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enhanced motor handling, bug fixes, initial optimization code

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This commit is contained in:
Sampo Niskanen 2010-09-02 21:10:11 +00:00
parent 8b01fe131f
commit f7aa3e2d4b
662 changed files with 29826 additions and 613 deletions
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12
ChangeLog
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@ -1,3 +1,15 @@
2010-09-01 Sampo Niskanen
* [BUG] Fixed rocket config dialog being too large
2010-08-31 Sampo Niskanen
* Updated all thrust curves from thrustcurve.org
2010-08-30 Sampo Niskanen
* Implemented user-defined thrust curve loading
2010-07-30 Sampo Niskanen
* [BUG] Fixed motor statistic computation

38
TODO
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@ -7,8 +7,6 @@ Must have:
- Logging system into use
- Reduce memory footprint
- Reduce memory leakage
- Load thrust curves from external directory
- Support duplicate motor definitions
Maybe:
@ -18,9 +16,25 @@ Maybe:
Done:
In 1.1.0:
- Reading .RKT
- Central logging system
- Simulation refactoring
In 1.1.1:
- Load thrust curves from external directory
- Support duplicate motor definitions
- Combine duplicates into one display in the selection dialog
- A single manufacturer/designation can contain multiple thrust curves
- Delays are combined
- Type is selected based on any not-unknown type
- Hybrid type always includes P delay
- Default delay selected based on heuristics
- Store recently used motors, use in default selection
- Plot motor thrust curve
- Change databases and icon loading to bean instances, implement stubs
for unit tests
- Remove database etc. initialization from class initialization,
create separate set of test motors
@ -39,16 +53,7 @@ Memory usage:
Motor support:
- Combine duplicates into one display in the selection dialog
- A single manufacturer/designation can contain multiple thrust curves
- Delays are combined
- Type is selected based on any not-unknown type
- Hybrid type always includes P delay
- Default delay selected based on heuristics
- Store recently used motors, use in default selection
- Integration with thrustcurve.org (syncing?)
- Reading thrust curves from external directory
- Plot motor thrust curve
- Water rocket modeling
@ -81,6 +86,8 @@ UI issues:
- Drag and drop of components / other table items
- Ctrl+scroll wheel to zoom in/out
- Move components by dragging on the figure
- Add tool tips to component tree and figure, display component comment
- Make simulation table columns configurable
Simulation:
@ -113,17 +120,14 @@ Component support:
File support:
- Reading (and writing) SpaceCad format
- Reading (and writing?) SpaceCad format
- Writing .RKT format ?
Refactoring tasks:
- Change databases and icon loading to bean instances, implement stubs
for unit tests
- Remove database etc. initialization from class initialization,
create separate set of test motors
- Extract event rules and data saving from Simulator into listeners
- Extract event rules and data saving from Simulator into listeners?
- Change SimulationStatus to include methods for obtaining basic
position (maybe even change to an interface, implements Cloneable)

10314
datafiles/thrustcurves/00INDEX.txt Normal file
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File diff suppressed because it is too large Load Diff

29
datafiles/thrustcurves/AMW_I220.eng Normal file
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@ -0,0 +1,29 @@
;Animal Motor Works 38-390
I220SK 38 249 20 0.202 0.495 AMW
0.0050 12.747
0.019 45.25
0.036 79.666
0.052 125.554
0.069 162.519
0.076 169.53
0.095 174.629
0.167 176.541
0.229 191.199
0.447 235.175
0.602 260.668
0.733 288.073
0.85 302.095
0.974 301.457
1.094 289.985
1.184 268.954
1.268 240.273
1.302 219.879
1.388 177.178
1.418 147.224
1.435 127.467
1.473 91.139
1.504 65.645
1.543 40.789
1.593 19.12
1.622 10.197
1.65 0.0

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

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

34
datafiles/thrustcurves/AMW_I315.eng Normal file
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@ -0,0 +1,34 @@
; This file my be used or given away. All I ask is that this header
; is maintained to give credit to NAR S&T. Thank you, Jack Kane
; The total impulse, peak thrust, average thrust and burn time are
; the same as the averaged static test data on the NAR web site in
; the certification file. The curve drawn with these data points is as
; close to the certification curve as can be with such a limited
; number of points (32) allowed with wRASP up to v1.6.
;Animal Motor Works 38-640
I315SK 38 369 20 0.3829 0.7166 AMW
0.011 314.573
0.030 312.796
0.066 300.786
0.084 300.502
0.120 304.087
0.175 312.998
0.266 324.086
0.356 332.224
0.447 347.855
0.538 371.972
0.629 382.833
0.719 385.552
0.810 385.586
0.901 384.836
0.992 382.296
1.082 378.323
1.173 370.837
1.264 357.564
1.355 347.122
1.445 328.332
1.536 202.733
1.627 90.867
1.718 35.427
1.808 8.192
1.815 0.000

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

35
datafiles/thrustcurves/AMW_J357.eng Normal file
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@ -0,0 +1,35 @@
; AMW Animal Motor Works fixed by dberez 12/08/03
;
;Animal Motor Works J357 White Wolf
J357WW 54 326 0 0.5481 1.2101 AMW
0.02 129.64
0.03 205.95
0.05 265.00
0.06 316.51
0.09 326.05
0.13 314.60
0.18 301.25
0.24 299.34
0.35 312.69
0.50 326.05
0.66 333.68
0.87 345.13
1.07 358.48
1.46 383.18
1.77 398.45
1.86 400.36
1.98 402.35
2.18 398.45
2.29 390.82
2.41 369.93
2.51 354.67
2.55 352.76
2.60 347.03
2.65 335.59
2.69 310.79
2.75 249.73
2.81 175.43
2.84 108.65
2.90 53.38
2.92 20.98
2.95 0.00

25
datafiles/thrustcurves/AMW_J365.eng Normal file
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@ -0,0 +1,25 @@
;
;Animal Motor Works 54-1400
J365SK 54 403 0 0.7571 1.4593 AMW
0.029 389.731
0.123 360.219
0.218 334.200
0.376 326.150
0.534 334.217
0.692 341.669
0.850 347.676
1.007 359.408
1.165 370.043
1.323 383.343
1.481 399.248
1.639 417.477
1.797 443.735
1.955 472.683
2.112 501.668
2.270 497.077
2.428 425.371
2.586 349.017
2.744 262.068
2.902 107.073
3.060 41.821
3.157 0.000

44
datafiles/thrustcurves/AMW_J370.eng Normal file
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@ -0,0 +1,44 @@
;
;Animal Motor Works 54-1050
;AMW J370GG RASP.ENG file made from NAR data
;File produced FEB 20, 2003
;This file my be used or given away. All I ask is that this header
;is maintained to give credit to NAR S&T. Thank you, Jack Kane
;The total impulse, peak thrust, average thrust and burn time are
;the same as the averaged static test data on the NAR web site in
;the certification file. The curve drawn with these data points is as
;close to the certification curve as can be with such a limited
;number of points (32) allowed with wRASP up to v1.6.
J370GG 54 326 100 0.5983 1.2491 Animal_Motor_Works
0.008 185.496
0.024 149.516
0.063 225.273
0.087 272.647
0.122 304.829
0.158 304.829
0.273 335.212
0.431 363.796
0.573 390.381
0.707 413.168
0.877 428.459
1.019 441.852
1.126 441.852
1.224 458.46
1.284 443.951
1.386 440.153
1.572 438.454
1.651 438.554
1.813 417.765
2.022 404.673
2.141 385.883
2.212 385.883
2.255 374.59
2.299 387.882
2.362 357.599
2.401 384.184
2.421 348.204
2.457 316.122
2.559 251.758
2.697 115.635
2.753 45.624
2.82 0

34
datafiles/thrustcurves/AMW_J400.eng Normal file
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@ -0,0 +1,34 @@
;
;AMW J400 RASP.ENG file made from NAR published data
;File produced April 19, 2004
;The total impulse, peak thrust, average thrust and burn time are
;the same as the averaged static test data on the NAR web site in
;the certification file. The curve drawn with these data points is as
;close to the certification curve as can be with such a limited
;number of points (32) allowed with wRASP up to v1.6.
J400RR 54 326 100 0.558 1.2314 Animal_Motor_Works
0.043 246.55
0.06 317.381
0.081 344.709
0.107 358.372
0.15 356.06
0.201 365.204
0.308 392.532
0.568 435.734
0.863 458.339
1.094 469.24
1.209 467.18
1.466 460.148
1.705 443.972
1.923 423.275
2.132 409.411
2.303 413.831
2.402 420.563
2.47 413.831
2.517 395.445
2.543 347.421
2.568 265.238
2.598 128.198
2.615 68.801
2.632 25.398
2.66 0

27
datafiles/thrustcurves/AMW_J440.eng Normal file
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@ -0,0 +1,27 @@
;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

33
datafiles/thrustcurves/AMW_J450_1.eng Normal file
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@ -0,0 +1,33 @@
;
;Animal Motor Works J450 Super Tiger
J450ST 54 326 0 0.5331 1.1964 AMW
0.009 251.586
0.016 376.074
0.030 413.450
0.051 430.832
0.094 423.296
0.162 413.149
0.262 395.566
0.402 420.182
0.495 444.898
0.805 504.078
1.048 536.028
1.223 550.597
1.299 563.180
1.334 555.319
1.470 560.042
1.588 559.841
1.764 546.980
1.921 516.838
1.993 496.743
2.025 499.154
2.047 479.160
2.086 414.354
2.115 344.525
2.141 252.290
2.177 140.161
2.213 82.780
2.239 50.347
2.271 27.861
2.296 12.860
2.330 0.000

32
datafiles/thrustcurves/AMW_J480.eng Normal file
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@ -0,0 +1,32 @@
;
;AMW J480 RASP.ENG file made from NAR published data
;File produced April 19, 2004
;The total impulse, peak thrust, average thrust and burn time are
;the same as the averaged static test data on the NAR web site in
;the certification file. The curve drawn with these data points is as
;close to the certification curve as can be with such a limited
;number of points (32) allowed with wRASP up to v1.6.
J480BB 54 326 100 0.556 1.2131 Animal_Motor_Works
0.015 225.429
0.041 348.18
0.071 388.127
0.194 422.453
0.385 459.49
0.699 502.347
0.968 528.042
1.2 536.573
1.454 543.15
1.674 533.763
1.887 522.321
2.044 519.41
2.108 525.131
2.164 528.042
2.197 488.095
2.25 419.543
2.283 333.928
2.328 231.15
2.354 176.95
2.392 111.309
2.418 68.501
2.436 37.106
2.49 0

32
datafiles/thrustcurves/AMW_J500.eng Normal file
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@ -0,0 +1,32 @@
;
;J500ST entered by Tim Van Milligan
;For RockSim - http://www.rocksim.com
;Based on TRA Certification paperwork from 06-01-2002
;Initial Mass from Jim Robinson at AMW
;Not approved by TRA or AMW.
J500ST 38 370 20 0.3265 0.744 Animal_Motor_Works
0.006 444.822
0.025 475.651
0.04 418.397
0.053 466.843
0.059 409.589
0.071 458.035
0.077 409.589
0.1 444.822
0.127 506.481
0.204 590.16
0.25 644.992
0.3 678.244
0.34 709.073
0.402 735.498
0.445 766.327
0.516 783.944
0.6 787.335
0.637 770.732
0.68 744.306
0.76 620.989
0.859 475.651
1.00464 303.888
1.122 171.763
1.227 52.8502
1.3 0

