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Updated motor files from thrustcurve download. Added correction files for Quest D5 and Micro_Maxx_II.

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This commit is contained in:
Kevin Ruland 2012-09-12 01:53:50 +00:00
parent b0d03cc473
commit 89a83d54fc
55 changed files with 1601 additions and 114 deletions
Show Stats Download Patch File Download Diff File Expand all files Collapse all files

35
core/resources-src/datafiles/thrustcurves/Quest_D5_1.eng Normal file
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; QUEST D5 RASP.ENG FILE
; 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.
D5 20 96 4-6 0.0240 0.0451 QUEST
0.010 1.014
0.122 2.652
0.172 4.836
0.273 7.723
0.331 10.610
0.390 13.809
0.448 16.800
0.480 12.403
0.484 8.266
0.517 5.221
0.713 4.125
0.974 4.121
1.135 3.338
1.324 3.101
1.550 3.254
1.971 3.169
2.393 3.162
2.752 3.391
3.069 3.386
3.547 3.301
3.694 3.064
3.948 3.294
4.215 3.290
4.412 3.287
4.496 2.505
4.586 1.801
4.610 0.000
;

39
core/resources-src/datafiles/thrustcurves/Quest_Micro_Maxx_II.eng Normal file
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; Traced from NAR certification data dated 1-29-2009
MicroMaxxII 6 26 1 5.0E-4 0.0010 Q
0.021 0.015
0.036 0.05
0.043 0.103
0.049 0.198
0.08 1.636
0.092 1.3
0.109 0.995
0.124 0.805
0.133 0.442
0.143 0.301
0.164 0.21
0.186 0.149
0.199 0.183
0.235 0.145
0.256 0.145
0.293 0.149
0.327 0.164
0.367 0.156
0.387 0.175
0.409 0.183
0.431 0.191
0.461 0.21
0.474 0.202
0.49 0.217
0.505 0.175
0.513 0.198
0.537 0.172
0.553 0.175
0.602 0.156
0.623 0.175
0.644 0.183
0.674 0.21
0.689 0.191
0.697 0.229
0.731 0.21
0.753 0.092
0.771 0.0

3
core/resources-src/datafiles/thrustcurves/README.txt
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@ -7,3 +7,6 @@ SF_*.eng - Thrust curves for Weco Feuerwerk motors, created by Sampo N.
Loki_J175.rse - Corrected motor type from hybrid to reloadable
Quest_D5_1.eng - Corrected motor mass from .451 to .0451
Quest_Micro_Maxx_II.eng - Removed "NE" from delays since OR cannot handle it.

35
core/resources/datafiles/thrustcurves/AeroTech_H178.eng Normal file
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; H178-14 Dark Matter
H178DM 38 191 14 0.177 0.324 AT
0.016 132.659
0.099 165.726
0.146 162.97
0.201 163.364
0.256 164.938
0.301 168.481
0.358 173.205
0.401 176.354
0.457 177.929
0.498 183.046
0.6 198.792
0.635 204.303
0.703 204.303
0.799 215.719
0.901 210.602
0.999 211.783
1.049 205.09
1.098 206.271
1.202 196.824
1.297 178.322
1.351 172.811
1.404 178.322
1.434 186.195
1.499 125.574
1.539 71.25
1.566 44.876
1.582 31.492
1.601 27.949
1.606 16.533
1.617 18.895
1.644 8.66
1.684 4.33
1.735 0.0

25
core/resources/datafiles/thrustcurves/AeroTech_I327.eng Normal file
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; I327-14 Dark Matter
I327DM 38 337 14 0.354 0.628 AT
0.0090 393.741
0.026 432.602
0.161 387.142
0.245 382.742
0.303 371.011
0.601 372.477
0.702 371.011
0.798 375.41
0.983 371.744
1.04 370.278
1.104 371.744
1.199 343.148
1.3 335.816
1.335 357.813
1.365 327.751
1.399 265.427
1.428 185.505
1.451 156.91
1.493 112.183
1.553 68.19
1.601 32.262
1.656 11.732
1.723 0.0

30
core/resources/datafiles/thrustcurves/AeroTech_I350.eng Normal file
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; Aerotech I350-10R single use motor file created using Aerotech instruction
; sheet data and thrust tracer utility.
I350-10R 38 356 P 0.34800000000000003 0.616 AT
0.0040 2.809
0.0080 207.896
0.031 272.512
0.035 359.603
0.046 407.363
0.081 432.648
0.104 435.457
0.127 427.029
0.184 435.457
0.223 443.886
0.299 469.17
0.399 480.408
0.503 486.027
0.603 474.789
0.702 469.17
0.802 457.933
0.906 443.886
1.002 432.648
1.098 415.792
1.205 390.507
1.298 368.032
1.401 345.556
1.443 325.891
1.497 216.324
1.532 101.138
1.57 33.713
1.605 0.0

26
core/resources/datafiles/thrustcurves/AeroTech_K1103.eng Normal file
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; K1103X Propellant X
K1103X 54 401 14 0.8300000000000001 1.459 AT
0.012 1335.712
0.016 1505.168
0.028 1619.8
0.045 1500.184
0.081 1393.028
0.151 1330.728
0.201 1305.808
0.399 1280.888
0.602 1243.508
0.803 1196.16
1.001 1143.828
1.203 1074.052
1.296 1041.656
1.384 1031.688
1.408 1004.276
1.423 961.912
1.438 839.804
1.46 737.632
1.49 510.86
1.505 446.068
1.603 176.932
1.608 209.328
1.638 97.188
1.688 0.0

32
core/resources/datafiles/thrustcurves/AeroTech_K456.eng Normal file
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; K456 Dark Matter
K456DM-14A 54 401 14 0.866 1.484 AT
0.027 444.074
0.038 519.582
0.066 482.95
0.129 461.269
0.302 467.998
0.389 468.745
0.499 476.969
0.655 476.221
0.798 483.697
0.946 488.93
1.096 499.397
1.401 500.892
1.603 503.882
1.801 501.64
1.905 498.649
2.1 485.94
2.302 456.036
2.404 435.851
2.505 420.151
2.574 398.471
2.607 373.052
2.645 356.605
2.703 289.321
2.768 178.676
2.804 123.354
2.837 88.964
2.875 50.837
2.908 24.671
2.957 10.466
3.037 0.0

29
core/resources/datafiles/thrustcurves/AeroTech_L1040.eng Normal file
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; L1040 Dark Matter
L1040DM-P 75 681 P 2.602 4.7170000000000005 AT
0.018 1126.167
0.042 1036.413
0.053 1002.543
0.116 988.995
0.504 1049.961
0.794 1095.685
1.002 1146.489
1.252 1192.213
1.499 1237.937
1.753 1261.646
1.912 1268.42
2.095 1254.872
2.511 1134.635
2.772 1056.734
3.012 966.98
3.153 933.11
3.217 863.677
3.291 817.953
3.34 758.681
3.488 438.613
3.552 284.505
3.598 220.153
3.657 167.655
3.746 118.544
3.88 42.337
3.996 6.774
4.127 0.0

6
core/resources/datafiles/thrustcurves/AeroTech_L339.eng
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@ -1,6 +1,6 @@
; Entered by Tim Van Milligan. Used John Coker's ThrustCurve Tracer software and
; data supplied by Aerotech thrust stand data. The total weight is a guess.
L339N 98 309 4 1.796 4.5 Aerotech
;This file is identical to Tim Van Milligan's L339 file except the motor and
; propellant weights have been corrected. Total weight was about 50% too high.
L339N 98 309 4 1.355 3.15 Aerotech
0.049 2.884
0.074 373.449
0.123 399.403

