hongshaorou/openrocket
1
0
Fork 0
Code Issues Pull Requests Packages Projects Releases Wiki Activity

Merge pull request #231 from openrocket/upstream-master

Browse Source 
Updated thrustcurves.
This commit is contained in:
kruland2607 2015-03-23 07:05:29 -05:00
commit 3ed9a02356
31 changed files with 914 additions and 325 deletions
Show Stats Download Patch File Download Diff File Expand all files Collapse all files

26
core/resources-src/datafiles/thrustcurves/manual/AT_F101T.eng Normal file
View File

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

87
core/resources-src/datafiles/thrustcurves/thrustcurve.org/00INDEX.txt
View File

@ -1,5 +1,5 @@
Rocket motor simulation data downloaded from ThrustCurve.org.
This ZIP file contains 1645 simulator data files.
This ZIP file contains 1656 simulator data files.
For more info, please see http://www.thrustcurve.org/
AMW_I195.eng
@ -7434,14 +7434,14 @@ Cesaroni_M1590.eng
Designation: 7545M1590-P
Data Format: RASP
Data Source: cert
Contributor: Andre Choquette
Contributor: Mark Koelsch
Cesaroni_M1590.rse
Manufacturer: Cesaroni Technology
Designation: 7545M1590-P
Data Format: RockSim
Data Source: cert
Contributor: Andre Choquette
Contributor: Mark Koelsch
Cesaroni_M1670.eng
Manufacturer: Cesaroni Technology
@ -9394,7 +9394,7 @@ Estes_B4.eng
Designation: B4
Data Format: RASP
Data Source: user
Contributor: John Coker
Contributor: Nicholas Domansky
Estes_B4.rse
Manufacturer: Estes Industries
@ -9403,6 +9403,13 @@ Estes_B4.rse
Data Source: user
Contributor: John Coker
Estes_B4_1.eng
Manufacturer: Estes Industries
Designation: B4
Data Format: RASP
Data Source: user
Contributor: John Coker
Estes_B6.eng
Manufacturer: Estes Industries
Designation: B6
@ -9450,7 +9457,7 @@ Estes_C6.eng
Designation: C6
Data Format: RASP
Data Source: user
Contributor: John Coker
Contributor: Nicholas Domansky
Estes_C6.rse
Manufacturer: Estes Industries
@ -9459,6 +9466,13 @@ Estes_C6.rse
Data Source: user
Contributor: John Coker
Estes_C6_1.eng
Manufacturer: Estes Industries
Designation: C6
Data Format: RASP
Data Source: user
Contributor: John Coker
Estes_D11.eng
Manufacturer: Estes Industries
Designation: D11
@ -9732,6 +9746,13 @@ GR_L1065.eng
Data Source: mfr
Contributor: John Coker
GR_L1112.eng
Manufacturer: Gorilla Rocket Motors
Designation: L1112BT
Data Format: RASP
Data Source: cert
Contributor: Mark Koelsch
GR_L1150.rse
Manufacturer: Gorilla Rocket Motors
Designation: L1150WC
@ -9802,6 +9823,13 @@ GR_M1665.eng
Data Source: mfr
Contributor: John Coker
GR_M1952.eng
Manufacturer: Gorilla Rocket Motors
Designation: M1952BT
Data Format: RASP
Data Source: cert
Contributor: Mark Koelsch
GR_O2700.eng
Manufacturer: Gorilla Rocket Motors
Designation: O2700BL
@ -10635,6 +10663,13 @@ Loki_J1000.rse
Data Source: mfr
Contributor: Mark Koelsch
Loki_J1026.eng
Manufacturer: Loki Research
Designation: J1026 CT
Data Format: RASP
Data Source: cert
Contributor: Mark Koelsch
Loki_J175.eng
Manufacturer: Loki Research
Designation: J175-LW
@ -10754,6 +10789,13 @@ Loki_J820.rse
Data Source: user
Contributor: John Coker
Loki_K1127.eng
Manufacturer: Loki Research
Designation: K1127LB
Data Format: RASP
Data Source: cert
Contributor: Mark Koelsch
Loki_K250.eng
Manufacturer: Loki Research
Designation: K250-LW
@ -10782,6 +10824,13 @@ Loki_K350.rse
Data Source: user
Contributor: John Coker
Loki_K527.eng
Manufacturer: Loki Research
Designation: K527LR
Data Format: RASP
Data Source: cert
Contributor: Mark Koelsch
Loki_K690.eng
Manufacturer: Loki Research
Designation: K690-SF
@ -10852,6 +10901,13 @@ Loki_L780.eng
Data Source: mfr
Contributor: John Coker
Loki_L840.eng
Manufacturer: Loki Research
Designation: L840CT
Data Format: RASP
Data Source: cert
Contributor: Mark Koelsch
Loki_L930.eng
Manufacturer: Loki Research
Designation: L930-LW
@ -10873,6 +10929,13 @@ Loki_M1200.eng
Data Source: mfr
Contributor: John Coker
Loki_M1650.eng
Manufacturer: Loki Research
Designation: M1650LC
Data Format: RASP
Data Source: cert
Contributor: Mark Koelsch
Loki_M1882.eng
Manufacturer: Loki Research
Designation: M1882-LW
@ -10887,6 +10950,13 @@ Loki_M1882.rse
Data Source: user
Contributor: John Coker
Loki_M1969.eng
Manufacturer: Loki Research
Designation: M1969SF
Data Format: RASP
Data Source: cert
Contributor: Mark Koelsch
Loki_M2550.eng
Manufacturer: Loki Research
Designation: M2550-LB
@ -10915,6 +10985,13 @@ Loki_M3000.rse
Data Source: mfr
Contributor: Mark Koelsch
Loki_M3464.eng
Manufacturer: Loki Research
Designation: M3464LB
Data Format: RASP
Data Source: cert
Contributor: Mark Koelsch
Loki_M900.rse
Manufacturer: Loki Research
Designation: M900-LR