37
datafiles/thrustcurves/AMW_K1000.eng Normal file
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@ -0,0 +1,37 @@
;
;AMW K1000 RASP.ENG file made from NAR published data
;File produced April 19, 2004
;The total impulse, peak thrust, average thrust and burn time are
;the same as the averaged static test data on the NAR web site in
;the certification file. The curve drawn with these data points is as
;close to the certification curve as can be with such a limited
;number of points (32) allowed with wRASP up to v1.6.
K1000SK 54 728 100 1.297 2.556 Animal_Motor_Works
0.019 1155.06
0.045 1426.12
0.094 1248.23
0.161 1112.99
0.239 1128.02
0.343 1113.99
0.377 1149.05
0.44 1121
0.544 1221.18
0.633 1178.11
0.674 1221.18
0.737 1193.13
0.883 1200.14
1.009 1194.13
1.057 1236.21
1.188 1137.03
1.299 1145.05
1.396 1087.94
1.516 954.104
1.631 855.228
1.717 827.077
1.777 650.061
1.848 465.932
1.93 303.141
2.023 147.463
2.083 83.879
2.132 41.484
2.18 0

39
datafiles/thrustcurves/AMW_K1075.eng Normal file
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@ -0,0 +1,39 @@
;
;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

35
datafiles/thrustcurves/AMW_K365.eng Normal file
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@ -0,0 +1,35 @@
;
;AMW K365RR RASP.ENG file made from NAR published data
;File produced April 19, 2004
;The total impulse, peak thrust, average thrust and burn time are
;the same as the averaged static test data on the NAR web site in
;the certification file. The curve drawn with these data points is as
;close to the certification curve as can be with such a limited
;number of points (32) allowed with wRASP up to v1.6.
K365RR 75 111 100 0.946 2.3456 Animal_Motor_Works
0.049 138.157
0.068 381.241
0.084 454.75
0.106 481.536
0.164 488.182
0.291 514.867
0.435 545.982
0.666 561.49
0.868 565.73
1.082 565.518
1.296 550.111
1.591 529.871
1.805 509.731
1.828 536.517
1.886 498.554
2.124 467.237
2.501 411.35
2.924 328.677
3.296 241.573
3.638 172.293
3.969 100.798
4.195 56.098
4.265 51.607
4.346 35.959
4.433 15.859
4.51 0

35
datafiles/thrustcurves/AMW_K450.eng Normal file
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@ -0,0 +1,35 @@
;
;AMW K450BB RASP.ENG file made from NAR published data
;File produced Aug 19, 2003
;This file my be used or given away. All I ask is that this header
;is maintained to give credit to NAR S&T. Thank you, Jack Kane.
;The total impulse, peak thrust, average thrust and burn time are
;the same as the averaged static test data on the NAR web site in
;the certification file. The curve drawn with these data points is as
;close to the certification curve as can be with such a limited
;number of points (32) allowed with wRASP up to v1.6.
K450BB 75 302 100 0.8816 2.8349 Animal_Motor_Works
0.03 78.903
0.045 227.9
0.064 449.955
0.069 508.417
0.094 555.187
0.151 563.956
0.362 625.442
0.562 651.85
0.825 660.62
1.134 652.254
1.453 626.147
1.793 594.296
2.113 538.958
2.458 469.106
2.798 384.538
3.165 276.686
3.201 279.609
3.325 232.94
3.51 171.757
3.732 107.65
3.861 58.018
3.959 40.55
4.036 20.149
4.11 0

36
datafiles/thrustcurves/AMW_K470.eng Normal file
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@ -0,0 +1,36 @@
;
;AMW K470ST RASP.ENG file made from Tripoli published data
;File produced May 15, 2004
;This file my be used or given away. All I ask is that this header
;is maintained to give credit to the people who produced the data.
;The total impulse, peak thrust, average thrust and burn time are
;the same as the averaged static test data on the NAR web site in
;the certification file. The curve drawn with these data points is as
;close to the certification curve as can be with such a limited
;number of points (32) allowed with wRASP up to v1.6.
K470ST 75 302 100 0.826 2.779 Animal_Motor_Works
0.028 699.309
0.039 799.337
0.09 765.845
0.157 770.311
0.258 785.941
0.41 804
0.572 794.425
0.707 794.425
0.886 792.192
0.998 783.261
1.15 752.002
1.318 709.579
1.447 655.992
1.593 595.707
1.728 522.025
1.885 444.101
2.092 354.923
2.356 270.167
2.664 187.554
2.945 131.734
3.27 78.058
3.433 55.686
3.478 48.987
3.556 28.909
3.7 0

38
datafiles/thrustcurves/AMW_K475.eng Normal file
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@ -0,0 +1,38 @@
;
;Animal Motor Works K475 RASP.ENG file made from NAR data
;File produced Feb 22, 2003
;The total impulse, peak thrust, average thrust and burn time are
;the same as the averaged static test data on the NAR web site in
;the certification file. The curve drawn with these data points is as
;close to the certification curve as can be with such a limited
;number of points (32) allowed with wRASP up to v1.6.
K475WW 54 403 100 0.7286 1.4925 Animal_Motor_Works
0.022 127.831
0.041 386.016
0.063 548.326
0.096 521.308
0.134 499.129
0.18 486.83
0.285 486.83
0.478 501.649
0.731 523.727
1.096 553.266
1.433 577.962
1.601 588.29
1.756 582.704
1.895 580.284
1.958 575.344
2.063 550.746
2.209 518.788
2.344 477.051
2.495 417.974
2.561 354.058
2.582 334.399
2.599 331.98
2.62 297.501
2.67 226.226
2.707 157.37
2.74 98.353
2.799 49.176
2.853 17.208
2.94 0

36
datafiles/thrustcurves/AMW_K500.eng Normal file
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@ -0,0 +1,36 @@
; Entered by Tim Van Milligan. Used John Coker's ThrustCurve Tracer software and
; data from NAR certification dated May 7, 2007
K500SK 75 368 100 1.1235 2.713 Animal
0.018 194.373
0.031 207.161
0.036 268.542
0.103 319.693
0.138 322.251
0.17 314.578
0.67 309.463
0.692 322.251
0.902 319.693
0.929 332.481
1.263 355.499
1.585 383.632
1.969 411.765
2.112 416.88
2.272 447.57
2.415 488.491
2.46 485.934
2.634 534.527
2.83 618.926
3.018 710.997
3.143 767.263
3.228 815.857
3.339 841.432
3.402 826.087
3.504 785.166
3.585 718.67
3.661 631.714
3.728 519.182
3.772 365.729
3.826 181.586
3.862 99.744
3.893 43.478
3.946 0.0

43
datafiles/thrustcurves/AMW_K530.eng Normal file
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@ -0,0 +1,43 @@
;
;Animal Motor Works 54-1400
;AMW K530GG RASP.ENG file made from NAR data
;File produced Feb 25, 2003
;This file my be used or given away. All I ask is that this header
;is maintained to give credit to NAR S&T. Thank you, Jack Kane
;The total impulse, peak thrust, average thrust and burn time are
;the same as the averaged static test data on the NAR web site in
;the certification file. The curve drawn with these data points is as
;close to the certification curve as can be with such a limited
;number of points (32) allowed with wRASP up to v1.6.
K530GG 54 403 1000 0.7967 1.616 Animal_Motor_Works
0.013 129.764
0.054 171.852
0.096 284.122
0.138 392.892
0.171 455.975
0.217 501.662
0.238 498.063
0.326 508.66
0.542 564.745
0.755 613.831
1.01 645.423
1.17 657.23
1.273 648.922
1.51 638.425
1.656 634.925
1.702 606.833
1.803 606.833
1.857 585.839
1.936 589.338
1.974 575.242
2.015 589.338
2.04 564.745
2.132 536.652
2.207 540.251
2.291 522.656
2.357 487.566
2.42 375.297
2.478 242.033
2.529 140.361
2.583 66.651
2.66 0

33
datafiles/thrustcurves/AMW_K555.eng Normal file
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@ -0,0 +1,33 @@
;Animal Motor Works 54-1750 K555 skidmark
;File provide by Joel Rogers of AMW
K555SK 54 492 0 0.8707 1.7343 AMW
0.063 507.328
0.144 535.181
0.226 559.826
0.308 585.793
0.389 607.239
0.471 629.034
0.553 664.586
0.634 683.688
0.716 697.625
0.798 719.618
0.879 756.521
0.961 777.700
1.043 789.004
1.124 797.934
1.206 801.689
1.288 804.331
1.369 799.414
1.451 768.014
1.533 704.469
1.614 641.709
1.696 568.727
1.778 481.013
1.859 401.614
1.941 333.897
2.023 277.226
2.104 205.009
2.186 129.425
2.268 73.717
2.349 22.380
2.368 0.000

37
datafiles/thrustcurves/AMW_K560.eng Normal file
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@ -0,0 +1,37 @@
;
;AMW K560 RASP.ENG file made from NAR published data
;File produced April 19, 2004
;The total impulse, peak thrust, average thrust and burn time are
;the same as the averaged static test data on the NAR web site in
;the certification file. The curve drawn with these data points is as
;close to the certification curve as can be with such a limited
;number of points (32) allowed with wRASP up to v1.6.
K560RR 54 430 100 0.75 1.5866 Animal_Motor_Works
0.023 229.13
0.046 415.135
0.059 485.264
0.078 512.268
0.106 525.67
0.154 523.05
0.211 528.39
0.261 536.451
0.369 560.734
0.511 587.738
0.657 603.86
0.77 612.022
1.096 625.75
1.358 620.083
1.627 612.022
1.839 603.86
2.057 590.459
2.218 598.52
2.335 609.301
2.385 601.24
2.407 585.018
2.426 533.831
2.467 385.511
2.507 283.037
2.542 164.441
2.576 67.399
2.595 29.653
2.62 0

28
datafiles/thrustcurves/AMW_K570.eng Normal file
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@ -0,0 +1,28 @@
;
;Animal Motor Works K570 White Wolf
K570WW 54 492 0 0.9146 1.8151 AMW
0.020 364.42
0.030 664.79
0.051 751.47
0.071 745.81
0.096 705.25
0.137 674.93
0.284 661.38
0.528 651.24
0.913 644.51
1.192 651.24
1.430 651.24
1.649 651.24
1.872 644.51
2.176 624.23
2.318 600.64
2.394 597.33
2.455 546.63
2.501 485.89
2.562 421.84
2.597 340.83
2.638 266.54
2.734 175.48
2.836 97.86
2.927 47.24
3.040 0.00

34
datafiles/thrustcurves/AMW_K600_1.eng Normal file
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@ -0,0 +1,34 @@
;
;Animal Motor Works K600 White Wolf
K600WW 75 368 0 1.2233 2.9129 AMW
0.010 412.229
0.029 522.21
0.059 547.215
0.083 524.8
0.122 497.305
0.181 484.852
0.333 495.113
0.690 560.464
1.195 643.548
1.400 673.833
1.420 708.799
1.508 701.427
1.591 721.551
1.782 731.712
2.017 752.035
2.174 756.816
2.257 765.2
2.502 766.44
2.727 752.931
2.918 738.187
3.143 705.91
3.408 643.847
3.603 569.131
3.692 526.793
3.745 439.426
3.799 289.596
3.883 112.272
3.922 64.862
3.971 37.437
3.995 22.474
4.070 0