69
core/resources/datafiles/thrustcurves/AeroTech_L339_1.eng Normal file
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@ -0,0 +1,69 @@
; Entered by Tim Van Milligan. Used John Coker's ThrustCurve Tracer software and
; data supplied by Aerotech thrust stand data. The total weight is a guess.
L339N 98 309 4 1.796 4.5 Aerotech
0.049 2.884
0.074 373.449
0.123 399.403
0.156 408.054
0.279 415.984
0.427 417.426
0.476 421.031
0.509 416.705
0.632 415.984
0.837 414.542
0.894 418.868
0.943 405.17
1.026 400.124
1.124 402.286
1.255 397.961
1.362 392.914
1.51 391.472
1.575 394.356
1.592 385.705
1.657 387.147
1.838 384.984
2.026 382.821
2.174 379.937
2.404 377.053
2.478 378.495
2.552 377.053
2.617 378.495
2.683 366.96
2.773 359.751
2.806 363.355
2.937 359.751
3.232 351.099
3.314 355.425
3.356 351.099
3.815 345.332
3.979 340.285
4.233 336.681
4.414 333.797
4.668 330.913
4.996 329.471
5.39 323.704
5.686 320.099
5.989 314.331
6.178 310.727
6.325 306.401
6.514 302.075
6.621 302.075
6.851 297.75
7.195 290.54
7.277 293.424
7.326 287.656
7.441 283.331
7.49 286.214
7.54 283.331
7.696 275.4
7.81 273.958
7.884 276.842
7.942 278.284
8.015 276.121
8.073 270.354
8.188 155.003
8.212 118.956
8.278 54.071
8.311 26.675
8.352 7.93
8.426 0.0

35
core/resources/datafiles/thrustcurves/AeroTech_L400.eng Normal file
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@ -0,0 +1,35 @@
; Aerotech L400W-PS created using TCtracer and AT thrustcurve
L400W 98 443.2 P 2.6489656 5.0847439 AT
0.031 436.662
0.062 493.929
0.063 586.988
0.108 634.711
0.154 606.077
0.277 622.78
0.4 639.483
0.508 610.85
0.538 601.305
0.908 665.731
1.092 684.82
1.631 720.612
1.954 706.295
2.385 703.909
2.6 701.523
2.769 689.592
3.2 656.186
3.754 586.988
4.354 527.335
5.262 434.276
5.815 386.553
6.477 336.445
7.354 276.791
8.046 217.138
8.846 167.029
9.862 107.376
10.969 64.426
11.969 40.564
12.969 26.247
13.985 14.317
14.938 7.158
15.462 2.386
15.938 0.0

30
core/resources/datafiles/thrustcurves/AeroTech_L900.eng Normal file
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@ -0,0 +1,30 @@
; L900 Dark Matter
L900DM 75 665.5 P 2.472 4.724 AT
0.016 577.998
0.041 870.377
0.086 851.787
0.303 931.219
0.417 944.74
0.515 910.939
0.998 936.289
1.272 976.851
1.501 992.061
1.747 1019.102
2.0 1029.242
2.205 1054.593
2.495 1047.833
2.77 1034.313
3.003 998.821
3.166 981.921
3.498 909.249
3.592 880.518
3.702 890.658
3.768 856.857
3.862 672.641
3.964 442.794
4.021 353.221
4.111 285.619
4.242 104.783
4.3 50.702
4.369 21.971
4.484 0.0

24
core/resources/datafiles/thrustcurves/AeroTech_M1075.eng Normal file
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@ -0,0 +1,24 @@
; M1075 Dark Matter
M1075DM 98 597 P 3.846 6.971 AT
0.02 927.501
0.112 988.073
0.26 1033.501
0.53 1080.823
0.897 1124.359
1.509 1198.18
1.998 1239.823
2.355 1260.644
2.503 1264.43
2.773 1237.93
2.997 1222.787
3.502 1162.216
4.001 1063.787
4.501 906.68
4.741 834.751
4.878 742.001
4.96 664.394
5.062 448.608
5.164 223.357
5.26 79.5
5.352 30.286
5.5 0.0

31
core/resources/datafiles/thrustcurves/AeroTech_M1305.eng Normal file
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@ -0,0 +1,31 @@
; M1305 Metalstorm
M1305M 98 597 P 4.08 7.098 AT
0.016 1288.076
0.043 1462.78
0.08 1370.986
0.407 1622.679
0.535 1640.446
0.787 1705.59
0.985 1693.745
1.13 1717.434
1.328 1693.745
1.349 1927.672
1.397 1726.317
1.751 1711.512
2.018 1687.823
2.275 1690.784
2.297 1892.139
2.318 1678.94
2.929 1412.441
3.748 1113.371
4.24 906.095
4.503 802.456
4.717 663.285
4.813 538.919
4.92 387.903
5.027 245.771
5.166 145.094
5.263 79.95
5.386 32.572
5.498 23.689
5.707 0.0

65
core/resources/datafiles/thrustcurves/AeroTech_M1780.eng
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@ -1,23 +1,42 @@
M1780 75 665 P 2.56 4.715 AT
0.028 2204.193
0.118 2566.025
0.173 2566.025
0.341 2214.151
0.44 2144.44
0.636 2114.564
1.34 2134.482
1.395 2204.193
1.648 2121.203
1.841 2041.534
1.874 1895.473
2.127 1643.186
2.353 1517.042
2.584 1460.61
2.672 1347.744
2.763 1068.901
2.829 723.666
2.939 438.183
2.999 292.122
3.101 172.617
3.272 36.515
3.5 0.0
; AT M1780NT 1" Core Revised
M1780NT 75 665 P 2.371 4.606 AT
0.0090 1337.154
0.026 2005.731
0.04 2106.521
0.046 2163.636
0.085 2156.916
0.108 2126.679
0.134 2113.24
0.168 2130.039
0.205 2126.679
0.259 2197.233
0.299 2156.916
0.347 2130.039
0.399 2123.32
0.495 2103.161
0.595 2089.723
0.697 2079.644
0.8 2083.003
0.9 2076.284
0.999 2069.565
1.201 2056.126
1.398 2029.248
1.603 2002.371
1.799 1965.414
1.998 1904.94
2.2 1817.588
2.3 1757.114
2.354 1723.517
2.405 1713.438
2.46 1629.446
2.502 1558.893
2.571 1333.794
2.622 1115.415
2.67 890.316
2.724 665.217
2.758 571.146
2.798 507.312
2.83 446.838
2.901 265.415
3.003 73.913
3.035 0.0

23
core/resources/datafiles/thrustcurves/AeroTech_M1780_1.eng Normal file
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@ -0,0 +1,23 @@
M1780 75 665 P 2.56 4.715 AT
0.028 2204.193
0.118 2566.025
0.173 2566.025
0.341 2214.151
0.44 2144.44
0.636 2114.564
1.34 2134.482
1.395 2204.193
1.648 2121.203
1.841 2041.534
1.874 1895.473
2.127 1643.186
2.353 1517.042
2.584 1460.61
2.672 1347.744
2.763 1068.901
2.829 723.666
2.939 438.183
2.999 292.122
3.101 172.617
3.272 36.515
3.5 0.0

31
core/resources/datafiles/thrustcurves/Cesaroni_E22.rse Normal file
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<engine-database>
<engine-list>
<engine mfg="CTI" code="24-E22-SS-13A" Type="unspecified" dia="24." len="69."
initWt="56.5" propWt="20.3" delays="13,10,8,6,4" auto-calc-mass="1"
auto-calc-cg="1" avgThrust="22.327" peakThrust="30.792" throatDia="0."
exitDia="0." Itot="24.27" burn-time="1.09" massFrac="35.93" Isp="121.91"
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>Smoky Sam 24mm 1G
24-E22-SS-13A
</comments>
<data>
<eng-data t="0." f="0." m="20.3" cg="34.5"/>
<eng-data t="0.008" f="18.292" m="20.2388" cg="34.5"/>
<eng-data t="0.026" f="30." m="19.8753" cg="34.5"/>
<eng-data t="0.038" f="30.792" m="19.5702" cg="34.5"/>
<eng-data t="0.067" f="18.708" m="18.9698" cg="34.5"/>
<eng-data t="0.101" f="21.875" m="18.3927" cg="34.5"/>
<eng-data t="0.33" f="26.083" m="13.7997" cg="34.5"/>
<eng-data t="0.528" f="28.042" m="9.31773" cg="34.5"/>
<eng-data t="0.716" f="27.875" m="4.92123" cg="34.5"/>
<eng-data t="0.841" f="23.542" m="2.23328" cg="34.5"/>
<eng-data t="0.912" f="17.833" m="1.00471" cg="34.5"/>
<eng-data t="0.987" f="7." m="0.225783" cg="34.5"/>
<eng-data t="1.016" f="3.333" m="0.100461" cg="34.5"/>
<eng-data t="1.065" f="1.083" m="0.00996451" cg="34.5"/>
<eng-data t="1.087" f="0." m="0." cg="34.5"/>
</data>
</engine>
</engine-list>
</engine-database>