60
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AeroTech_G25.eng
View File

@ -1,41 +1,19 @@
;
;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
G25W-10A 29 152.4 10 0.097 0.17 AT
0.01 38.046
0.029 21.768
0.11 30.475
0.239 35.775
0.496 40.696
0.568 42.116
0.592 45.429
0.749 46.186
0.997 45.713
1.255 44.198
1.498 39.939
1.999 31.421
2.501 23.093
3.006 14.196
3.503 7.288
3.999 4.07
4.371 1.988
4.414 0.0

60
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AeroTech_G25_1.eng
View File

@ -1,19 +1,41 @@
G25W-10A 29 152.4 10 0.097 0.17 AT
0.01 38.046
0.029 21.768
0.11 30.475
0.239 35.775
0.496 40.696
0.568 42.116
0.592 45.429
0.749 46.186
0.997 45.713
1.255 44.198
1.498 39.939
1.999 31.421
2.501 23.093
3.006 14.196
3.503 7.288
3.999 4.07
4.371 1.988
4.414 0.0
;
;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

43
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AeroTech_H45.eng
View File

@ -1,30 +1,13 @@
; AeroTech H45W
; converted from TMT test stand data 1998 (www.tripoli.org)
; provided by ThrustCurve.org (www.thrustcurve.org)
H45W 38 194 0 0.193984 0.294784 AT
0.141 62.554
0.424 63.504
0.707 65.913
0.992 68.370
1.276 69.315
1.559 68.523
1.843 67.231
2.127 65.705
2.411 63.154
2.695 59.210
2.979 55.600
3.264 50.790
3.547 45.237
3.830 39.835
4.115 34.562
4.399 29.213
4.682 24.720
4.967 20.616
5.251 17.475
5.534 14.498
5.818 12.697
6.102 10.792
6.386 9.229
6.670 7.754
6.954 6.075
7.239 0.000
; From AT DMS announcement May 2014.
H45 38 202.7 10 0.18 0.364 AT
0.04 84.004
0.854 86.004
1.377 84.804
2.046 79.204
2.69 66.003
3.286 51.603
4.414 28.401
5.042 16.001
5.429 9.2
6.113 6.4
6.186 0.0