31
datafiles/thrustcurves/AMW_K605.eng Normal file
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@ -0,0 +1,31 @@
;
;AMW K605 RASP.ENG file made from NAR published data
;File produced April 19, 2004
;The total impulse, peak thrust, average thrust and burn time are
;the same as the averaged static test data on the NAR web site in
;the certification file. The curve drawn with these data points is as
;close to the certification curve as can be with such a limited
;number of points (32) allowed with wRASP up to v1.6.
K605RR 75 368 100 1.231 2.7688 Animal_Motor_Works
0.03 165.845
0.053 309.12
0.077 361.916
0.142 392.042
0.527 501.412
0.988 606.905
1.515 682.37
2.101 730.593
2.355 737.58
2.692 731.289
3 712.497
3.361 671.036
3.503 663.479
3.586 659.701
3.645 633.353
3.692 573
3.734 444.838
3.775 297.785
3.828 162.066
3.864 98.015
3.905 41.471
3.95 0

38
datafiles/thrustcurves/AMW_K650.eng Normal file
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@ -0,0 +1,38 @@
; Animal Motor Works 54-1750
; AMW K650RR RASP.ENG file made from NAR published data
; File produced April 19, 2004
; This file my be used or given away. All I ask is that this header
; is maintained to give credit to NAR S&T. Thank you, Jack Kane
; The total impulse, peak thrust, average thrust and burn time are
; the same as the averaged static test data on the NAR web site in
; the certification file. The curve drawn with these data points is as
; close to the certification curve as can be with such a limited
; number of points (32) allowed with wRASP up to v1.6.
K650RR 54 492 0 0.931 1.8087 AMW
0.022 308.257
0.045 566.480
0.058 620.440
0.081 639.668
0.135 639.668
0.229 643.494
0.351 662.823
0.594 701.380
0.810 724.434
0.999 743.763
1.151 751.220
1.381 747.588
1.610 736.001
1.835 709.031
2.073 685.876
2.244 674.400
2.334 682.051
2.429 685.876
2.469 666.648
2.528 597.285
2.573 481.714
2.609 358.391
2.631 250.471
2.681 146.477
2.721 65.507
2.748 23.124
2.770 0.000

28
datafiles/thrustcurves/AMW_K670_1.eng Normal file
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@ -0,0 +1,28 @@
;
;Animal Motor Works K670 Green Gorilla
K670GG 54 492 0 1.0140 1.9145 AMW
0.016 294.05
0.035 398.577
0.086 506.292
0.153 496.428
0.264 506.093
0.461 558.108
0.722 629.553
0.983 688.044
1.116 714.051
1.193 785.795
1.409 788.784
1.737 804.56
2.074 781.41
2.195 764.87
2.226 781.211
2.277 764.77
2.398 751.517
2.440 744.941
2.468 718.834
2.484 666.521
2.525 418.107
2.551 218.818
2.573 120.768
2.595 52.143
2.620 0

36
datafiles/thrustcurves/AMW_K700.eng Normal file
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@ -0,0 +1,36 @@
;
;AMW K700 RASP.ENG file made from NAR published data
;File produced April 19, 2004
;The total impulse, peak thrust, average thrust and burn time are
;the same as the averaged static test data on the NAR web site in
;the certification file. The curve drawn with these data points is as
;close to the certification curve as can be with such a limited
;number of points (32) allowed with wRASP up to v1.6.
K700BB 54 430 100 0.754 1.4831 Animal_Motor_Works
0.014 359.559
0.022 625.425
0.03 737.756
0.047 771.505
0.082 786.516
0.106 771.505
0.144 775.233
0.272 786.516
0.477 812.71
0.693 842.632
0.97 847.06
1.283 838.904
1.516 816.438
1.706 801.427
1.779 793.972
1.811 775.233
1.841 726.573
1.873 625.425
1.909 509.367
1.95 393.208
1.982 337.093
2.035 292.16
2.073 228.489
2.111 153.535
2.155 86.137
2.193 37.446
2.24 0

35
datafiles/thrustcurves/AMW_K800.eng Normal file
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@ -0,0 +1,35 @@
; This file my be used or given away. All I ask is that this header
; is maintained to give credit to NAR S&T. Thank you, Jack Kane
; The total impulse, peak thrust, average thrust and burn time are
; the same as the averaged static test data on the NAR web site in
; the certification file. The curve drawn with these data points is as
; close to the certification curve as can be with such a limited
; number of points (32) allowed with wRASP up to v1.6.
K800BB 54 492 0 0.9140 1.7866 AMW
0.017 516.316
0.035 745.845
0.046 817.592
0.090 860.560
0.191 889.338
0.270 908.424
0.438 918.017
0.689 945.892
0.996 955.090
1.325 922.713
1.557 894.035
1.726 874.949
1.849 884.542
1.920 894.035
1.954 894.035
1.984 855.863
2.011 741.048
2.049 592.859
2.079 492.433
2.113 430.280
2.154 377.719
2.196 329.854
2.237 243.818
2.275 152.986
2.309 71.716
2.339 33.465
2.380 0.000

33
datafiles/thrustcurves/AMW_K950_1.eng Normal file
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@ -0,0 +1,33 @@
;
;Animal Motor Works K950 Super Tiger
K950ST 54 492 0 .8874 1.7949 AMW
0.011 771.836
0.025 1204.520
0.039 1083.244
0.053 1158.054
0.067 1036.364
0.085 1110.176
0.099 1022.399
0.135 982.102
0.220 968.835
0.404 1010.430
0.566 1044.343
0.701 1079.254
0.867 1106.186
0.995 1134.115
1.211 1114.166
1.313 1101.199
1.430 1067.285
1.529 1020.404
1.579 993.772
1.642 892.430
1.674 818.119
1.717 757.273
1.738 621.918
1.766 466.313
1.791 351.306
1.823 249.864
1.865 175.553
1.908 87.696
1.943 33.654
1.970 0.000

35
datafiles/thrustcurves/AMW_K975.eng Normal file
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@ -0,0 +1,35 @@
;
;Animal Motor Works K975 White Wolf
K975WW 54 728 0 1.357 2.5985 AMW
0.017 526.644
0.029 901.850
0.038 1098.918
0.046 1151.722
0.076 1112.867
0.130 1060.063
0.219 1053.089
0.336 1053.089
0.479 1059.066
0.609 1091.944
0.866 1136.778
1.046 1176.630
1.164 1175.634
1.202 1228.437
1.239 1208.511
1.315 1215.486
1.353 1267.293
1.387 1228.437
1.487 1241.389
1.538 1260.319
1.634 1290.900
1.723 1281.241
1.794 1266.297
1.836 1207.515
1.933 1049.103
1.992 851.437
2.080 666.923
2.118 640.521
2.193 462.582
2.269 212.311
2.378 119.854
2.510 0.000

33
datafiles/thrustcurves/AMW_L1060_1.eng Normal file
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@ -0,0 +1,33 @@
;
;Animal Motor Works L1060 Green Gorilla
L1060GG 75 497 0 1.9188 3.9388 AMW
0.020 258.773
0.024 368.235
0.032 328.386
0.076 427.96
0.100 567.284
0.116 751.352
0.128 791.202
0.169 816.071
0.225 816.071
0.309 875.795
0.518 985.257
0.763 1079.639
1.024 1174.519
1.308 1229.45
1.606 1288.375
1.782 1298.25
1.983 1293.369
2.256 1239.437
2.525 1184.506
2.822 1129.576
3.038 1069.651
3.111 1044.683
3.135 995.145
3.183 835.946
3.239 552.303
3.299 268.661
3.327 164.193
3.339 84.593
3.360 44.783
3.400 0

35
datafiles/thrustcurves/AMW_L1080.eng Normal file
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@ -0,0 +1,35 @@
;
;AMW L1080 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.
L1080BB 75 497 100 1.717 3.5922 Animal_Motor_Works
0.024 406.295
0.043 812.489
0.052 895.202
0.088 929.641
0.314 991.55
0.626 1087.69
0.988 1163.44
1.346 1218.99
1.638 1246.25
1.864 1257.91
2.247 1254.84
2.6 1218.99
2.766 1211.92
2.851 1197.78
2.942 1204.85
3.002 1226.06
3.033 1204.85
3.089 1040.23
3.124 874.499
3.15 660.999
3.191 461.336
3.232 275.408
3.268 144.622
3.303 75.744
3.339 41.316
3.39 0

26
datafiles/thrustcurves/AMW_L1111.eng Normal file
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@ -0,0 +1,26 @@
;
;L1111ST entered by Tim Van Milligan
;For RockSim - http://www.rocksim.com
;Based on TRA Certification paperwork from 06-01-2002
;Initial Mass from Jim Robinson at AMW
;Not approved by TRA or AMW.
L1111ST 75 497 100 1.642 3.517 Animal_Motor_Works
0.015 1023.97
0.1 924.878
0.147 902.857
0.502 1034.98
0.75 1156.1
1.005 1266.2
1.229 1354.29
1.492 1398.33
1.739 1398.33
2.009 1354.29
2.272 1244.18
2.504 1123.07
2.728 968.92
2.782 902.857
2.836 770.732
2.98 363.345
3.053 99.094
3.083 22.021
3.14 0

35
datafiles/thrustcurves/AMW_L1300.eng Normal file
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@ -0,0 +1,35 @@
;
;AMW L1300 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.
L1300BB 75 728 100 1.314 2.5454 Animal_Motor_Works
0.014 710.467
0.025 1247.64
0.039 1384.13
0.053 1447.83
0.074 1420.53
0.12 1447.83
0.276 1474.12
0.475 1519.61
0.712 1555
0.942 1586.74
1.147 1562.08
1.36 1534.78
1.484 1551.97
1.537 1551.97
1.569 1497.37
1.59 1406.38
1.604 1451.87
1.615 1333.58
1.64 1168.78
1.689 986.687
1.753 767.749
1.824 512.503
1.891 275.512
1.933 147.816
1.987 74.737
2.06 0

35
datafiles/thrustcurves/AMW_L1400.eng Normal file
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@ -0,0 +1,35 @@
; @File: SK-75-6000.txt, @Pts-I: 3609, @Pts-O: 31, @Sm: 6, @CO: 5%
; @TI: 4740.56, @TIa: 4732.91, @TIe: 0.0%, @ThMax: 1908.398, @ThAvg: 1382.678, @Tb: 3.423
; Exported using ThrustCurveTool, www.ThrustGear.com, by John DeMar
L1400SK 75 785 P 2.8267 5.1985 AMW
0.0 68.1234
0.0040 193.7893
0.016 690.259
0.021 814.579
0.027 900.741
0.045 997.475
0.076 1251.156
0.092 1354.553
0.107 1405.971
0.132 1440.082
0.169 1453.774
0.368 1397.446
0.525 1411.875
0.705 1488.288
1.082 1734.489
1.414 1906.629
1.556 1875.238
1.766 1882.261
1.899 1803.008
2.142 1745.497
2.34 1659.082
2.504 1522.458
2.58 1402.287
2.819 844.839
2.847 841.674
2.893 730.795
3.068 406.536
3.176 265.8
3.425 94.9644
3.608 0.874524
3.609 0