29
core/resources/datafiles/thrustcurves/Cesaroni_E31.rse Normal file
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@ -0,0 +1,29 @@
<engine-database>
<engine-list>
<engine mfg="CTI" code="26-E31-WH-15A" Type="unspecified" dia="24." len="69."
initWt="52." propWt="16.9" delays="15,12,10,8,6" auto-calc-mass="1"
auto-calc-cg="1" avgThrust="29.982" peakThrust="43.824" throatDia="0."
exitDia="0." Itot="26.084" burn-time="0.87" massFrac="32.5" Isp="157.39"
tDiv="10" tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10"
mStep="-1." mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<comments>White 24mm 1G
26-E31-WH-15A
</comments>
<data>
<eng-data t="0." f="0." m="16.9" cg="34.5"/>
<eng-data t="0.02" f="43.824" m="16.6161" cg="34.5"/>
<eng-data t="0.027" f="39.964" m="16.4261" cg="34.5"/>
<eng-data t="0.049" f="26.781" m="15.9504" cg="34.5"/>
<eng-data t="0.113" f="32.601" m="14.7192" cg="34.5"/>
<eng-data t="0.193" f="34.739" m="12.974" cg="34.5"/>
<eng-data t="0.282" f="35.808" m="10.94" cg="34.5"/>
<eng-data t="0.5" f="34.442" m="5.97881" cg="34.5"/>
<eng-data t="0.727" f="29.276" m="1.29315" cg="34.5"/>
<eng-data t="0.771" f="22.743" m="0.551669" cg="34.5"/>
<eng-data t="0.807" f="9.561" m="0.174929" cg="34.5"/>
<eng-data t="0.84" f="3.563" m="0.0346274" cg="34.5"/>
<eng-data t="0.87" f="0." m="0." cg="34.5"/>
</data>
</engine>
</engine-list>
</engine-database>

29
core/resources/datafiles/thrustcurves/Cesaroni_F50.rse Normal file
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@ -0,0 +1,29 @@
<engine-database>
<engine-list>
<engine mfg="CTI" code="60-F50-SK-13A" Type="unspecified" dia="24." len="133."
initWt="93.9" propWt="38.2" delays="13,10,8,6,4" auto-calc-mass="1"
auto-calc-cg="1" avgThrust="45.996" peakThrust="69.516" throatDia="0."
exitDia="0." Itot="59.702" burn-time="1.3" massFrac="40.68" Isp="159.37"
tDiv="10" tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10"
mStep="-1." mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<comments>Skidmark 24mm 3G
60-F50-SK-13A
</comments>
<data>
<eng-data t="0." f="0." m="38.2" cg="66.5"/>
<eng-data t="0.015" f="64.982" m="37.8882" cg="66.5"/>
<eng-data t="0.022" f="69.516" m="37.587" cg="66.5"/>
<eng-data t="0.064" f="55.537" m="35.9067" cg="66.5"/>
<eng-data t="0.118" f="62.81" m="33.8621" cg="66.5"/>
<eng-data t="0.342" f="62.149" m="24.9073" cg="66.5"/>
<eng-data t="0.536" f="59.41" m="17.3628" cg="66.5"/>
<eng-data t="0.743" f="53.837" m="9.86315" cg="66.5"/>
<eng-data t="0.884" f="46.942" m="5.31712" cg="66.5"/>
<eng-data t="0.976" f="40.047" m="2.7568" cg="66.5"/>
<eng-data t="1.096" f="12.562" m="0.737116" cg="66.5"/>
<eng-data t="1.246" f="2.078" m="0.0345694" cg="66.5"/>
<eng-data t="1.298" f="0." m="0." cg="66.5"/>
</data>
</engine>
</engine-list>
</engine-database>

26
core/resources/datafiles/thrustcurves/Cesaroni_F51.rse Normal file
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<engine-database>
<engine-list>
<engine mfg="CTI" code="75-F51-CL-12A" Type="unspecified" dia="24." len="133."
initWt="95." propWt="40." delays="12,9,7,5" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="47.72" peakThrust="84.148" throatDia="0." exitDia="0." Itot="75.254"
burn-time="1.58" massFrac="42.11" Isp="191.85" tDiv="10" tStep="-1." tFix="1"
FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10"
cgStep="-1." cgFix="1">
<comments>Classic 24mm 3G
75-F51-CL-12A
</comments>
<data>
<eng-data t="0." f="0." m="40." cg="66.5"/>
<eng-data t="0.02" f="75.924" m="39.5964" cg="66.5"/>
<eng-data t="0.031" f="84.148" m="39.1285" cg="66.5"/>
<eng-data t="0.062" f="70.441" m="37.8549" cg="66.5"/>
<eng-data t="0.117" f="73.659" m="35.7485" cg="66.5"/>
<eng-data t="1.211" f="38.737" m="3.06972" cg="66.5"/>
<eng-data t="1.376" f="14.779" m="0.722981" cg="66.5"/>
<eng-data t="1.456" f="7.271" m="0.254171" cg="66.5"/>
<eng-data t="1.532" f="3.337" m="0.0399086" cg="66.5"/>
<eng-data t="1.577" f="0." m="0." cg="66.5"/>
</data>
</engine>
</engine-list>
</engine-database>

41
core/resources/datafiles/thrustcurves/Cesaroni_G69_1.eng
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@ -1,16 +1,25 @@
; CTI Pro38 G69 Skidmark
G69SK-14A 38 117 5-7-9-11-14 0.0615 0.197 CTI
0.025 102.515
0.058 97.371
0.069 77.862
0.088 59.593
0.22 72.541
0.359 81.054
1.036 81.586
1.289 75.201
1.384 71.831
1.488 76.443
1.551 64.205
1.613 34.053
1.696 9.932
1.814 0.0
; Pro38 G69
G69 38 127 5-7-9-12 0.066500 0.2045 Pro38
0.079 79.935
0.103 72.367
0.136 82.989
0.217 85.910
0.247 82.193
0.311 84.317
0.352 80.201
0.387 82.856
0.840 72.499
0.944 72.234
0.978 69.047
1.017 71.835
1.082 67.852
1.227 66.657
1.237 65.329
1.493 62.010
1.530 59.354
1.591 60.151
1.714 56.167
1.769 54.574
1.848 46.607
1.887 27.884
1.958 00.000

39
core/resources/datafiles/thrustcurves/Cesaroni_G69_2.eng
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@ -1,25 +1,14 @@
; Pro38 G69
G69 38 127 5-7-9-12 0.066500 0.2045 Pro38
0.079 79.935
0.103 72.367
0.136 82.989
0.217 85.910
0.247 82.193
0.311 84.317
0.352 80.201
0.387 82.856
0.840 72.499
0.944 72.234
0.978 69.047
1.017 71.835
1.082 67.852
1.227 66.657
1.237 65.329
1.493 62.010
1.530 59.354
1.591 60.151
1.714 56.167
1.769 54.574
1.848 46.607
1.887 27.884
1.958 00.000
;
133G69 38.0 127.00 3-5-7-9-12 0.08400 0.20510 CTI
0.06 80.77
0.20 84.50
0.41 82.74
0.59 80.11
0.81 76.82
1.00 72.87
1.20 68.92
1.40 64.31
1.61 59.48
1.82 50.92
1.90 21.40
1.93 0.00

16
core/resources/datafiles/thrustcurves/Cesaroni_I165.eng Normal file
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@ -0,0 +1,16 @@
;Pro-54-1G C-Star 518-I165-17A
;Ejection adjustable from 7 to 17
518-I165-CS-17A 54 69 17-15-13-11-9-7 0.267 0.594 CTI
0.027 133.424
0.056 174.831
0.067 179.973
0.497 188.633
1.018 184.032
1.704 169.959
2.95 129.364
3.05 130.717
3.168 44.655
3.213 17.862
3.271 3.518
3.5 0
;