43
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AeroTech_H45_1.eng
View File

@ -1,13 +1,30 @@
; From AT DMS announcement May 2014.
H45 38 202.7 10 0.18 0.364 AT
0.04 84.004
0.854 86.004
1.377 84.804
2.046 79.204
2.69 66.003
3.286 51.603
4.414 28.401
5.042 16.001
5.429 9.2
6.113 6.4
6.186 0.0
; AeroTech H45W
; converted from TMT test stand data 1998 (www.tripoli.org)
; provided by ThrustCurve.org (www.thrustcurve.org)
H45W 38 194 0 0.193984 0.294784 AT
0.141 62.554
0.424 63.504
0.707 65.913
0.992 68.370
1.276 69.315
1.559 68.523
1.843 67.231
2.127 65.705
2.411 63.154
2.695 59.210
2.979 55.600
3.264 50.790
3.547 45.237
3.830 39.835
4.115 34.562
4.399 29.213
4.682 24.720
4.967 20.616
5.251 17.475
5.534 14.498
5.818 12.697
6.102 10.792
6.386 9.229
6.670 7.754
6.954 6.075
7.239 0.000

45
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AeroTech_I65.eng
View File

@ -1,30 +1,15 @@
; AeroTech I65W
; converted from TMT test stand data 1997 (www.tripoli.org)
; provided by ThrustCurve.org (www.thrustcurve.org)
I65W 54 235 0 0.41216 0.7616 AT
0.180 125.414
0.544 139.304
0.908 145.369
1.273 148.283
1.638 146.745
2.002 139.049
2.367 131.200
2.731 123.276
3.096 113.454
3.460 102.368
3.825 90.210
4.190 78.084
4.554 66.812
4.919 55.780
5.283 47.281
5.648 39.154
6.012 32.528
6.377 27.069
6.742 22.099
7.106 18.095
7.471 14.819
7.835 12.097
8.200 9.763
8.565 7.875
8.929 5.999
9.294 0.000
; From AT DMS announcement May 2014.
I65 54 218 10 0.377 0.752 AT
0.023 148.274
0.211 196.341
0.398 167.827
0.797 149.903
1.395 135.239
2.238 122.204
3.199 99.392
4.711 69.249
5.367 48.882
6.246 29.329
6.926 15.479
7.395 11.406
8.496 0.0

45
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AeroTech_I65_1.eng
View File

@ -1,15 +1,30 @@
; From AT DMS announcement May 2014.
I65 54 218 10 0.377 0.752 AT
0.023 148.274
0.211 196.341
0.398 167.827
0.797 149.903
1.395 135.239
2.238 122.204
3.199 99.392
4.711 69.249
5.367 48.882
6.246 29.329
6.926 15.479
7.395 11.406
8.496 0.0
; AeroTech I65W
; converted from TMT test stand data 1997 (www.tripoli.org)
; provided by ThrustCurve.org (www.thrustcurve.org)
I65W 54 235 0 0.41216 0.7616 AT
0.180 125.414
0.544 139.304
0.908 145.369
1.273 148.283
1.638 146.745
2.002 139.049
2.367 131.200
2.731 123.276
3.096 113.454
3.460 102.368
3.825 90.210
4.190 78.084
4.554 66.812
4.919 55.780
5.283 47.281
5.648 39.154
6.012 32.528
6.377 27.069
6.742 22.099
7.106 18.095
7.471 14.819
7.835 12.097
8.200 9.763
8.565 7.875
8.929 5.999
9.294 0.000

79
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AeroTech_M1780.eng
View File