34
datafiles/thrustcurves/AMW_L666.eng Normal file
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@ -0,0 +1,34 @@
;Animal Motor Works 75-3500
L666SK 75 497 0 1.8877 3.5344 AMW
0.096 105.880
0.175 509.783
0.312 549.481
0.449 577.319
0.586 602.900
0.722 615.605
0.859 632.540
0.996 652.072
1.133 671.418
1.270 685.671
1.407 701.286
1.543 718.069
1.680 734.116
1.817 753.292
1.954 771.589
2.091 790.453
2.228 819.222
2.364 846.663
2.501 874.629
2.638 890.083
2.775 898.271
2.912 899.312
3.049 881.683
3.185 845.157
3.322 768.451
3.459 672.771
3.596 525.466
3.733 304.694
3.870 86.663
3.968 0.000
;
;

29
datafiles/thrustcurves/AMW_L700.eng Normal file
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@ -0,0 +1,29 @@
;
;
L700BB 75.0 368.00 100 1.19310 2.73200 AMW
0.02 221.87
0.03 399.33
0.05 467.56
0.08 494.89
0.13 498.41
0.24 535.99
0.48 614.67
0.77 683.20
1.23 755.25
1.62 789.72
1.92 810.42
2.26 821.14
2.58 817.85
2.91 801.07
3.14 773.94
3.25 750.13
3.32 743.39
3.37 729.83
3.42 688.83
3.46 593.37
3.50 484.14
3.53 368.18
3.57 248.80
3.62 149.82
3.66 61.13
3.72 0.00

34
datafiles/thrustcurves/AMW_L777_1.eng Normal file
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;
;Animal Motor Works L777 White Wolf
L777WW 75 497 0 1.7623 3.6987 AMW
0.025 140.882
0.064 209.474
0.108 360.055
0.204 652.185
0.360 641.518
0.373 693.745
0.418 683.28
0.528 730.073
0.670 761.268
0.761 781.998
0.787 802.828
0.871 802.728
1.065 854.754
1.338 911.811
1.668 963.636
1.914 989.498
2.115 1000.16
2.368 962.831
2.647 926
2.985 878.603
3.303 805.143
3.472 752.815
3.550 705.72
3.602 648.26
3.647 611.631
3.693 512.409
3.779 334.897
3.857 178.216
3.935 89.379
3.981 26.687
4.050 0

37
datafiles/thrustcurves/AMW_L900.eng Normal file
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@ -0,0 +1,37 @@
;
;AMW L900 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.
L900RR 75 497 100 1.771 3.5888 Animal_Motor_Works
0.029 464.292
0.053 630.937
0.059 684.506
0.096 702.328
0.133 696.387
0.201 714.311
0.486 803.524
0.777 910.661
1.099 988.093
1.26 1041.16
1.284 1071.37
1.378 1053.24
1.607 1101.57
1.917 1142.86
2.208 1173.56
2.413 1160.98
2.624 1107.62
2.866 976.211
3.053 886.897
3.208 839.27
3.314 827.388
3.382 809.465
3.432 720.252
3.495 547.564
3.57 345.273
3.627 214.273
3.714 77.382
3.79 0

21
datafiles/thrustcurves/AMW_M1350.eng Normal file
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@ -0,0 +1,21 @@
;
;Animal Motor Works M1350 White Wolf
M1350WW 75 781 0 2.92700 5.40300 AMW
0.03 1197.771588
0.04 1465.181058
0.07 1660.167131
0.09 1665.738162
0.16 1587.743733
0.45 1587.743733
0.61 1576.601671
1.86 1649.02507
2.27 1643.454039
2.64 1598.885794
3.18 1504.178273
3.29 1353.760446
3.41 991.643454
3.49 841.2256267
3.62 646.2395543
3.74 428.9693593
3.90 373.2590529
4.22 0

37
datafiles/thrustcurves/AMW_M1480.eng Normal file
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@ -0,0 +1,37 @@
;
;AMW M1480 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.
M1480RR 75 785 100 3 5.5248 Animal_Motor_Works
0.022 713.002
0.032 1254.68
0.055 1473.37
0.078 1569.11
0.156 1569.11
0.352 1559.03
0.642 1597.33
0.974 1644.69
1.289 1702.13
1.52 1739.42
1.918 1796.87
2.279 1814.83
2.481 1796.87
2.707 1739.42
2.968 1644.69
3.058 1616.47
3.135 1520.73
3.218 1378.64
3.284 1217.39
3.332 1065.22
3.344 1140.8
3.368 1016.85
3.41 741.522
3.5 522.935
3.613 275.727
3.691 171.12
3.768 66.553
3.85 0

36
datafiles/thrustcurves/AMW_M1730.eng Normal file
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@ -0,0 +1,36 @@
;
;Animal Motor Works 98-11000
M1730SK 98 870 0 4.9452 9.8718 AMW
0.040 682.642
0.064 1153.387
0.221 1354.665
0.269 1414.771
0.381 1458.026
0.541 1526.924
0.701 1589.200
0.861 1675.203
1.021 1732.669
1.181 1802.227
1.341 1886.644
1.500 1973.713
1.660 2070.514
1.820 2183.822
1.980 2299.313
2.140 2433.862
2.300 2568.119
2.460 2679.423
2.620 2638.376
2.780 2484.185
2.940 2306.038
3.099 2173.849
3.259 2074.688
3.419 1961.303
3.579 1807.810
3.739 1640.258
3.899 1303.035
4.059 940.600
4.219 567.152
4.379 309.143
4.539 188.981
4.637 0.000
;

18
datafiles/thrustcurves/AMW_M1850.eng Normal file
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@ -0,0 +1,18 @@
;
; Animal Motor Works M1850GG
; estimated from TRA graph by John DeMar jsdemar@syr.edu
; motor mass is a guess based on similar types
M1850GG 75 781 0 3.3750 4.5000 AMW
0.08 979.00
0.13 1180.00
0.28 1290.00
0.33 1468.00
0.73 1936.00
1.33 2202.00
1.73 2279.00
2.58 2105.00
2.83 2007.00
2.88 1860.00
3.08 538.00
3.20 174.00
3.30 0.00

30
datafiles/thrustcurves/AMW_M1850_1.eng Normal file
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@ -0,0 +1,30 @@
;
;Animal Motor Works M1850 Green Gorilla
M1850GG 75 781 0 3.37000 5.85100 AMW
0.12 1201.01994
0.25 1321.121934
0.37 1579.11881
0.50 1699.220804
0.62 1846.01213
0.75 1930.528348
0.87 1997.251678
1.00 2059.526786
1.12 2126.250116
1.25 2192.973446
1.37 2224.111
1.50 2246.35211
1.62 2268.59322
1.75 2277.489664
1.87 2268.59322
2.00 2246.35211
2.12 2224.111
2.25 2192.973446
2.37 2166.284114
2.50 2144.043004
2.62 2099.560784
2.75 2046.18212
2.87 1912.73546
3.00 831.817514
3.12 311.37554
3.25 84.516218
3.3 0.000

38
datafiles/thrustcurves/AMW_M1900.eng Normal file
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@ -0,0 +1,38 @@
;
;AMW M1900 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.
M1900BB 75 785 100 2.733 5.4225 Animal_Motor_Works
0.018 1109.21
0.044 1761.75
0.061 1910.65
0.085 1938.62
0.159 1929.63
0.29 1956.62
0.409 2031.56
0.438 1974.6
0.569 2011.58
0.815 2104.51
1.073 2197.44
1.401 2280.39
1.688 2324.7
1.905 2297.37
2.073 2241.41
2.254 2138.49
2.397 2063.54
2.479 2016.57
2.54 2025.57
2.581 2006.58
2.63 1885.67
2.716 1493.94
2.805 1120.21
2.887 840.605
2.972 569.996
3.046 299.488
3.119 150.193
3.168 56.829
3.23 0

33
datafiles/thrustcurves/AMW_M2500.eng Normal file
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@ -0,0 +1,33 @@
;
;Animal Motor Works M2500 Green Gorilla
M2500GG 75 1039 0 4.248 7.5515 AMW
0.026 1288.791
0.053 2021.398
0.079 2140.011
0.123 2105.125
0.207 2117.086
0.540 2309.458
0.971 2560.637
1.265 2727.094
1.480 2836.736
1.678 2920.462
1.757 2980.267
1.946 2995.51
2.047 2959.335
2.240 2889.563
2.310 2854.677
2.486 2820.788
2.526 2880.593
2.592 2773.941
2.653 2821.785
2.706 2752.012
2.758 2752.012
2.807 2763.973
2.842 2504.82
2.886 2115.092
2.930 1630.674
2.987 1051.565
3.040 437.571
3.057 284.072
3.079 142.434
3.110 0

32
datafiles/thrustcurves/AMW_M3000.eng Normal file
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@ -0,0 +1,32 @@
;
; Animal Motor Works M3000ST
; estimated from TRA graph by Rob Bazinet rbazinet66@hotmail.com
; motor mass is a guess based on similar types
M3000ST 75 1038 0 3.8190 6.72 AMW
0.032 2494.225
0.113 2621.05
0.242 2705.6
0.355 2811.288
0.435 2895.838
0.5 2959.25
0.645 3128.35
0.75 3297.45
0.871 3382
0.968 3551.1
1.032 3656.788
1.145 3804.75
1.355 3973.85
1.452 4037.263
1.629 4079.538
1.742 4142.95
1.903 4185.225
1.935 3847.025
2.081 3424.275
2.129 2959.25
2.177 2536.5
2.194 2113.75
2.226 1691
2.274 1268.25
2.323 845.5
2.403 422.75
2.5 0

35
datafiles/thrustcurves/AMW_N2020.eng Normal file
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@ -0,0 +1,35 @@
;
;Animal Motor Works 98-11000
N2020WT 98 870 0 5.1609 9.9693 AMW
.106 1941.344
0.221 2151.149
0.381 2253.406
0.541 2340.792
0.701 2400.847
0.861 2453.821
1.021 2506.314
1.181 2556.306
1.341 2607.251
1.500 2652.790
1.660 2688.660
1.820 2710.675
1.980 2729.797
2.140 2733.895
2.300 2704.255
2.460 2634.582
2.620 2532.160
2.780 2433.380
2.940 2329.740
3.099 2234.246
3.259 2165.804
3.419 2099.684
3.579 2028.350
3.739 1951.013
3.899 1871.316
4.059 1558.113
4.219 1053.376
4.379 890.506
4.539 636.689
4.998 0.000
;

26
datafiles/thrustcurves/AMW_N2600.eng Normal file
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@ -0,0 +1,26 @@
;
;Animal Motor Works 98-11000
N2600GG 98 870 1000 4.8812 10.4726 Animal_Motor_Works
0.024 1674.37
0.064 1949.62
0.104 2039.52
0.306 2189.98
0.508 2334.45
0.709 2491.23
0.911 2668.93
1.113 2874.7
1.314 3038.83
1.516 3191.29
1.718 3266.01
1.92 3318.98
2.121 3336.18
2.323 3229.26
2.525 3089.68
2.726 2943.98
2.928 2847.69
3.13 2751.68
3.331 2682.22
3.533 2463.48
3.735 1339.63
3.937 269.834
4.034 0