16
core/resources/datafiles/thrustcurves/Cesaroni_J316.eng Normal file
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; Pink 38mm 5G
; 654-J316-PK-17A
654-J316-PK-17A 38 367 17-14-12-10-8 0.3508 0.6071000000000001 CTI
0.017 393.07
0.026 443.25
0.064 381.123
0.223 393.07
0.503 379.331
1.029 354.241
1.52 320.789
1.672 313.023
1.695 296.296
1.816 145.759
1.901 88.411
2.043 32.855
2.184 0.0

30
core/resources/datafiles/thrustcurves/Cesaroni_J316.rse Normal file
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@ -0,0 +1,30 @@
<engine-database>
<engine-list>
<engine mfg="CTI" code="654-J316-PK-17A" Type="unspecified" dia="38." len="367."
initWt="607.1" propWt="350.8" delays="17,14,12,10,8" auto-calc-mass="1"
auto-calc-cg="1" avgThrust="299.405" peakThrust="443.25" throatDia="0."
exitDia="0." Itot="653.901" burn-time="2.18" massFrac="57.78" Isp="190.08"
tDiv="10" tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10"
mStep="-1." mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<comments>Pink 38mm 5G
654-J316-PK-17A
</comments>
<data>
<eng-data t="0." f="0." m="350.8" cg="183.5"/>
<eng-data t="0.017" f="393.07" m="349.008" cg="183.5"/>
<eng-data t="0.026" f="443.25" m="346.989" cg="183.5"/>
<eng-data t="0.064" f="381.123" m="338.586" cg="183.5"/>
<eng-data t="0.223" f="393.07" m="305.567" cg="183.5"/>
<eng-data t="0.503" f="379.331" m="247.555" cg="183.5"/>
<eng-data t="1.029" f="354.241" m="144.053" cg="183.5"/>
<eng-data t="1.52" f="320.789" m="55.1492" cg="183.5"/>
<eng-data t="1.672" f="313.023" m="29.3074" cg="183.5"/>
<eng-data t="1.695" f="296.296" m="25.5483" cg="183.5"/>
<eng-data t="1.816" f="145.759" m="11.2007" cg="183.5"/>
<eng-data t="1.901" f="88.411" m="5.86159" cg="183.5"/>
<eng-data t="2.043" f="32.855" m="1.24262" cg="183.5"/>
<eng-data t="2.184" f="0." m="0." cg="183.5"/>
</data>
</engine>
</engine-list>
</engine-database>

107
core/resources/datafiles/thrustcurves/Cesaroni_J425.eng
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@ -1,24 +1,83 @@
J425BS 38 421 16-13-11-9-7 0.405 0.7000000000000001 Cesaroni
0.028 141.739
0.053 133.043
0.079 126.957
0.126 123.478
0.574 116.957
1.014 110.0
1.3 105.652
1.34 102.609
1.374 95.217
1.414 77.826
1.437 73.478
1.472 72.174
1.519 64.783
1.547 54.783
1.595 36.087
1.658 18.261
1.695 13.913
1.747 10.87
1.821 9.13
1.898 6.087
1.935 4.783
1.944 3.478
1.945 0.0
; Pro38 784J425-16A
J425 38 409.2 16-13-11-9-7 0.405 0.7000000000000001 CTI
0.0060 4.399
0.01 92.386
0.011 272.759
0.012 434.068
0.013 507.39
0.016 589.511
0.02 668.699
0.021 720.025
0.027 659.901
0.037 632.038
0.053 589.511
0.069 566.048
0.098 554.317
0.135 552.85
0.167 548.451
0.206 546.984
0.251 542.585
0.289 542.585
0.326 538.186
0.369 533.786
0.41 526.454
0.455 527.921
0.489 523.521
0.508 520.588
0.524 520.588
0.561 517.655
0.589 522.055
0.62 517.655
0.656 513.256
0.687 510.323
0.72 505.924
0.75 507.39
0.787 505.924
0.818 504.457
0.856 500.058
0.887 495.659
0.919 494.192
0.952 492.726
0.987 489.793
1.017 489.793
1.05 485.394
1.078 482.461
1.113 482.461
1.146 479.528
1.18 479.528
1.217 472.196
1.252 473.662
1.288 470.729
1.321 464.863
1.348 451.665
1.366 431.135
1.382 401.806
1.395 378.343
1.407 357.813
1.421 338.749
1.445 325.551
1.476 313.819
1.498 300.621
1.521 278.625
1.541 249.296
1.556 224.366
1.568 206.769
1.58 184.772
1.596 161.309
1.607 140.779
1.625 117.316
1.641 93.853
1.67 73.322
1.69 63.057
1.717 52.792
1.745 48.393
1.772 45.46
1.796 42.527
1.821 42.527
1.849 38.128
1.884 29.329
1.906 26.396
1.929 19.064
1.955 16.131
1.978 10.265
1.996 0.0

28
core/resources/datafiles/thrustcurves/Cesaroni_J453.rse Normal file
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@ -0,0 +1,28 @@
<engine-database>
<engine-list>
<engine mfg="CTI" code="1013-J453-WH-16A" Type="unspecified" dia="38." len="500."
initWt="964.3" propWt="613.2" delays="16,13,11,9,7" auto-calc-mass="1"
auto-calc-cg="1" avgThrust="430.622" peakThrust="725.18" throatDia="0."
exitDia="0." Itot="1017.99" burn-time="2.36" massFrac="63.59" Isp="169.29"
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>White 38mm 6GXL
1013-J453-WH-16A
</comments>
<data>
<eng-data t="0." f="0." m="613.2" cg="250."/>
<eng-data t="0.018" f="663.789" m="609.601" cg="250."/>
<eng-data t="0.04" f="725.18" m="600.398" cg="250."/>
<eng-data t="0.105" f="630.216" m="573.864" cg="250."/>
<eng-data t="0.23" f="578.417" m="528.362" cg="250."/>
<eng-data t="0.451" f="543.885" m="453.66" cg="250."/>
<eng-data t="1.454" f="535.252" m="127.669" cg="250."/>
<eng-data t="1.797" f="291.607" m="42.2501" cg="250."/>
<eng-data t="1.91" f="188.969" m="25.8944" cg="250."/>
<eng-data t="2.088" f="128.537" m="8.87281" cg="250."/>
<eng-data t="2.276" f="19.185" m="0.508479" cg="250."/>
<eng-data t="2.364" f="0." m="0." cg="250."/>
</data>
</engine>
</engine-list>
</engine-database>

30
core/resources/datafiles/thrustcurves/Cesaroni_K2000.rse Normal file
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@ -0,0 +1,30 @@
<engine-database>
<engine-list>
<engine mfg="CTI" code="2330-K2000-VM-P" Type="unspecified" dia="75." len="350."
initWt="2464.5" propWt="1164.2" delays="0" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="1957.59" peakThrust="2473.68" throatDia="0." exitDia="0."
Itot="2331.49" burn-time="1.19" massFrac="47.24" Isp="204.21" 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>VMax 75mm 2G
2330-K2000-VM-P
</comments>
<data>
<eng-data t="0." f="0." m="1164.2" cg="175."/>
<eng-data t="0.01" f="1979.53" m="1159.26" cg="175."/>
<eng-data t="0.029" f="1634.5" m="1142.11" cg="175."/>
<eng-data t="0.161" f="1947.37" m="1024.07" cg="175."/>
<eng-data t="0.321" f="2190.06" m="858.791" cg="175."/>
<eng-data t="0.457" f="2397.66" m="703.015" cg="175."/>
<eng-data t="0.548" f="2473.68" m="592.339" cg="175."/>
<eng-data t="0.678" f="2383.04" m="434.704" cg="175."/>
<eng-data t="0.768" f="2263.16" m="330.303" cg="175."/>
<eng-data t="0.977" f="1923.98" m="111.815" cg="175."/>
<eng-data t="1.027" f="1883.04" m="64.2905" cg="175."/>
<eng-data t="1.104" f="859.649" m="11.5636" cg="175."/>
<eng-data t="1.149" f="87.719" m="0.91983" cg="175."/>
<eng-data t="1.191" f="0." m="0." cg="175."/>
</data>
</engine>
</engine-list>
</engine-database>