@ -1,37 +1,42 @@
; M1780NT Redesign and recert
M1780NT-PS 75 665 P 2.46 4.649 AT
0.014 1112.055
0.015 1497.932
0.022 1783.542
0.036 2105.612
0.047 2157.265
0.066 2169.419
0.104 2123.843
0.14 2108.651
0.164 2135.996
0.197 2129.92
0.238 2157.265
0.263 2205.88
0.274 2169.419
0.312 2145.112
0.411 2111.689
0.595 2081.305
0.899 2075.228
1.299 2047.883
1.601 1996.23
1.899 1938.5
2.058 1889.886
2.201 1813.926
2.3 1753.158
2.423 1701.505
2.467 1622.506
2.508 1555.662
2.566 1336.897
2.62 1112.055
2.67 893.29
2.724 668.448
2.755 568.181
2.812 486.144
2.9 267.379
2.999 75.96
3.029 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

65
core/resources-src/datafiles/thrustcurves/thrustcurve.org/AeroTech_M1780_1.eng
View File

@ -1,42 +1,23 @@
; 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
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

27
core/resources-src/datafiles/thrustcurves/thrustcurve.org/Cesaroni_F31.rse Normal file
View File

@ -0,0 +1,27 @@
<engine-database>
<engine-list>
<engine mfg="CTI" code="56-F31-CL-12A" Type="unspecified" dia="24." len="98.0008"
initWt="102." propWt="32." delays="13,9,7,5,3" auto-calc-mass="1"
auto-calc-cg="1" avgThrust="30.41" peakThrust="64.053" throatDia="0."
exitDia="0." Itot="55.589" burn-time="1.83" massFrac="31.37" Isp="177.14"
tDiv="10" tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10"
mStep="-1." mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<comments>CTI 56-F31-CL-12A</comments>
<data>
<eng-data t="0." f="0." m="32." cg="49."/>
<eng-data t="0.001" f="3.483" m="31.999" cg="49."/>
<eng-data t="0.023" f="64.053" m="31.5714" cg="49."/>
<eng-data t="0.05" f="31.347" m="30.83" cg="49."/>
<eng-data t="0.059" f="28.459" m="30.6751" cg="49."/>
<eng-data t="0.095" f="32.027" m="30.0483" cg="49."/>
<eng-data t="0.212" f="36.189" m="27.7511" cg="49."/>
<eng-data t="0.344" f="37.549" m="24.9496" cg="49."/>
<eng-data t="1.567" f="26.165" m="2.5217" cg="49."/>
<eng-data t="1.631" f="26.93" m="1.54365" cg="49."/>
<eng-data t="1.663" f="25.316" m="1.06244" cg="49."/>
<eng-data t="1.785" f="3.653" m="0.0452111" cg="49."/>
<eng-data t="1.828" f="0." m="0." cg="49."/>
</data>
</engine>
</engine-list>
</engine-database>

47
core/resources-src/datafiles/thrustcurves/thrustcurve.org/Cesaroni_M1590.eng
View File

@ -1,21 +1,28 @@
; Pro75-6G 7545M1590-CL P
M1590-CL 75 893 P 3.1590000000000003 5.223 CTI
0.028 1210.592
0.059 2024.222
0.163 2235.371
0.214 2302.939
0.492 2153.727
0.767 2091.79
1.015 2103.051
1.335 2083.344
1.571 2029.852
2.366 1779.288
3.488 1534.354
3.755 1030.41
3.895 960.027
4.12 650.341
4.207 591.219
4.44 340.655
4.665 199.888
4.778 90.091
M1590 75 893 P 3.59 6.0760000000000005 CTI
0.053 2045.469
0.119 2130.875
0.133 2220.551
0.226 2305.957
0.363 2241.903
0.438 2177.849
0.571 2130.875
0.748 2092.443
0.973 2088.172
1.225 2100.983
1.433 2079.632
1.597 2032.659
1.995 1883.198
2.411 1759.36
3.362 1567.197
3.491 1533.035
3.721 1076.113
3.769 1012.059
3.871 973.626
3.946 896.761
4.074 687.517
4.132 640.544
4.203 619.192
4.504 294.65
4.641 226.325
4.716 170.812
4.8 0.0

12
core/resources-src/datafiles/thrustcurves/thrustcurve.org/Cesaroni_M1590.rse
View File