26
datafiles/thrustcurves/AMW_N2700.eng Normal file
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@ -0,0 +1,26 @@
;
;Animal Motor Works 98-11000
N2700BB 98 870 1000 4.7837 9.9308 Animal_Motor_Works
0.027 2229.53
0.069 2476.18
0.111 2539.74
0.36 2723.21
0.527 2863.83
0.735 3016.48
0.943 3141.25
1.151 3241.72
1.359 3335.56
1.567 3519.92
1.775 3425.88
1.983 3420.56
2.191 3356.08
2.399 3270.48
2.607 3182.6
2.815 3098.31
3.023 3002.95
3.231 2888.73
3.439 2266.61
3.647 1498.26
3.855 780.04
4.063 233.545
4.16 0

28
datafiles/thrustcurves/AMW_N4000.eng Normal file
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@ -0,0 +1,28 @@
;
;Animal Motor Works 98-17500
N4000BB 98 1213 0 6.1026 13.6683 AMW
0.029 4207.591
0.071 4709.549
0.113 4906.310
0.155 5007.780
0.239 5041.557
0.323 4993.595
0.534 5046.912
0.744 5145.819
0.954 5248.063
1.165 5293.196
1.375 5232.456
1.585 5209.528
1.796 5165.473
2.006 5047.698
2.216 4913.086
2.427 4783.447
2.637 4659.163
2.847 4195.994
3.058 2850.731
3.268 1981.973
3.478 1295.536
3.689 907.699
3.899 490.196
4.110 316.338
4.207 0.000

13
datafiles/thrustcurves/AeroTech_E11.eng Normal file
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@ -0,0 +1,13 @@
;
;Based On NAR Test Data
;12/23/93
E11J 24 70 4 0.025 0.0624 Aerotech
0.0725446 14.3704
0.16183 17.6296
0.206473 18.3704
0.418527 19.2593
0.731027 18.3704
1.31696 14.2222
1.91964 9.03704
2.51116 2.22222
2.83 0

42
datafiles/thrustcurves/AeroTech_E12.eng Normal file
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@ -0,0 +1,42 @@
;
;
;Aerotech E12JRC 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.
E12JRC 24 70 100 0.0303 0.0594 AT
0.054 16.764
0.095 18.33
0.197 16.545
0.313 16.654
0.36 17.211
0.401 16.316
0.442 17.55
0.476 16.206
0.578 16.316
0.666 16.764
0.7 15.649
0.768 16.316
0.89 16.097
1.019 15.649
1.162 14.983
1.23 14.983
1.25 13.968
1.291 14.754
1.332 13.749
1.373 14.197
1.434 13.53
1.488 13.749
1.597 12.635
1.726 11.401
1.828 10.615
1.889 9.613
1.957 9.613
1.998 8.495
2.093 8.607
2.277 7.042
2.487 5.813
3.05 0

41
datafiles/thrustcurves/AeroTech_E15_1.eng Normal file
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@ -0,0 +1,41 @@
; Aerotech E15 RASP.ENG file made from NAR published data
; File produced July 4, 2000
; Submitted to ThrustCurve.org by Chris Kobel (3/30/07)
; 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.
E15W 24 70 4-7 .0201 .0501 AT
0.020 23.330
0.036 27.318
0.058 28.840
0.079 27.171
0.139 25.638
0.183 24.263
0.237 24.106
0.297 22.426
0.373 21.964
0.400 20.894
0.443 21.355
0.487 20.442
0.617 19.833
0.742 18.457
0.812 20.000
0.850 18.006
0.899 18.467
1.035 17.711
1.100 16.945
1.160 16.945
1.377 15.736
1.426 14.656
1.436 16.198
1.463 14.813
1.550 14.361
1.572 15.432
1.610 13.752
1.827 12.839
2.126 10.098
2.337 6.116
2.538 1.369
2.600 0.000

34
datafiles/thrustcurves/AeroTech_E7.eng Normal file
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@ -0,0 +1,34 @@
;
;Aerotech E7TRC 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.
E7RC 24 70 100 0.0171 0.0484 AT
0.038 6.636
0.063 10.056
0.087 11.019
0.134 11.42
0.206 11.58
0.312 11.149
0.466 10.738
0.667 9.777
0.94 8.132
1.223 6.281
1.484 5.182
1.709 4.701
2.112 4.423
2.776 4.279
3.31 4.205
3.926 4.266
4.401 4.192
4.638 4.258
4.744 4.119
5.124 3.979
5.219 3.977
5.266 3.156
5.313 1.992
5.36 0.965
5.43 0

38
datafiles/thrustcurves/AeroTech_F13.eng Normal file
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@ -0,0 +1,38 @@
;
;Aerotech F13RCJ 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.
F13RCJ 32 107 100 0.0323 0.1105 AT
0.048 15.309
0.084 18.629
0.143 19.98
0.311 18.968
0.538 18.172
0.729 17.138
0.992 15.428
1.279 13.828
1.673 12.456
1.984 11.879
2.044 12.227
2.139 11.313
2.378 11.193
2.51 11.084
2.558 12.108
2.641 10.855
2.976 10.736
3.49 10.627
3.873 10.507
3.992 10.965
4.028 10.627
4.41 10.507
4.625 10.736
4.769 9.941
4.829 8.684
4.865 6.742
4.96 3.199
5.02 1.485
5.1 0

41
datafiles/thrustcurves/AeroTech_F16.eng Normal file
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@ -0,0 +1,41 @@
;
;Aerotech F16RCJ 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.
F16RCJ 32 107 100 0.0625 0.1404 AT
0.046 26.35
0.116 22.388
0.139 21.374
0.185 21.886
0.22 20.54
0.301 19.696
0.498 18.35
0.579 19.194
0.637 16.492
0.718 18.35
0.834 18.35
0.95 18.35
1.054 19.194
1.147 17.848
1.181 18.853
1.263 17.336
1.436 18.009
1.633 17.165
1.784 17.336
1.865 18.682
1.934 16.834
1.981 17.336
2.178 16.332
2.375 16.332
2.502 18.18
2.664 15.659
2.896 15.488
3.29 13.8
3.718 11.611
4.181 9.426
4.888 5.891
5.69 0

35
datafiles/thrustcurves/AeroTech_F20.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

38
datafiles/thrustcurves/AeroTech_F22.eng Normal file
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@ -0,0 +1,38 @@
;
;Aerotech F22 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.
F22 29 125 4-7 0.0463 0.1342 AT
0.014 11.527
0.075 20.126
0.157 26.572
0.293 29.113
0.382 30.278
0.45 29.69
0.539 30.667
0.614 30.089
0.662 31.15
0.771 30.478
0.948 29.89
0.996 28.714
1.078 28.136
1.187 27.738
1.289 26.761
1.337 26.96
1.412 25.984
1.474 25.008
1.515 26.173
1.542 24.808
1.706 22.856
1.938 20.903
2.101 18.173
2.129 19.338
2.251 16.21
2.402 13.48
2.64 8.791
2.961 3.32
3.31 0

36
datafiles/thrustcurves/AeroTech_F23.eng Normal file
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@ -0,0 +1,36 @@
;
;F23FJ Motor Thrust Curve created by Tim Van Milligan
;for RockSim Users - www.rocksim.com
;file produced March 2, 2005
;Based on data supplied by Aerotech for the newer molded case F23 econojet.
F23FJ 29 83 4-7 0.033 0.0839 AeroTech
0.03 48.7
0.05 43.11
0.08 41.41
0.1 42.26
0.13 40.84
0.17 39.42
0.23 38.85
0.27 38.85
0.3 37.44
0.31 38.57
0.36 37.72
0.43 36.59
0.5 36.02
0.56 36.02
0.59 34.6
0.69 33.18
0.77 32.61
0.85 31.2
0.94 29.5
1.04 27.79
1.18 24.39
1.2 25.24
1.25 22.97
1.37 20.98
1.53 16.73
1.69 12.48
1.83 9.07
1.95 5.11
2.07 2.27
2.22 0

41
datafiles/thrustcurves/AeroTech_F23_1.eng Normal file
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@ -0,0 +1,41 @@
;
;Aerotech F23RCWSK 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.
F23-RC-SK 32 107 100 0.0378 0.1287 AT
0.042 22.644
0.133 28.191
0.161 27.261
0.189 29.57
0.252 31.419
0.343 32.578
0.399 32.348
0.441 33.737
0.476 30.729
0.539 33.507
0.609 34.197
0.777 34.886
0.826 34.656
0.896 36
0.938 34.656
1.015 34.656
1.071 34.197
1.12 33.038
1.218 32.578
1.267 29.81
1.351 29.34
1.393 27.731
1.54 26.802
1.645 24.263
1.799 21.255
1.862 19.866
2.051 15.479
2.317 11.552
2.618 6.7
2.884 3.234
3.185 1.386
3.47 0

15
datafiles/thrustcurves/AeroTech_F25.eng Normal file
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@ -0,0 +1,15 @@
;
;F25 Motor Thrust Curve created by Tim Van Milligan
;for RockSim Users - www.rocksim.com
;file produced March 2, 2005
;Based on data supplied by Aerotech for the newer molded case F25.
F25 29 98 4-6-9 0.0388 0.0972 Aerotech
0.039 57.631
0.187 53.491
0.342 51.239
0.5 47.86
1 33.806
1.5 22.94
2 10.135
2.207 4.504
2.69 0

20
datafiles/thrustcurves/AeroTech_F26.eng Normal file
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@ -0,0 +1,20 @@
;
;F26FJ Motor Thrust Curve created by Tim Van Milligan
;for RockSim Users - www.rocksim.com
;File created March 2, 2005
;Based on data supplied by Aerotech prior to NAR certification.
F26FJ 29 98 6-9 0.0431 0.1007 Aerotech
0.041 38.289
0.114 36.318
0.293 34.347
0.497 32.939
0.774 32.376
1 31.25
1.254 28.716
1.498 25.338
1.743 22.241
2.003 17.737
2.077 15.484
2.304 5.349
2.484 1.689
2.61 0

36
datafiles/thrustcurves/AeroTech_F32.eng Normal file
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@ -0,0 +1,36 @@
; @File: F32T.txt, @Pts-I: 1501, @Pts-O: 32, @Sm: 3, @CO: 5%
; @TI: 56.7109, @TIa: 56.4715, @TIe: 0.0%, @ThMax: 58.525, @ThAvg: 34.2667, @Tb: 1.648
; Exported using ThrustCurveTool, www.ThrustGear.com
F32 24 90 4-6-8 0.0258 0.064 Aerotech/RCS
0.0 0.00669778
0.17 0.236738
0.192 0.794052
0.202 2.68628
0.204 3.57052
0.208 7.96887
0.21 11.79011
0.212 16.82641
0.22 39.2314
0.224 46.779
0.228 51.8968
0.232 55.296
0.236 56.9612
0.258 58.4048
0.288 55.2426
0.316 53.4728
0.394 49.5892
0.458 47.4002
0.73 41.2237
0.904 39.3815
1.11 35.6689
1.198 35.0946
1.22 33.8331
1.2599 33.5013
1.4779 27.3792
1.4899 27.7527
1.5099 25.4378
1.6759 11.26592
1.7679 5.94688
1.8519 2.91383
1.9519 0.745781
2.0639 0.0