48
core/resources/datafiles/thrustcurves/Cesaroni_K580.eng Normal file
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@ -0,0 +1,48 @@
;Created by Jesus Manuel Recuenco Andres 2011
;with Tctracer v1.0
K580 54.0 491.00 1000 0.89500 1.82300 Cesaroni
0.02 624.92
0.03 1076.60
0.07 846.73
0.12 884.56
0.20 855.46
0.29 840.91
0.39 835.09
0.48 822.58
0.56 808.60
0.66 800.62
0.74 784.64
0.83 776.66
0.90 762.68
0.96 760.68
1.03 748.71
1.10 734.32
1.14 713.24
1.18 720.75
1.27 704.78
1.35 682.82
1.43 666.85
1.51 650.87
1.59 632.91
1.67 622.92
1.73 604.95
1.79 598.96
1.86 579.00
1.94 561.03
1.99 559.03
2.03 539.07
2.09 533.08
2.16 517.11
2.24 507.12
2.31 491.15
2.39 477.18
2.45 463.20
2.51 442.28
2.55 407.36
2.60 360.81
2.65 320.07
2.69 276.42
2.76 232.78
2.82 194.95
2.96 122.21
3.20 0.00

35
core/resources/datafiles/thrustcurves/Cesaroni_K650.rse
View File

@ -1,27 +1,24 @@
<engine-database>
<engine-list>
<engine mfg="Cesaroni Technology Inc." code="K650SS" Type="reloadable" dia="54."
len="488." initWt="1989.9" propWt="1281." delays="16" auto-calc-mass="1"
auto-calc-cg="1" avgThrust="657.68" peakThrust="728.7" throatDia="0."
exitDia="0." Itot="1749.43" burn-time="2.66" massFrac="64.38" Isp="139.26"
<engine mfg="CTI" code="1997-K650-PK-21" Type="unspecified" dia="54." len="488."
initWt="1710." propWt="1065.1" delays="21,19,17,15,13,11" auto-calc-mass="1"
auto-calc-cg="1" avgThrust="578.782" peakThrust="1353.5" throatDia="0."
exitDia="0." Itot="1997.38" burn-time="3.45" massFrac="62.29" Isp="191.23"
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>Pink 54mm 5G
1997-K650-PK-21
</comments>
<data>
<eng-data t="0." f="0." m="1281." cg="244."/>
<eng-data t="0.04" f="664.52" m="1271.27" cg="244."/>
<eng-data t="0.12" f="645.9" m="1232.89" cg="244."/>
<eng-data t="0.31" f="642.24" m="1143.28" cg="244."/>
<eng-data t="0.6" f="664.78" m="1004.51" cg="244."/>
<eng-data t="0.91" f="684.59" m="851.358" cg="244."/>
<eng-data t="1.22" f="712.82" m="692.757" cg="244."/>
<eng-data t="1.5" f="723.41" m="545.524" cg="244."/>
<eng-data t="1.8" f="728.7" m="386.03" cg="244."/>
<eng-data t="2.1" f="664.52" m="233.005" cg="244."/>
<eng-data t="2.4" f="614.68" m="92.5027" cg="244."/>
<eng-data t="2.51" f="680.53" m="40.3405" cg="244."/>
<eng-data t="2.55" f="534.62" m="22.5449" cg="244."/>
<eng-data t="2.61" f="268.19" m="4.90948" cg="244."/>
<eng-data t="2.66" f="0." m="0." cg="244."/>
<eng-data t="0." f="0." m="1065.1" cg="244."/>
<eng-data t="0.011" f="1353.5" m="1061.13" cg="244."/>
<eng-data t="0.028" f="793.832" m="1051.4" cg="244."/>
<eng-data t="0.186" f="815.421" m="983.605" cg="244."/>
<eng-data t="2.578" f="601.186" m="80.1407" cg="244."/>
<eng-data t="2.689" f="479.953" m="48.144" cg="244."/>
<eng-data t="2.855" f="189.324" m="18.522" cg="244."/>
<eng-data t="3.086" f="43.179" m="4.20209" cg="244."/>
<eng-data t="3.451" f="0." m="0." cg="244."/>
</data>
</engine>
</engine-list>

28
core/resources/datafiles/thrustcurves/Cesaroni_K650_1.rse Normal file
View File

@ -0,0 +1,28 @@
<engine-database>
<engine-list>
<engine mfg="Cesaroni Technology Inc." code="K650SS" Type="reloadable" dia="54."
len="488." initWt="1989.9" propWt="1281." delays="16" auto-calc-mass="1"
auto-calc-cg="1" avgThrust="657.68" peakThrust="728.7" throatDia="0."
exitDia="0." Itot="1749.43" burn-time="2.66" massFrac="64.38" Isp="139.26"
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="1281." cg="244."/>
<eng-data t="0.04" f="664.52" m="1271.27" cg="244."/>
<eng-data t="0.12" f="645.9" m="1232.89" cg="244."/>
<eng-data t="0.31" f="642.24" m="1143.28" cg="244."/>
<eng-data t="0.6" f="664.78" m="1004.51" cg="244."/>
<eng-data t="0.91" f="684.59" m="851.358" cg="244."/>
<eng-data t="1.22" f="712.82" m="692.757" cg="244."/>
<eng-data t="1.5" f="723.41" m="545.524" cg="244."/>
<eng-data t="1.8" f="728.7" m="386.03" cg="244."/>
<eng-data t="2.1" f="664.52" m="233.005" cg="244."/>
<eng-data t="2.4" f="614.68" m="92.5027" cg="244."/>
<eng-data t="2.51" f="680.53" m="40.3405" cg="244."/>
<eng-data t="2.55" f="534.62" m="22.5449" cg="244."/>
<eng-data t="2.61" f="268.19" m="4.90948" cg="244."/>
<eng-data t="2.66" f="0." m="0." cg="244."/>
</data>
</engine>
</engine-list>
</engine-database>

33
core/resources/datafiles/thrustcurves/Cesaroni_K661.rse Normal file
View File

@ -0,0 +1,33 @@
<engine-database>
<engine-list>
<engine mfg="CTI" code="2430-K661-BS-P" Type="unspecified" dia="75." len="350."
initWt="2527.8" propWt="1262.5" delays="0" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="641.518" peakThrust="758.091" throatDia="0." exitDia="0."
Itot="2436.49" burn-time="3.8" massFrac="49.94" Isp="196.79" 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>Blue Streak 75mm 2G
2430-K661-BS-P
</comments>
<data>
<eng-data t="0." f="0." m="1262.5" cg="175."/>
<eng-data t="0.041" f="588.591" m="1256.25" cg="175."/>
<eng-data t="0.073" f="659.371" m="1245.9" cg="175."/>
<eng-data t="0.122" f="635.157" m="1229.47" cg="175."/>
<eng-data t="0.225" f="634.226" m="1195.59" cg="175."/>
<eng-data t="0.679" f="713.388" m="1037.08" cg="175."/>
<eng-data t="1.039" f="751.572" m="900.446" cg="175."/>
<eng-data t="1.241" f="758.091" m="821.438" cg="175."/>
<eng-data t="1.832" f="727.357" m="593.99" cg="175."/>
<eng-data t="2.298" f="687.311" m="423.194" cg="175."/>
<eng-data t="2.729" f="667.753" m="271.882" cg="175."/>
<eng-data t="3.195" f="645.402" m="113.341" cg="175."/>
<eng-data t="3.367" f="670.547" m="54.6998" cg="175."/>
<eng-data t="3.584" f="182.538" m="6.73867" cg="175."/>
<eng-data t="3.672" f="55.879" m="1.30294" cg="175."/>
<eng-data t="3.72" f="18.626" m="0.376402" cg="175."/>
<eng-data t="3.798" f="0." m="0." cg="175."/>
</data>
</engine>
</engine-list>
</engine-database>

