-data t="0.549972" f="2.35294" m="1.71773" cg="35."/>
<eng-data t="1.00607" f="2.28571" m="0.364525" cg="35."/>
<eng-data t="1.11099" f="1.81513" m="0.0893446" cg="35."/>
<eng-data t="1.18167" f="0.10084" m="0.00273043" cg="35."/>
<eng-data t="1.20707" f="0.0672269" m="0." cg="35."/>
</data>
</engine>
</engine-list>
</engine-database>

24
core/resources-src/datafiles/thrustcurves/thrustcurve.org/SCR_C3.rse Normal file
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@ -0,0 +1,24 @@
<engine-database>
<engine-list>
<engine mfg="Southern Cross Rocketry" code="C6" Type="single-use" dia="18." len="70."
initWt="21." propWt="12." delays="0,3,5" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="3.362" peakThrust="12.283" throatDia="0." exitDia="0." Itot="9.749"
burn-time="2.9" massFrac="48." Isp="82.84" 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>
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<eng-data t="0.0993926" f="1.88406" m="11.8847" cg="35."/>
<eng-data t="0.45831" f="12.2826" m="8.75531" cg="35."/>
<eng-data t="0.516289" f="4.96377" m="8.13989" cg="35."/>
<eng-data t="0.599117" f="3.42857" m="7.71207" cg="35."/>
<eng-data t="0.770293" f="3.22689" m="7.0109" cg="35."/>
<eng-data t="0.866924" f="2.85714" m="6.64906" cg="35."/>
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<eng-data t="2.05411" f="2.89076" m="2.29043" cg="35."/>
<eng-data t="2.63114" f="2.42754" m="0.401695" cg="35."/>
<eng-data t="2.9" f="0." m="0." cg="35."/>
</data>
</engine>
</engine-list>
</engine-database>

BIN
core/resources/datafiles/thrustcurves/thrustcurves.ser
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