40
datafiles/thrustcurves/AeroTech_F32_1.eng Normal file
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@ -0,0 +1,40 @@
;
;Aerotech F32 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.
F32 24 124 5-10-15 0.0377 0.0814 AeroTech
0.025 46.699
0.031 51.846
0.061 55.64
0.085 52.868
0.126 47.37
0.245 45.637
0.34 44.946
0.394 42.873
0.447 42.873
0.572 41.14
0.72 39.408
0.744 40.78
0.786 38.026
1.041 35.592
1.136 33.179
1.177 34.541
1.225 32.818
1.379 31.436
1.474 30.394
1.635 28.311
1.676 27.28
1.694 29.683
1.712 26.929
1.854 25.537
1.943 23.815
2.092 21.051
2.187 18.287
2.276 13.82
2.382 7.281
2.525 2.457
2.72 0

48
datafiles/thrustcurves/AeroTech_F32_1.rse Normal file
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@ -0,0 +1,48 @@
<engine-database>
<engine-list>
<engine FDiv="10" FFix="1" FStep="-1." Isp="214.23" Itot="79.202" Type="single-use" auto-calc-cg="1" auto-calc-mass="1" avgThrust="29.118" burn-time="2.72" cgDiv="10" cgFix="1" cgStep="-1." code="F32" delays="5,10,15" dia="24." exitDia="0." initWt="81.4" len="124." mDiv="10" mFix="1" mStep="-1." massFrac="46.31" mfg="Aerotech" peakThrust="55.64" propWt="37.7" tDiv="10" tFix="1" tStep="-1." throatDia="0.">
<comments>Aerotech F32 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.
</comments>
<data>
<eng-data cg="62." f="0." m="37.7" t="0."/>
<eng-data cg="62." f="46.699" m="37.4221" t="0.025"/>
<eng-data cg="62." f="51.846" m="37.2814" t="0.031"/>
<eng-data cg="62." f="55.64" m="36.514" t="0.061"/>
<eng-data cg="62." f="52.868" m="35.8942" t="0.085"/>
<eng-data cg="62." f="47.37" m="34.9161" t="0.126"/>
<eng-data cg="62." f="45.637" m="32.2819" t="0.245"/>
<eng-data cg="62." f="44.946" m="30.2339" t="0.34"/>
<eng-data cg="62." f="42.873" m="29.1052" t="0.394"/>
<eng-data cg="62." f="42.873" m="28.0236" t="0.447"/>
<eng-data cg="62." f="41.14" m="25.5243" t="0.572"/>
<eng-data cg="62." f="39.408" m="22.6871" t="0.72"/>
<eng-data cg="62." f="40.78" m="22.229" t="0.744"/>
<eng-data cg="62." f="38.026" m="21.4413" t="0.786"/>
<eng-data cg="62." f="35.592" m="16.9735" t="1.041"/>
<eng-data cg="62." f="33.179" m="15.4186" t="1.136"/>
<eng-data cg="62." f="34.541" m="14.7578" t="1.177"/>
<eng-data cg="62." f="32.818" m="13.9882" t="1.225"/>
<eng-data cg="62." f="31.436" m="11.6332" t="1.379"/>
<eng-data cg="62." f="30.394" m="10.2353" t="1.474"/>
<eng-data cg="62." f="28.311" m="7.98582" t="1.635"/>
<eng-data cg="62." f="27.28" m="7.44337" t="1.676"/>
<eng-data cg="62." f="29.683" m="7.19934" t="1.694"/>
<eng-data cg="62." f="26.929" m="6.95681" t="1.712"/>
<eng-data cg="62." f="25.537" m="5.18369" t="1.854"/>
<eng-data cg="62." f="23.815" m="4.13832" t="1.943"/>
<eng-data cg="62." f="21.051" m="2.54729" t="2.092"/>
<eng-data cg="62." f="18.287" m="1.65787" t="2.187"/>
<eng-data cg="62." f="13.82" m="0.977781" t="2.276"/>
<eng-data cg="62." f="7.281" m="0.445449" t="2.382"/>
<eng-data cg="62." f="2.457" m="0.114029" t="2.525"/>
<eng-data cg="62." f="0." m="0." t="2.72"/>
</data>
</engine>
</engine-list>
</engine-database>

31
datafiles/thrustcurves/AeroTech_F37.eng Normal file
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@ -0,0 +1,31 @@
;
;Aerotech F37 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.
F37 29 99 6-10-14 0.0282 0.1086 AT
0.018 7.251
0.053 13.626
0.088 22.331
0.106 25.227
0.141 26.385
0.183 28.411
0.26 37.685
0.31 41.449
0.422 44.035
0.524 45.183
0.59 46.47
0.682 45.153
0.864 43.386
0.934 40.471
1.042 35.23
1.151 29.699
1.246 25.037
1.354 19.796
1.445 13.397
1.498 7.586
1.54 3.226
1.6 0

31
datafiles/thrustcurves/AeroTech_F40.eng Normal file
View File

@ -0,0 +1,31 @@
;
;Aerotech F40 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.
F40 29 124 4-7-10 0.04 0.126 AT
0.015 17.776
0.049 41.016
0.089 58.793
0.124 62.9
0.148 65.173
0.183 62.442
0.242 68.07
0.292 60.617
0.321 61.524
0.415 60.617
0.524 58.334
0.741 52.412
0.87 48.314
0.889 49.221
0.914 47.397
1.102 40.109
1.285 33.728
1.492 25.064
1.665 15.952
1.808 8.659
1.942 3.19
2.06 0

17
datafiles/thrustcurves/AeroTech_F42.eng Normal file
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@ -0,0 +1,17 @@
;
;F42T Motor Thrust Curve created by Tim Van Milligan
;for RockSim Users - www.rocksim.com
;Based on data supplied by Aerotech prior to NAR certification.
F42T 29 83 4-8 0.027 0.076 Aerotech
0.01 68.694
0.029 65.879
0.202 62.5
0.511 51.802
0.739 43.356
0.993 31.532
1.02 29.279
1.072 23.086
1.199 9.572
1.262 4.505
1.319 2.815
1.47 0

18
datafiles/thrustcurves/AeroTech_F50.eng Normal file
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@ -0,0 +1,18 @@
;
;Aerotech F50 RASP.ENG file made by Tim Van Milligan
;For RockSim www.RockSim.com
;File Created March 2, 2005
;Thrust curve supplied by Aerotech for the molded case F50T motors.
F50T 29 98 4-6-9 0.0336 0.0898 AeroTech
0.013 73.762
0.0326 70.383
0.267 69.82
0.518 67.005
0.792 56.87
0.906 50.676
1 44.482
1.036 39.978
1.107 23.649
1.199 6.194
1.316 1.126
1.43 0

39
datafiles/thrustcurves/AeroTech_F52.eng Normal file
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@ -0,0 +1,39 @@
;
;Aerotech F52 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.
F52 29 124 5-8-11 0.0366 0.1214 AT
0.012 46.899
0.033 61.778
0.056 69.441
0.097 73.483
0.115 76.636
0.13 74.381
0.153 74.82
0.168 78.422
0.182 78.95
0.206 77.963
0.238 77.504
0.258 73.892
0.314 72.974
0.39 72.046
0.428 70.679
0.501 65.699
0.565 62.975
0.688 58.874
0.749 56.15
0.837 52.517
0.901 49.793
0.971 46.161
1.088 39.365
1.144 34.386
1.173 29.417
1.222 20.376
1.275 13.151
1.339 5.461
1.389 1.838
1.42 0

33
datafiles/thrustcurves/AeroTech_F62.eng Normal file
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@ -0,0 +1,33 @@
; Aerotech F62T (Blue Thunder)
;
; AeroTech RMS-29/60 Easy Access Reloadable Motor Hardware.
;
; RASP.ENG file made from manufacturers catalog data.
;
; File produced May, 17 2004.
;
; The file was produced by scaling 16 data points off
; the thrust curves in the manufacturers catalog.
;
; The F62T cannot be found on thrustcurve.org.
; Hence the amateur file production.
; The file was created by Stan Hemphill.
; Contact at stanley_hemphill@hotmail.com.
;
; Motor Dia Len Delay Prop Gross Mfg
F62T 29 99 6-8-9-10-11-13-14-16-18 0.025 0.109 AT
0.0046 053.6364
0.0416 055.2727
0.0909 058.3636
0.1356 061.6364
0.1649 064.9091
0.1864 067.6364
0.5085 067.6364
0.5701 064.7273
0.6687 060.0000
0.7427 055.0909
0.7982 049.6364
0.9029 048.7273
0.9492 024.7273
0.9661 020.1818
0.9985 000.0000

41
datafiles/thrustcurves/AeroTech_F72.eng Normal file
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@ -0,0 +1,41 @@
;
;Aerotech F72 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.
F72 24 124 5-10-15 0.0368 0.0742 AeroTech
0.012 62.586
0.017 84.986
0.02 98.78
0.03 94.748
0.05 90.152
0.069 82.688
0.089 85.556
0.104 80.39
0.136 83.255
0.146 80.96
0.176 82.688
0.198 78.672
0.213 80.96
0.253 80.39
0.315 80.96
0.38 79.821
0.429 79.241
0.489 78.092
0.523 78.672
0.536 75.225
0.675 73.496
0.699 67.182
0.719 68.331
0.747 64.884
0.769 66.033
0.858 60.867
0.923 52.824
0.98 40.195
1.012 29.864
1.034 20.092
1.089 11.48
1.21 0

45
datafiles/thrustcurves/AeroTech_G104.eng Normal file
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@ -0,0 +1,45 @@
;
; Aerotech G104T (Blue Thunder)
;
; AeroTech RMS-29/100 EZ Access Reloadable Motors.
;
; File produced 28 Feb 2005.
;
; The file was produced by scaling data points off the
; thrust curve in the manufacturers catalog sheet.
;
; The motor is not yet on www.thrustcurve.org.
; Hence the amateur file production.
; The file was created by Stan Hemphill.
; Contact at stanley_hemphill@hotmail.com.
;
; Motor Dia Len Delay Prop Gross Mfg
G104T 29 124 6-8-9-10-11-13-14-16-18 0.0408 0.136 AT
0.0067 125.3426
0.0471 123.5424
0.0856 121.9671
0.1019 121.4046
0.1462 121.1795
0.1837 120.8420
0.2029 120.5044
0.2385 118.8167
0.2644 117.2415
0.2798 116.9039
0.3279 116.6789
0.3923 116.6789
0.4298 116.1163
0.4615 114.0910
0.5067 110.1530
0.5404 104.6397
0.5760 096.2010
0.6067 089.5626
0.6817 078.8736
0.7692 067.9595
0.7865 064.9216
0.7990 062.5588
0.8058 058.0582
0.8192 050.5196
0.8385 039.0430
0.8625 027.5664
0.8769 016.6523
0.9019 000.0000