31
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<engine-database>
<engine-list>
<engine mfg="CTI" code="1955-K735-SK-P" Type="unspecified" dia="75." len="350."
initWt="2508.8" propWt="1222.1" delays="0" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="692.838" peakThrust="889.282" throatDia="0." exitDia="0."
Itot="1961.42" burn-time="2.83" massFrac="48.71" Isp="163.66" 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>Skidmark 75mm 2G
1955-K735-SK-P
</comments>
<data>
<eng-data t="0." f="0." m="1222.1" cg="175."/>
<eng-data t="0.053" f="683.157" m="1210.82" cg="175."/>
<eng-data t="0.142" f="593.64" m="1175.42" cg="175."/>
<eng-data t="0.408" f="697.291" m="1068.44" cg="175."/>
<eng-data t="0.893" f="848.057" m="834.95" cg="175."/>
<eng-data t="1.109" f="886.926" m="718.2" cg="175."/>
<eng-data t="1.24" f="882.214" m="646." cg="175."/>
<eng-data t="1.362" f="889.282" m="578.671" cg="175."/>
<eng-data t="2." f="783.274" m="246.236" cg="175."/>
<eng-data t="2.346" f="706.714" m="85.6289" cg="175."/>
<eng-data t="2.439" f="648.999" m="46.3503" cg="175."/>
<eng-data t="2.612" f="123.675" m="4.70677" cg="175."/>
<eng-data t="2.676" f="36.514" m="1.51289" cg="175."/>
<eng-data t="2.754" f="12.956" m="0.31079" cg="175."/>
<eng-data t="2.831" f="0." m="0." cg="175."/>
</data>
</engine>
</engine-list>
</engine-database>

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

32
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<engine-database>
<engine-list>
<engine mfg="CTI" code="3727-L1050-BS-P" Type="unspecified" dia="75." len="486."
initWt="3447.7" propWt="1863.4" delays="0" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="1000.17" peakThrust="1207.29" throatDia="0." exitDia="0."
Itot="3731.64" burn-time="3.73" massFrac="54.05" Isp="204.21" 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>Blue Streak 75mm 3G
3727-L1050-BS-P
</comments>
<data>
<eng-data t="0." f="0." m="1863.4" cg="243."/>
<eng-data t="0.035" f="721.412" m="1857.1" cg="243."/>
<eng-data t="0.081" f="1110.12" m="1836.06" cg="243."/>
<eng-data t="0.131" f="1057.41" m="1809." cg="243."/>
<eng-data t="0.249" f="1100.23" m="1745.43" cg="243."/>
<eng-data t="0.913" f="1194.12" m="1365.06" cg="243."/>
<eng-data t="1.125" f="1207.29" m="1237.96" cg="243."/>
<eng-data t="2.271" f="1100.23" m="577.705" cg="243."/>
<eng-data t="2.797" f="1055.77" m="294.559" cg="243."/>
<eng-data t="3.076" f="1042.59" m="148.389" cg="243."/>
<eng-data t="3.122" f="996.471" m="124.97" cg="243."/>
<eng-data t="3.23" f="807.059" m="76.3379" cg="243."/>
<eng-data t="3.452" f="289.882" m="15.5367" cg="243."/>
<eng-data t="3.544" f="123.529" m="6.04054" cg="243."/>
<eng-data t="3.685" f="36.235" m="0.416162" cg="243."/>
<eng-data t="3.731" f="0." m="0." cg="243."/>
</data>
</engine>
</engine-list>
</engine-database>

32
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<engine-database>
<engine-list>
<engine mfg="CTI" code="4263-L1350-CS-P" Type="unspecified" dia="75." len="486."
initWt="3570.7" propWt="2024.5" delays="0" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="1303.34" peakThrust="1540.73" throatDia="0." exitDia="0."
Itot="4280.17" burn-time="3.28" massFrac="56.7" Isp="215.59" 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>C-Star 75mm 3G
4263-L1350-CS-P
</comments>
<data>
<eng-data t="0." f="0." m="2024.5" cg="243."/>
<eng-data t="0.016" f="1421.72" m="2019.12" cg="243."/>
<eng-data t="0.034" f="1345.22" m="2007.34" cg="243."/>
<eng-data t="0.049" f="1502.48" m="1997.24" cg="243."/>
<eng-data t="0.081" f="1415.35" m="1975.16" cg="243."/>
<eng-data t="0.21" f="1432.35" m="1888.28" cg="243."/>
<eng-data t="0.453" f="1432.35" m="1723.65" cg="243."/>
<eng-data t="0.809" f="1462.1" m="1479.96" cg="243."/>
<eng-data t="1.07" f="1534.36" m="1295." cg="243."/>
<eng-data t="1.28" f="1540.73" m="1142.27" cg="243."/>
<eng-data t="2.661" f="1283.59" m="219.84" cg="243."/>
<eng-data t="2.843" f="1277.21" m="109.616" cg="243."/>
<eng-data t="2.932" f="1115.7" m="59.2496" cg="243."/>
<eng-data t="3.037" f="488.784" m="19.4066" cg="243."/>
<eng-data t="3.163" f="82.881" m="2.37174" cg="243."/>
<eng-data t="3.284" f="0." m="0." cg="243."/>
</data>
</engine>
</engine-list>
</engine-database>

30
core/resources/datafiles/thrustcurves/Cesaroni_L3200.rse Normal file
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<engine-database>
<engine-list>
<engine mfg="CTI" code="3300-L3200-VM-P" Type="unspecified" dia="75." len="486."
initWt="3263.7" propWt="1658.4" delays="0" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="3127.56" peakThrust="3711.92" throatDia="0." exitDia="0."
Itot="3299.58" burn-time="1.05" massFrac="50.81" Isp="202.88" tDiv="10"
tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."
mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<comments>VMax 75mm 3G
3300-L3200-VM-P
</comments>
<data>
<eng-data t="0." f="0." m="1658.4" cg="243."/>
<eng-data t="0.008" f="3315.23" m="1651.73" cg="243."/>
<eng-data t="0.024" f="2672.96" m="1627.66" cg="243."/>
<eng-data t="0.108" f="2975.21" m="1508.43" cg="243."/>
<eng-data t="0.415" f="3669.42" m="995.789" cg="243."/>
<eng-data t="0.524" f="3711.92" m="793.598" cg="243."/>
<eng-data t="0.644" f="3669.42" m="571.002" cg="243."/>
<eng-data t="0.819" f="3225.5" m="267.774" cg="243."/>
<eng-data t="0.911" f="3022.43" m="123.322" cg="243."/>
<eng-data t="0.937" f="3050.77" m="83.6397" cg="243."/>
<eng-data t="0.957" f="2899.65" m="53.7324" cg="243."/>
<eng-data t="1.022" f="288.076" m="1.66152" cg="243."/>
<eng-data t="1.039" f="51.948" m="0.208877" cg="243."/>
<eng-data t="1.055" f="0." m="0." cg="243."/>
</data>
</engine>
</engine-list>
</engine-database>

29
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<engine-database>
<engine-list>
<engine mfg="CTI" code="3419-L645-GR-P" Type="unspecified" dia="75." len="486."
initWt="3751.8" propWt="2144.1" delays="0" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="637.051" peakThrust="764.97" throatDia="0." exitDia="0." Itot="3433.7"
burn-time="5.39" massFrac="57.15" Isp="163.3" tDiv="10" tStep="-1." tFix="1"
FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10"
cgStep="-1." cgFix="1">
<comments>Green 75mm 3G
3419-L645-GR-P
</comments>
<data>
<eng-data t="0." f="0." m="2144.1" cg="243."/>
<eng-data t="0.05" f="511.243" m="2136.12" cg="243."/>
<eng-data t="0.12" f="647.574" m="2110.79" cg="243."/>
<eng-data t="0.256" f="689.231" m="2054.03" cg="243."/>
<eng-data t="0.425" f="684.497" m="1981.55" cg="243."/>
<eng-data t="1.554" f="736.568" m="1480.64" cg="243."/>
<eng-data t="2.043" f="764.97" m="1251.39" cg="243."/>
<eng-data t="3.075" f="687.337" m="783.453" cg="243."/>
<eng-data t="4.557" f="601.183" m="187.254" cg="243."/>
<eng-data t="4.756" f="550.059" m="115.726" cg="243."/>
<eng-data t="4.985" f="412.781" m="46.8863" cg="243."/>
<eng-data t="5.281" f="69.112" m="2.35197" cg="243."/>
<eng-data t="5.39" f="0." m="0." cg="243."/>
</data>
</engine>
</engine-list>
</engine-database>