@ -1,11 +1,11 @@
<engine-database>
<engine-list>
<engine mfg="CTI" code="M1590-CL" Type="unspecified" dia="75." len="893." initWt="5223."
propWt="3159." delays="0" auto-calc-mass="1" auto-calc-cg="1" avgThrust="1574.92"
peakThrust="2302.94" throatDia="0." exitDia="0." Itot="7559.63" burn-time="4.8"
massFrac="60.48" Isp="244.02" tDiv="10" tStep="-1." tFix="1" FDiv="10"
FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10" cgStep="-1."
cgFix="1">
<engine mfg="Cesaroni Technology Inc." code="M1590-CL" Type="reloadable" dia="75."
len="893." initWt="6076." propWt="3590." delays="1000" auto-calc-mass="1"
auto-calc-cg="1" avgThrust="1574.92" peakThrust="2302.94" throatDia="0."
exitDia="0." Itot="7559.63" burn-time="4.8" massFrac="60.48" Isp="244.02"
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>Pro75-6G 7545M1590-CL P</comments>
<data>
<eng-data t="0." f="0." m="3159." cg="446.5"/>

65
core/resources-src/datafiles/thrustcurves/thrustcurve.org/Estes_B4.eng
View File

@ -1,34 +1,31 @@
;
;Estes B4 RASP.ENG file made from NAR published data
;File produced October 3, 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.
B4 18 70 2-4 0.006 0.0189 Estes
0.02 0.418
0.04 1.673
0.065 4.076
0.085 6.69
0.105 9.304
0.119 11.496
0.136 12.75
0.153 11.916
0.173 10.666
0.187 9.304
0.198 7.214
0.207 5.645
0.226 4.809
0.258 4.182
0.326 3.763
0.422 3.554
0.549 3.345
0.665 3.345
0.776 3.345
0.863 3.345
0.94 3.449
0.991 3.449
1.002 2.404
1.01 1.254
1.03 0
; B4-4
B4-4 18 70 P 0.006 0.0195 E
0.058 2.361
0.102 2.921
0.122 3.797
0.15 5.866
0.18 8.373
0.199 9.882
0.208 10.88
0.216 11.367
0.238 11.245
0.245 10.832
0.262 8.982
0.293 6.134
0.322 5.306
0.357 4.917
0.388 4.795
0.416 4.746
0.46 4.625
0.502 4.576
0.544 4.357
0.575 4.503
0.605 4.527
0.674 4.552
0.731 4.454
0.88 4.454
0.915 4.503
0.96 4.406
1.0 4.065
1.047 2.556
1.049 0.0

34
core/resources-src/datafiles/thrustcurves/thrustcurve.org/Estes_B4_1.eng Normal file
View File

@ -0,0 +1,34 @@
;
;Estes B4 RASP.ENG file made from NAR published data
;File produced October 3, 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.
B4 18 70 2-4 0.006 0.0189 Estes
0.02 0.418
0.04 1.673
0.065 4.076
0.085 6.69
0.105 9.304
0.119 11.496
0.136 12.75
0.153 11.916
0.173 10.666
0.187 9.304
0.198 7.214
0.207 5.645
0.226 4.809
0.258 4.182
0.326 3.763
0.422 3.554
0.549 3.345
0.665 3.345
0.776 3.345
0.863 3.345
0.94 3.449
0.991 3.449
1.002 2.404
1.01 1.254
1.03 0

56
core/resources-src/datafiles/thrustcurves/thrustcurve.org/Estes_C6.eng
View File