33
datafiles/thrustcurves/AeroTech_G12.eng Normal file
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@ -0,0 +1,33 @@
;
;Aerotech G12RC 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.
G12RC 32 107 100 0.0511 0.131 AT
0.03 18.549
0.117 19.96
0.239 20.64
0.362 20.111
0.519 18.982
0.694 17.138
0.886 15.02
1.131 13.186
1.375 11.915
1.689 11.069
2.021 10.363
2.422 10.232
3.172 9.677
4.114 9.267
5.039 8.857
6.137 8.733
7.132 8.607
7.795 8.335
7.952 8.196
8.074 8.055
8.179 6.924
8.319 4.661
8.476 1.973
8.55 0

41
datafiles/thrustcurves/AeroTech_G25.eng Normal file
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@ -0,0 +1,41 @@
;
;Aerotech G25 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.
G25 29 124 5-10-15 0.0625 0.1197 AeroTech
0.035 30.499
0.047 36.712
0.059 41.18
0.13 40.669
0.177 38.969
0.295 38.969
0.343 40.947
0.413 40.38
0.437 38.69
0.484 39.824
0.532 37.845
0.65 37.557
0.721 38.969
0.803 38.69
0.85 37.279
0.98 39.535
1.063 36.434
1.098 38.124
1.252 37.845
1.37 37.279
1.583 37
1.819 35.3
1.984 33.61
2.185 31.344
2.315 28.809
2.622 24.286
3.024 18.917
3.39 13.838
3.839 7.624
4.323 4.518
4.783 2.541
5.3 0

40
datafiles/thrustcurves/AeroTech_G33.eng Normal file
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@ -0,0 +1,40 @@
;
;Aerotech G33 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.
G33 29 124 5-7 0.0722 0.1593 AT
0.027 22.642
0.061 42.201
0.117 47.354
0.243 46.678
0.34 46.339
0.438 47.384
0.48 50.92
0.508 46.359
0.543 47.732
0.662 45.693
0.851 42.28
1.039 41.266
1.116 42.987
1.193 39.226
1.221 42.31
1.312 38.888
1.326 40.609
1.479 38.221
1.675 35.157
1.843 32.77
1.878 36.888
1.899 32.093
1.997 30.382
2.13 26.622
2.263 23.547
2.444 19.11
2.591 13.977
2.752 8.502
2.892 4.743
3.053 2.014
3.27 0

17
datafiles/thrustcurves/AeroTech_G339.eng Normal file
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@ -0,0 +1,17 @@
;
; 38-120
; Created from TRA Certification Record issued 23 Nov 2006
; Bill Wagstaff - 04/30/07
G339N 38 97 0 0.049 0.190 AT
0.009 371
0.05 375
0.10 375
0.15 364
0.20 349
0.25 310
0.30 264
0.324 257
0.342 39
0.359 0
;
;

33
datafiles/thrustcurves/AeroTech_G35.eng Normal file
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@ -0,0 +1,33 @@
;
;
G35EJ 29 98 4-7 0.05 0.1005 AeroTech
0.01 39.14
0.02 76.22
0.05 64.46
0.13 57.54
0.21 57.53
0.24 64.43
0.25 57.06
0.35 56.12
0.43 55.2
0.48 57.49
0.51 52.41
0.55 53.33
0.76 50.54
0.91 50.06
1.11 44.96
1.32 41.24
1.55 35.68
1.6 36.13
1.63 33.36
1.67 34.28
1.8 30.12
2 25.02
2.14 21.32
2.23 19.46
2.3 15.77
2.41 9.76
2.53 6.52
2.65 3.74
2.74 1.88
2.91 0

17
datafiles/thrustcurves/AeroTech_G38.eng Normal file
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@ -0,0 +1,17 @@
;
;Aerotech G38FJ RASP.ENG file made by Tim Van Milligan
;For RockSim www.RockSim.com
;File Created March 2, 2005
;Thrust curve supplied by Aerotech for the molded case G38FJ motors.
G38FJ 29 124 4-7 0.0597 0.1264 Aerotech
0.024 52.928
0.171 48.424
0.497 45.045
1 42.23
1.279 39.978
1.498 36.599
1.783 30.406
2.011 23.086
2.272 10.135
2.467 3.941
2.64 0

18
datafiles/thrustcurves/AeroTech_G40.eng Normal file
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@ -0,0 +1,18 @@
;
;Aerotech G40W RASP.ENG file made by Tim Van Milligan
;For RockSim www.RockSim.com
;File Created March 2, 2005
;Thrust curve supplied by Aerotech for the molded case G40W motors.
G40W 29 124 4-7-10 0.0538 0.123 AeroTech
0.024 74.325
0.057 67.005
0.252 65.879
0.5 63.063
0.765 60.248
1 54.054
1.25 47.298
1.502 36.599
1.751 25.338
1.999 12.951
2.121 3.941
2.3 0

26
datafiles/thrustcurves/AeroTech_G53.eng Normal file
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@ -0,0 +1,26 @@
; G53FJ based on Aerotech instruction sheet by C. Kobel 12/9/07
G53FJ 29 124 5-7-10 0.060 0.152 AT
0.012 44.898
0.031 71.504
0.064 80.234
0.081 83.976
0.100 86.47
0.150 84.599
0.200 81.897
0.300 78.571
0.400 76.493
0.500 73.583
0.600 70.881
0.700 67.347
0.800 63.813
0.900 60.072
1.000 54.667
1.100 47.392
1.200 39.909
1.300 32.426
1.400 25.983
1.500 20.578
1.600 10.601
1.700 3.949
1.800 1.247
1.850 0.0

39
datafiles/thrustcurves/AeroTech_G54.eng Normal file
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@ -0,0 +1,39 @@
;
;Aerotech G54 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.
G54 29 124 6-10-14 0.046 0.1365 AT
0.018 10.953
0.042 39.215
0.083 66.888
0.14 72.075
0.223 74.958
0.25 76.694
0.282 80.156
0.315 79.577
0.336 79.577
0.354 81.64
0.365 77.841
0.374 80.724
0.389 76.694
0.455 76.116
0.523 74.39
0.639 70.928
0.722 67.467
0.82 64.005
0.897 58.817
0.992 51.894
1.084 43.824
1.197 34.017
1.268 28.251
1.283 29.987
1.295 27.104
1.328 23.642
1.366 16.719
1.399 9.803
1.435 4.612
1.51 0

41
datafiles/thrustcurves/AeroTech_G55.eng Normal file
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@ -0,0 +1,41 @@
;
;Aerotech G55 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.
G55 24 117 5-10-15 0.0625 0.1148 AeroTech
0.009 81.136
0.014 84.65
0.034 80.557
0.084 77.064
0.13 71.823
0.18 72.422
0.206 68.919
0.342 69.538
0.483 68.989
0.513 66.663
0.543 68.42
0.664 66.114
0.876 66.164
0.901 64.418
0.997 65.026
1.062 66.793
1.088 63.879
1.148 63.889
1.158 66.813
1.173 63.31
1.209 62.741
1.325 61.593
1.395 59.277
1.456 57.541
1.486 58.129
1.587 52.32
1.708 40.094
1.824 26.11
1.95 15.63
2.112 7.498
2.258 3.446
2.44 0

21
datafiles/thrustcurves/AeroTech_G61.eng Normal file
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@ -0,0 +1,21 @@
;
;G61W Data Entered by Tim Van Milligan
;For RockSim: www.RockSim.com
;Based on TRA Certification Test date: June 13, 2004
;Not Approved by TRA or Aerotech
G61W 38 106.7 6-10-14 0.0613 0.1904 AT
0.008 3.083
0.054 71.348
0.089 72.229
0.174 75.312
0.216 78.394
0.247 79.716
0.502 81.037
0.753 77.073
1.001 72.669
1.132 66.944
1.252 55.933
1.503 38.316
1.754 10.13
1.905 3.523
2.04 0

38
datafiles/thrustcurves/AeroTech_G64.eng Normal file
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@ -0,0 +1,38 @@
;
;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

49
datafiles/thrustcurves/AeroTech_G67.eng Normal file
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@ -0,0 +1,49 @@
;
; Aerotech G67R (Redline)
;
; AeroTech RMS-38/120 EZ Access Reloadable Motors (New! Hardware).
; New AeroTech Redline Motor. Just announced on AeroTech's Website!
; File produced 28 Feb 2005.
;
; The file was produced by scaling data points off the
; thrust curve in the manufacturers catalog sheet.
;
; The motor is not yet on www.thrustcurve.org.
; Hence the amateur file production.
; The file was created by Stan Hemphill.
; Contact at stanley_hemphill@hotmail.com.
;
; Motor Dia Len Delay Prop Gross Mfg
G67R 38 106 4-6-8-9-10-12-13-15-17 0.0576 0.191 AT
0.0400 004.9200
0.0500 006.5600
0.0600 009.8400
0.0700 016.4100
0.0800 032.8100
0.1000 049.2200
0.1300 068.0800
0.1500 076.2900
0.1800 080.3900
0.2400 082.8500
0.2600 085.3100
0.3100 087.7700
0.5100 089.4100
0.5300 091.0500
0.5600 087.7700
0.6000 086.9500
0.6100 088.5900
0.6700 086.9500
0.6900 085.3100
0.7100 086.9500
0.7200 085.3100
0.7400 086.1300
0.7700 085.3100
0.8100 082.0300
0.9500 078.7500
1.0500 073.8200
1.4300 053.3200
1.5000 052.5000
1.5200 050.8600
1.5400 045.9400
1.6200 011.4800
1.6400 000.0000

28
datafiles/thrustcurves/AeroTech_G69.eng Normal file
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@ -0,0 +1,28 @@
; Submitted to ThrustCurve.org by Chris Kobel (4/13/07)
; G69N based on Aerotech instruction sheet by C. Kobel 3/29/07
G69N 38 106 0 0.0622 0.195 AT
0.020 51.972
0.050 75.574
0.100 76.709
0.200 77.617
0.300 79.206
0.400 81.475
0.500 84.425
0.600 86.922
0.700 88.737
0.800 89.645
0.900 91.688
1.000 93.503
1.100 94.411
1.200 94.638
1.300 93.957
1.350 93.05
1.400 89.418
1.500 62.865
1.600 33.362
1.650 19.518
1.700 12.028
1.750 7.489
1.800 4.539
1.900 1.816
2.000 0.0

21
datafiles/thrustcurves/AeroTech_G71.eng Normal file
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@ -0,0 +1,21 @@
; G71R based on Aerotech instruction sheet by C. Kobel 3/29/07
G71R 29 124 4-7-10 0.0569 0.147 AT
0.000 0.389
0.050 109.714
0.100 117.884
0.200 113.216
0.300 109.714
0.400 105.045
0.500 99.21
0.600 92.207
0.700 83.258
0.800 75.477
0.900 68.085
1.000 57.97
1.100 47.465
1.200 33.848
1.300 21.009
1.400 11.283
1.500 5.447
1.600 2.334
1.700 0.0