27
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<engine-database>
<engine-list>
<engine mfg="CTI" code="2833-L805-WH-P" Type="unspecified" dia="54." len="649."
initWt="2502.5" propWt="1675.2" delays="0" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="746.357" peakThrust="1618.1" throatDia="0." exitDia="0."
Itot="2856.31" burn-time="3.83" massFrac="66.94" Isp="173.87" tDiv="10"
tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."
mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<comments>White 54mm 6GXL
2833-L805-WH-P
</comments>
<data>
<eng-data t="0." f="0." m="1675.2" cg="324.5"/>
<eng-data t="0.012" f="1618.1" m="1669.51" cg="324.5"/>
<eng-data t="0.037" f="1171.8" m="1649.05" cg="324.5"/>
<eng-data t="0.173" f="1027.97" m="1561.32" cg="324.5"/>
<eng-data t="0.388" f="994.125" m="1433.83" cg="324.5"/>
<eng-data t="0.626" f="985.664" m="1295.66" cg="324.5"/>
<eng-data t="2.318" f="886.251" m="366.868" cg="324.5"/>
<eng-data t="3.054" f="448.414" m="78.8087" cg="324.5"/>
<eng-data t="3.464" f="126.91" m="9.63702" cg="324.5"/>
<eng-data t="3.608" f="40.188" m="2.58091" cg="324.5"/>
<eng-data t="3.827" f="0." m="0." cg="324.5"/>
</data>
</engine>
</engine-list>
</engine-database>

30
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<engine-database>
<engine-list>
<engine mfg="CTI" code="2856-L910-CS-P" Type="unspecified" dia="75." len="350."
initWt="2615.8" propWt="1364.3" delays="0" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="879.58" peakThrust="1047.55" throatDia="0." exitDia="0."
Itot="2869.19" burn-time="3.26" massFrac="52.16" Isp="214.45" tDiv="10"
tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."
mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<comments>C-Star 75mm 2G
2856-L910-CS-P
</comments>
<data>
<eng-data t="0." f="0." m="1364.3" cg="175."/>
<eng-data t="0.034" f="858.741" m="1357.36" cg="175."/>
<eng-data t="0.056" f="921.678" m="1348.05" cg="175."/>
<eng-data t="0.305" f="952.448" m="1237.1" cg="175."/>
<eng-data t="0.718" f="983.217" m="1047.03" cg="175."/>
<eng-data t="1.221" f="1047.55" m="804.178" cg="175."/>
<eng-data t="1.642" f="1005.59" m="598.673" cg="175."/>
<eng-data t="1.842" f="973.427" m="504.57" cg="175."/>
<eng-data t="2.951" f="773.427" m="43.9864" cg="175."/>
<eng-data t="3.035" f="584.615" m="16.8649" cg="175."/>
<eng-data t="3.108" f="169.231" m="3.78139" cg="175."/>
<eng-data t="3.152" f="72.727" m="1.25026" cg="175."/>
<eng-data t="3.182" f="27.972" m="0.532027" cg="175."/>
<eng-data t="3.262" f="0." m="0." cg="175."/>
</data>
</engine>
</engine-list>
</engine-database>

13
core/resources/datafiles/thrustcurves/Cesaroni_M2245.eng Normal file
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; Imax Pro75 6GXL
; 9977 M2245-IM-P
9977-M2245-IM-P 75 1025 P 5.309 8.182 CTI
0.043 3045.655
0.136 2629.813
1.393 3003.3
2.168 3007.151
2.708 2972.497
2.837 2883.938
3.152 1955.996
3.397 1409.241
3.878 562.156
4.371 0.0

27
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<engine-database>
<engine-list>
<engine mfg="CTI" code="9977-M2245-IM-P" Type="unspecified" dia="75." len="1025."
initWt="8182." propWt="5309." delays="0" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="2282.85" peakThrust="3045.66" throatDia="0." exitDia="0."
Itot="9978.32" burn-time="4.37" massFrac="64.89" Isp="191.66" 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>Imax Pro75 6GXL
9977 M2245-IM-P
</comments>
<data>
<eng-data t="0." f="0." m="5309." cg="512.5"/>
<eng-data t="0.043" f="3045.66" m="5274.16" cg="512.5"/>
<eng-data t="0.136" f="2629.81" m="5133.75" cg="512.5"/>
<eng-data t="1.393" f="3003.3" m="3250.06" cg="512.5"/>
<eng-data t="2.168" f="3007.15" m="2010.88" cg="512.5"/>
<eng-data t="2.708" f="2972.5" m="1151.88" cg="512.5"/>
<eng-data t="2.837" f="2883.94" m="950.898" cg="512.5"/>
<eng-data t="3.152" f="1956." m="545.32" cg="512.5"/>
<eng-data t="3.397" f="1409.24" m="325.985" cg="512.5"/>
<eng-data t="3.878" f="562.156" m="73.7274" cg="512.5"/>
<eng-data t="4.371" f="0." m="0." cg="512.5"/>
</data>
</engine>
</engine-list>
</engine-database>

30
core/resources/datafiles/thrustcurves/Cesaroni_N2540.rse Normal file
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<engine-database>
<engine-list>
<engine mfg="CTI" code="17907-N2540-GR-P" Type="unspecified" dia="98." len="1239."
initWt="16280.5" propWt="10704.2" delays="0" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="2479.42" peakThrust="2894.98" throatDia="0." exitDia="0."
Itot="17906.4" burn-time="7.22" massFrac="65.75" Isp="170.58" 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>Green 98mm 6GXL
17907-N2540-GR-P
</comments>
<data>
<eng-data t="0." f="0." m="10704.2" cg="619.5"/>
<eng-data t="0.073" f="2586.93" m="10647.8" cg="619.5"/>
<eng-data t="0.11" f="2789.97" m="10588.3" cg="619.5"/>
<eng-data t="0.398" f="2761.96" m="10110.4" cg="619.5"/>
<eng-data t="1.14" f="2761.96" m="8885.29" cg="619.5"/>
<eng-data t="1.73" f="2828.47" m="7899.43" cg="619.5"/>
<eng-data t="2.613" f="2894.98" m="6388.88" cg="619.5"/>
<eng-data t="4.16" f="2747.96" m="3779.65" cg="619.5"/>
<eng-data t="5.666" f="2565.93" m="1387.7" cg="619.5"/>
<eng-data t="5.972" f="2415.4" m="932.099" cg="619.5"/>
<eng-data t="6.338" f="1953.33" m="454.182" cg="619.5"/>
<eng-data t="6.819" f="745.624" m="66.1607" cg="619.5"/>
<eng-data t="7.061" f="101.517" m="4.88518" cg="619.5"/>
<eng-data t="7.222" f="0." m="0." cg="619.5"/>
</data>
</engine>
</engine-list>
</engine-database>

28
core/resources/datafiles/thrustcurves/Cesaroni_O25000.rse Normal file
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<engine-database>
<engine-list>
<engine mfg="CTI" code="O25,000-VM-P" Type="unspecified" dia="132." len="1407."
initWt="23558." propWt="14705." delays="0" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="23414.8" peakThrust="26281.5" throatDia="0." exitDia="0."
Itot="30907.5" burn-time="1.32" massFrac="62.42" Isp="214.33" tDiv="10"
tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."
mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<comments>CTI 30,795-O25,000-VM-P
Single-Use
</comments>
<data>
<eng-data t="0." f="0." m="14705." cg="703.5"/>
<eng-data t="0.008" f="21113.4" m="14664.8" cg="703.5"/>
<eng-data t="0.022" f="24705.9" m="14512.2" cg="703.5"/>
<eng-data t="0.042" f="26281.5" m="14269.6" cg="703.5"/>
<eng-data t="0.067" f="24390.8" m="13968.3" cg="703.5"/>
<eng-data t="0.201" f="24044.1" m="12424.3" cg="703.5"/>
<eng-data t="0.56" f="25052.5" m="8231.4" cg="703.5"/>
<eng-data t="0.927" f="24075.6" m="3942.28" cg="703.5"/>
<eng-data t="1.202" f="22815.1" m="874.738" cg="703.5"/>
<eng-data t="1.25" f="23602.9" m="344.709" cg="703.5"/>
<eng-data t="1.297" f="4852.94" m="26.5524" cg="703.5"/>
<eng-data t="1.32" f="0." m="0." cg="703.5"/>
</data>
</engine>
</engine-list>
</engine-database>