@ -1,33 +1,23 @@
;
;Estes C6 RASP.ENG file made from NAR published data
;File produced October 3, 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.
C6 18 70 0-3-5-7 0.0108 0.0231 Estes
0.031 0.946
0.092 4.826
0.139 9.936
0.192 14.09
0.209 11.446
0.231 7.381
0.248 6.151
0.292 5.489
0.37 4.921
0.475 4.448
0.671 4.258
0.702 4.542
0.723 4.164
0.85 4.448
1.063 4.353
1.211 4.353
1.242 4.069
1.303 4.258
1.468 4.353
1.656 4.448
1.821 4.448
1.834 2.933
1.847 1.325
1.86 0
; C6-0
C6-0 18 70 P 0.012480000000000002 0.0227 E
0.014 0.633
0.026 1.533
0.067 2.726
0.099 5.136
0.15 9.103
0.183 11.465
0.207 11.635
0.219 11.391
0.262 6.377
0.333 5.014
0.349 5.209
0.392 4.722
0.475 4.771
0.653 4.746
0.913 4.673
1.366 4.625
1.607 4.625
1.745 4.868
1.978 4.795
2.023 0.828
2.024 0.0

33
core/resources-src/datafiles/thrustcurves/thrustcurve.org/Estes_C6_1.eng Normal file
View File

@ -0,0 +1,33 @@
;
;Estes C6 RASP.ENG file made from NAR published data
;File produced October 3, 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.
C6 18 70 0-3-5-7 0.0108 0.0231 Estes
0.031 0.946
0.092 4.826
0.139 9.936
0.192 14.09
0.209 11.446
0.231 7.381
0.248 6.151
0.292 5.489
0.37 4.921
0.475 4.448
0.671 4.258
0.702 4.542
0.723 4.164
0.85 4.448
1.063 4.353
1.211 4.353
1.242 4.069
1.303 4.258
1.468 4.353
1.656 4.448
1.821 4.448
1.834 2.933
1.847 1.325
1.86 0

30
core/resources-src/datafiles/thrustcurves/thrustcurve.org/GR_L1112.eng Normal file
View File

@ -0,0 +1,30 @@
L1112BT 75 497.8 P 1.8 3.628 Gorilla
0.05 1131.791
0.071 1174.3
0.113 1176.957
0.176 1211.495
0.263 1293.855
0.397 1145.075
0.493 1129.134
0.786 1182.27
1.062 1254.003
1.078 1232.749
1.229 1275.258
1.308 1254.003
1.492 1283.228
2.002 1293.855
2.236 1299.169
2.345 1283.228
2.545 1227.435
2.608 1198.211
2.688 1190.24
2.759 1206.181
2.809 1168.986
2.884 892.68
2.922 672.167
3.009 504.789
3.223 225.827
3.26 108.928
3.331 37.195
3.44 5.314
3.595 0.0

33
core/resources-src/datafiles/thrustcurves/thrustcurve.org/GR_M1952.eng Normal file
View File

@ -0,0 +1,33 @@
M1952BT 75 784.9 P 2.97 5.4430000000000005 Gorilla
0.025 1639.097
0.033 2397.644
0.046 2100.59
0.075 2519.648
0.096 2599.215
0.104 2689.392
0.187 2689.392
0.228 2620.434
0.274 2445.384
0.316 2328.685
0.403 2275.64
0.523 2291.553
1.001 2339.294
1.188 2344.598
1.499 2328.685
1.637 2302.162
1.794 2270.335
2.093 2238.508
2.193 2206.681
2.243 2143.027
2.368 1777.015
2.505 1310.217
2.525 1241.258
2.584 1220.04
2.609 1119.254
2.663 960.118
2.733 763.851
2.8 567.584
2.87 413.753
2.987 238.703
3.178 63.654
3.41 0.0

27
core/resources-src/datafiles/thrustcurves/thrustcurve.org/Loki_J1026.eng Normal file
View File

@ -0,0 +1,27 @@
J1026 38 625.5 P 0.616 1.172 Loki
0.019 62.798
0.034 795.446
0.045 1167.004
0.07 1182.703
0.149 1153.921
0.249 1146.071
0.4 1161.77
0.49 1185.32
0.6 1193.17
0.8 1180.087
0.851 1172.237
0.899 1169.62
0.922 1159.154
0.947 1167.004
0.979 1127.755
1.009 1067.573
1.089 669.85
1.13 486.688
1.142 468.371
1.151 408.19
1.161 316.609
1.176 222.411
1.201 128.213
1.227 65.415
1.264 26.166
1.297 0.0