83
datafiles/thrustcurves/AeroTech_G75.eng Normal file
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@ -0,0 +1,83 @@
;
; Aerotech G75J (Black Jack)
;
; AeroTech RMS-29/180 Easy Access Reloadable Motor Hardware.
;
; RASP.ENG file made from made from NAR or TMT published data.
;
; File produced May, 17 2004.
;
; The total impulse, peak thrust, average thrust and burn time are
; the same as the averaged static test data from NAR or TMT files.
;
; The curve drawn with these data points is as accurate as could
; could be made scaling the data from the curve on the TMT html
; page. The file is 63 data points. NOT wRASP v1.6 compatible.
;
; The file was created by Stan Hemphill.
; Contact at stanley_hemphill@hotmail.com.
;
; Motor Dia Len Delay Prop Gross Mfg
G75J 29 194 1-3--4-6-7-9-10 0.114 0.236 AT
0.0281 068.8604
0.0380 078.6517
0.0561 075.9230
0.0660 073.0337
0.0776 070.4655
0.1139 069.3419
0.1403 068.6998
0.1667 067.5762
0.1881 070.3050
0.2013 069.0209
0.2294 072.5522
0.2541 076.4045
0.2723 071.4286
0.3102 076.2440
0.3350 071.9101
0.4208 075.6019
0.4604 072.3917
0.5215 079.2937
0.5941 073.3547
0.6436 080.0963
0.7013 073.8363
0.7393 076.4045
0.7541 074.6388
0.7657 077.3676
0.7937 078.6517
0.8036 077.0465
0.8168 080.2568
0.8267 075.2809
0.8383 081.5409
0.8581 075.7624
0.8795 077.8491
0.9340 074.1573
0.9868 079.9358
1.0380 076.7255
1.0561 072.2311
1.0941 078.8122
1.1221 075.6019
1.1502 080.8989
1.1617 076.8860
1.1848 080.0963
1.1997 076.7255
1.2327 078.8122
1.2508 076.4045
1.2871 082.5040
1.3102 077.5281
1.3267 081.8620
1.3564 075.2809
1.3729 080.0963
1.4076 075.7624
1.4884 079.9358
1.5116 073.6758
1.5297 081.0594
1.5512 074.6388
1.5611 080.8989
1.6040 072.8732
1.7211 075.6019
1.7607 068.6998
1.7789 070.1445
1.8119 066.9342
1.8267 070.7865
1.8482 070.7865
2.3878 000.0000

61
datafiles/thrustcurves/AeroTech_G75.rse
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@ -1,19 +1,48 @@
<engine-database>
<engine-list>
<engine FDiv="10" FFix="1" FStep="-1." Isp="155.88" Itot="161.429" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="73.377" burn-time="2.2" cgDiv="10" cgFix="1" cgStep="-1." code="G75J" delays="6,10" dia="29." exitDia="0." initWt="227.9" len="195." mDiv="10" mFix="1" mStep="-1." massFrac="46.34" mfg="Aerotech" peakThrust="87.27" propWt="105.6" tDiv="10" tFix="1" tStep="-1." throatDia="0.">
<data>
<eng-data cg="97.5" f="0." m="105.6" t="0."/>
<eng-data cg="97.5" f="0.04" m="105.6" t="0."/>
<eng-data cg="97.5" f="82.64" m="102.896" t="0.1"/>
<eng-data cg="97.5" f="78.06" m="97.6396" t="0.2"/>
<eng-data cg="97.5" f="78.06" m="92.5332" t="0.3"/>
<eng-data cg="97.5" f="87.27" m="81.718" t="0.5"/>
<eng-data cg="97.5" f="87.27" m="24.6297" t="1.5"/>
<eng-data cg="97.5" f="82.64" m="13.5149" t="1.7"/>
<eng-data cg="97.5" f="64.27" m="3.90467" t="1.9"/>
<eng-data cg="97.5" f="18.37" m="1.20169" t="2."/>
<eng-data cg="97.5" f="0." m="0." t="2.2"/>
</data>
</engine>
</engine-list>
<engine mfg="Aerotech" code="G75M" Type="single-use" dia="29." len="124." initWt="131."
propWt="66.8" delays="4,7,10" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="60.51" peakThrust="101.497" throatDia="0." exitDia="0." Itot="119.265"
burn-time="1.97" massFrac="50.99" Isp="182.06" 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>29mm Aerotech G75 Metal Storm single use</comments>
<data>
<eng-data t="0." f="0." m="66.8" cg="62."/>
<eng-data t="0.01" f="81.492" m="66.5718" cg="62."/>
<eng-data t="0.013" f="94.731" m="66.4237" cg="62."/>
<eng-data t="0.021" f="101.497" m="65.9841" cg="62."/>
<eng-data t="0.037" f="87.964" m="65.1352" cg="62."/>
<eng-data t="0.068" f="86.199" m="63.6232" cg="62."/>
<eng-data t="0.154" f="87.67" m="59.4357" cg="62."/>
<eng-data t="0.188" f="90.906" m="57.7353" cg="62."/>
<eng-data t="0.211" f="90.024" m="56.5699" cg="62."/>
<eng-data t="0.31" f="95.613" m="51.4232" cg="62."/>
<eng-data t="0.357" f="91.494" m="48.9604" cg="62."/>
<eng-data t="0.464" f="93.848" m="43.4066" cg="62."/>
<eng-data t="0.696" f="92.083" m="31.3264" cg="62."/>
<eng-data t="0.879" f="84.728" m="22.265" cg="62."/>
<eng-data t="0.907" f="85.611" m="20.9293" cg="62."/>
<eng-data t="0.92" f="92.965" m="20.2792" cg="62."/>
<eng-data t="0.939" f="77.667" m="19.3713" cg="62."/>
<eng-data t="1.014" f="72.96" m="16.2075" cg="62."/>
<eng-data t="1.027" f="78.55" m="15.656" cg="62."/>
<eng-data t="1.053" f="71.489" m="14.5635" cg="62."/>
<eng-data t="1.171" f="64.134" m="10.0817" cg="62."/>
<eng-data t="1.304" f="52.367" m="5.74245" cg="62."/>
<eng-data t="1.312" f="56.78" m="5.49792" cg="62."/>
<eng-data t="1.325" f="52.661" m="5.09948" cg="62."/>
<eng-data t="1.374" f="48.542" m="3.71074" cg="62."/>
<eng-data t="1.411" f="44.129" m="2.7505" cg="62."/>
<eng-data t="1.442" f="36.186" m="2.05324" cg="62."/>
<eng-data t="1.492" f="22.359" m="1.23347" cg="62."/>
<eng-data t="1.538" f="14.121" m="0.76352" cg="62."/>
<eng-data t="1.585" f="7.649" m="0.476977" cg="62."/>
<eng-data t="1.643" f="3.825" m="0.290606" cg="62."/>
<eng-data t="1.7" f="2.648" m="0.187279" cg="62."/>
<eng-data t="1.802" f="1.471" m="0.0696199" cg="62."/>
<eng-data t="1.971" f="0." m="0." cg="62."/>
</data>
</engine>
</engine-list>
</engine-database>

30
datafiles/thrustcurves/AeroTech_G75_1.eng Normal file
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@ -0,0 +1,30 @@
; AeroTech G75J
; converted from TMT test stand data 1997 (www.tripoli.org)
; provided by ThrustCurve.org (www.thrustcurve.org)
G75J 29 194 10 0.112 0.23296 AT
0.047 65.701
0.143 68.564
0.239 72.143
0.334 73.261
0.430 73.960
0.526 75.036
0.622 75.705
0.718 75.030
0.814 77.886
0.909 76.183
1.005 76.852
1.101 75.729
1.197 78.854
1.293 78.669
1.389 76.464
1.484 76.440
1.580 74.976
1.676 72.657
1.772 69.460
1.868 62.121
1.964 39.090
2.059 19.703
2.155 7.554
2.251 2.062
2.347 0.382
2.443 0.000

19
datafiles/thrustcurves/AeroTech_G75_1.rse Normal file
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@ -0,0 +1,19 @@
<engine-database>
<engine-list>
<engine FDiv="10" FFix="1" FStep="-1." Isp="155.88" Itot="161.429" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="73.377" burn-time="2.2" cgDiv="10" cgFix="1" cgStep="-1." code="G75J" delays="6,10" dia="29." exitDia="0." initWt="227.9" len="195." mDiv="10" mFix="1" mStep="-1." massFrac="46.34" mfg="Aerotech" peakThrust="87.27" propWt="105.6" tDiv="10" tFix="1" tStep="-1." throatDia="0.">
<data>
<eng-data cg="97.5" f="0." m="105.6" t="0."/>
<eng-data cg="97.5" f="0.04" m="105.6" t="0."/>
<eng-data cg="97.5" f="82.64" m="102.896" t="0.1"/>
<eng-data cg="97.5" f="78.06" m="97.6396" t="0.2"/>
<eng-data cg="97.5" f="78.06" m="92.5332" t="0.3"/>
<eng-data cg="97.5" f="87.27" m="81.718" t="0.5"/>
<eng-data cg="97.5" f="87.27" m="24.6297" t="1.5"/>
<eng-data cg="97.5" f="82.64" m="13.5149" t="1.7"/>
<eng-data cg="97.5" f="64.27" m="3.90467" t="1.9"/>
<eng-data cg="97.5" f="18.37" m="1.20169" t="2."/>
<eng-data cg="97.5" f="0." m="0." t="2.2"/>
</data>
</engine>
</engine-list>
</engine-database>

41
datafiles/thrustcurves/AeroTech_G76.eng Normal file
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@ -0,0 +1,41 @@
; Curve fit of AT Instruction sheet by C. Kobel 7/29/08
G76G 29 124 4-7-10 0.06 0.147 AT
0.025 89.368
0.042 133.581
0.052 144.87
0.067 154.277
0.098 144.399
0.117 136.873
0.150 132.64
0.196 129.348
0.255 123.233
0.299 118.059
0.349 112.885
0.399 108.652
0.449 101.126
0.486 101.597
0.511 105.36
0.516 118.53
0.543 100.186
0.601 95.482
0.656 88.897
0.720 81.842
0.737 93.601
0.754 80.431
0.797 70.553
0.856 63.498
0.898 58.794
0.948 51.739
1.000 47.976
1.063 43.273
1.102 41.391
1.152 39.04
1.200 36.688
1.301 30.103
1.347 25.399
1.401 19.755
1.499 12.229
1.547 7.996
1.599 5.644
1.699 2.352
1.750 0.0

33
datafiles/thrustcurves/AeroTech_G77.eng Normal file
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@ -0,0 +1,33 @@
; Single-Use Casing. Entered by Tim Van Milligan for RockSim Users. Used John
; Coker's ThrustCurve Tracer software and NAR cert paperwork dated 7-29-06.
G77R 29 124 4 0.0591 0.122 Aerotech
0.01 19.124
0.018 15.668
0.059 66.59
0.084 72.35
0.122 75.115
0.151 77.419
0.173 77.65
0.271 85.945
0.337 88.018
0.424 91.935
0.475 93.318
0.523 94.931
0.57 96.313
0.61 96.313
0.644 99.309
0.656 96.774
0.728 95.622
0.792 94.24
0.902 91.014
0.961 88.479
1.017 88.018
1.047 84.562
1.071 81.106
1.099 76.037
1.127 69.355
1.158 61.06
1.188 44.931
1.213 30.184
1.231 18.203
1.277 0.0

Some files were not shown because too many files have changed in this diff Show More