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; Based on NAR Published Data, 7/31/12, C. J. Kobel
E12 24 95 0-4-6-8 0.0359 0.0599 Estes
0.052 5.045
0.096 9.910
0.196 24.144
0.251 31.351
0.287 32.973
0.300 29.910
0.344 17.117
0.370 14.414
0.400 12.973
0.500 11.712
0.600 11.171
0.700 10.631
0.800 10.09
0.900 9.73
1.000 9.55
1.101 9.91
1.200 9.55
1.300 9.73
1.400 9.73
1.500 9.73
1.600 9.73
1.700 9.55
1.800 9.73
1.900 9.73
2.000 9.55
2.100 9.55
2.200 9.73
2.300 9.19
2.375 9.37
2.400 5.95
2.440 0.0

29
core/resources/datafiles/thrustcurves/Estes_E30.eng Normal file
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; Estes E30
; from NAR data sheet updated 08/01/2010
; created by David Moore 08/17/2012
E30 24 70 4-7 .0178 .0470 ESTES
0.01 49
0.02 49
0.05 46
0.10 44
0.20 43
0.25 42
0.30 41
0.35 40
0.40 39
0.45 38
0.50 37
0.55 35
0.60 33
0.65 32
0.70 31
0.75 30
0.80 27
0.85 25
0.90 20
0.91 19
0.93 12
0.95 5
0.97 1
1.00 0
;

36
core/resources/datafiles/thrustcurves/Estes_F26.eng Normal file
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;
;ESTES G80
;From NAR Certification 11/28/2007
;File created 08/17/2012 by David Moore
;Blue Thunder propellant [Relabeled Aerotech]
G80 29 128 7 0.0625 0.128 Estes
0.006 1.2
0.008 7.5
0.010 33.8
0.012 64.6
0.014 62.9
0.016 58.8
0.018 74.9
0.020 85.0
0.022 91.1
0.026 94.0
0.028 98.4
0.032 97.7
0.074 97.3
0.124 95.4
0.376 99.3
0.680 99.4
0.994 91.6
1.246 83.0
1.282 77.4
1.316 62.0
1.360 44.6
1.424 29.1
1.504 21.2
1.598 19.3
1.656 16.3
1.676 13.9
1.678 11.8
1.714 5.1
1.734 1.4
1.808 0.0

37
core/resources/datafiles/thrustcurves/Estes_F50.eng Normal file
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; Estes F50 Blue thunder Porpellant [Relabeled Aerotech]
; 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.
F50 29 98 6 .0379 .0836 Estes
0.012 51.377
0.023 61.197
0.026 66.117
0.044 66.564
0.082 69.685
0.152 73.264
0.208 75.053
0.237 77.279
0.254 76.832
0.272 77.726
0.307 77.726
0.330 76.832
0.336 78.621
0.342 76.832
0.354 79.590
0.363 76.385
0.371 77.756
0.395 76.385
0.447 75.937
0.523 73.711
0.652 68.344
0.810 60.302
0.828 62.539
0.836 58.076
0.901 53.603
1.079 37.074
1.158 29.480
1.196 25.464
1.246 16.976
1.301 9.380
1.430 0.000

16
core/resources/datafiles/thrustcurves/Estes_G40.eng Normal file
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@ -0,0 +1,16 @@
;ESTES G40W [Relabeled Aerotech]
;Entered for ESTES on 8/18/2012 by David Moore
;Original file by Tim VanMilligan
G40W 29 124 7 0.0538 0.123 AeroTech
0.024 74.325
0.057 67.005
0.252 65.879
0.500 63.063
0.765 60.248
1.000 54.054
1.250 47.298
1.502 36.599
1.751 25.338
1.999 12.951
2.121 3.941
2.300 0

16
core/resources/datafiles/thrustcurves/Estes_G40_1.eng Normal file
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;ESTES G40W [Relabeled Aerotech]
;Entered for ESTES on 8/18/2012 by David Moore
;Original file by Tim VanMilligan
G40W 29 124 4-7-10 0.0538 0.123 AeroTech
0.024 74.325
0.057 67.005
0.252 65.879
0.500 63.063
0.765 60.248
1.000 54.054
1.250 47.298
1.502 36.599
1.751 25.338
1.999 12.951
2.121 3.941
2.300 0

19
core/resources/datafiles/thrustcurves/GR_M1025.rse Normal file
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<engine-database>
<engine-list>
<engine mfg="Gorilla_Rocket_Motors" code="M1025WC" Type="reloadable" dia="98."
len="869.95" initWt="10138." propWt="5329." delays="1000" auto-calc-mass="1"
auto-calc-cg="1" avgThrust="1024.39" peakThrust="1780." throatDia="0."
exitDia="0." Itot="9590.88" burn-time="9.36" massFrac="52.56" Isp="183.52"
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="5329." cg="434.975"/>
<eng-data t="0.1" f="1780." m="5279.55" cg="434.975"/>
<eng-data t="0.5" f="1558." m="4908.61" cg="434.975"/>
<eng-data t="3.25641" f="1500." m="2566.87" cg="434.975"/>
<eng-data t="6.17949" f="795.082" m="703.085" cg="434.975"/>
<eng-data t="9.3625" f="0." m="0." cg="434.975"/>
</data>
</engine>
</engine-list>
</engine-database>

22
core/resources/datafiles/thrustcurves/GR_M1465.rse Normal file
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<engine-database>
<engine-list>
<engine mfg="Gorilla_Rocket_Motors" code="M1465BL" Type="reloadable" dia="98."
len="869.95" initWt="9801." propWt="4992." delays="1000" auto-calc-mass="1"
auto-calc-cg="1" avgThrust="1449.69" peakThrust="2219." throatDia="0."
exitDia="0." Itot="7538.4" burn-time="5.2" massFrac="50.93" Isp="153.99"
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="4992." cg="434.975"/>
<eng-data t="0.33" f="1113." m="4870.39" cg="434.975"/>
<eng-data t="1.64957" f="1752.05" m="3618.6" cg="434.975"/>
<eng-data t="3." f="2219." m="1843.01" cg="434.975"/>
<eng-data t="3.51282" f="2100.41" m="1109.59" cg="434.975"/>
<eng-data t="3.98291" f="1823.77" m="498.8" cg="434.975"/>
<eng-data t="4.3" f="1335." m="167.156" cg="434.975"/>
<eng-data t="4.45299" f="334." m="82.6109" cg="434.975"/>
<eng-data t="5.2" f="0." m="0." cg="434.975"/>
</data>
</engine>
</engine-list>
</engine-database>

2
core/resources/datafiles/thrustcurves/Quest_D5_1.eng
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@ -4,7 +4,7 @@
; 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.
D5 20 96 4-6 0.0240 0.451 QUEST
D5 20 96 4-6 0.0240 0.0451 QUEST
0.010 1.014
0.122 2.652
0.172 4.836

39
core/resources/datafiles/thrustcurves/Quest_Micro_Maxx_II.eng Normal file
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; Traced from NAR certification data dated 1-29-2009
MicroMaxxII 6 26 1 5.0E-4 0.0010 Q
0.021 0.015
0.036 0.05
0.043 0.103
0.049 0.198
0.08 1.636
0.092 1.3
0.109 0.995
0.124 0.805
0.133 0.442
0.143 0.301
0.164 0.21
0.186 0.149
0.199 0.183
0.235 0.145
0.256 0.145
0.293 0.149
0.327 0.164
0.367 0.156
0.387 0.175
0.409 0.183
0.431 0.191
0.461 0.21
0.474 0.202
0.49 0.217
0.505 0.175
0.513 0.198
0.537 0.172
0.553 0.175
0.602 0.156
0.623 0.175
0.644 0.183
0.674 0.21
0.689 0.191
0.697 0.229
0.731 0.21
0.753 0.092
0.771 0.0