37
core/resources-src/datafiles/thrustcurves/thrustcurve.org/Loki_K1127.eng Normal file
View File

@ -0,0 +1,37 @@
K1127LB 38 625.5 P 0.624 1.172 Loki
0.009 77.978
0.021 1002.962
0.033 1368.654
0.045 1210.008
0.058 1365.965
0.067 1263.786
0.08 1360.587
0.092 1255.719
0.105 1331.009
0.117 1242.275
0.13 1312.186
0.142 1261.097
0.155 1304.12
0.167 1261.097
0.218 1290.675
0.395 1325.631
0.542 1368.654
0.689 1392.854
0.726 1382.098
0.755 1344.453
0.814 1110.518
0.867 949.184
0.874 1099.763
0.883 962.629
0.908 847.006
0.989 548.537
0.997 363.002
1.003 715.249
1.014 494.759
1.048 406.025
1.091 352.247
1.152 228.557
1.198 158.645
1.244 69.912
1.286 32.267
1.37 0.0

27
core/resources-src/datafiles/thrustcurves/thrustcurve.org/Loki_K527.eng Normal file
View File

@ -0,0 +1,27 @@
K527LR 54 492.1 P 1.0150000000000001 1.973 Loki
0.023 87.866
0.051 624.477
0.06 701.36
0.079 759.414
0.125 707.636
0.176 682.531
0.269 654.288
0.501 649.581
1.01 644.874
1.265 640.167
1.52 646.443
1.701 643.305
2.035 618.201
2.526 567.991
2.827 539.749
2.943 530.335
2.999 513.075
3.04 442.468
3.115 356.171
3.309 219.665
3.481 91.004
3.546 59.623
3.652 43.933
3.791 37.657
3.967 10.983
4.129 0.0

25
core/resources-src/datafiles/thrustcurves/thrustcurve.org/Loki_L840.eng Normal file
View File

@ -0,0 +1,25 @@
L840CT 75 498 P 2.074 3.748 Loki
0.021 889.644
0.046 1182.485
0.077 1082.4
0.139 978.608
0.303 971.195
0.662 1015.677
1.011 1108.348
1.33 1149.124
1.689 1189.899
1.971 1163.951
2.089 1145.417
2.3 1034.211
2.633 893.351
2.823 822.921
3.455 656.112
3.737 596.803
3.891 585.682
3.984 385.512
4.112 355.858
4.215 203.877
4.292 140.86
4.384 103.792
4.589 63.016
4.8 0.0

22
core/resources-src/datafiles/thrustcurves/thrustcurve.org/Loki_M1650.eng Normal file
View File

@ -0,0 +1,22 @@
M1650LC 76 784.2 P 3.23 5.63 Loki
0.015 1912.965
0.046 3779.835
0.097 3149.862
0.132 2865.606
0.183 2642.811
0.295 2458.429
0.407 2350.873
0.509 2297.095
0.91 2097.347
1.495 1920.648
1.612 1882.235
2.772 1336.771
3.266 1044.832
3.342 960.324
3.398 860.45
3.505 798.989
3.606 629.972
3.81 361.082
3.901 238.16
4.008 153.652
4.613 0.0

28
core/resources-src/datafiles/thrustcurves/thrustcurve.org/Loki_M1969.eng Normal file
View File

@ -0,0 +1,28 @@
M1969SF 75 1038 P 4.266 7.189 Loki
0.036 263.323
0.044 1504.064
0.075 2204.77
0.087 2356.515
0.186 2204.77
0.23 2280.643
0.274 2240.475
0.503 2347.589
1.003 2432.388
1.058 2454.703
1.495 2307.421
2.002 2236.012
2.315 2186.918
2.501 2182.454
2.628 2169.065
2.815 2244.938
2.882 2191.381
3.045 1338.929
3.096 1142.553
3.164 1044.365
3.267 964.029
3.378 807.821
3.5 504.33
3.639 267.786
3.77 102.651
3.881 22.315
3.96 0.0

25
core/resources-src/datafiles/thrustcurves/thrustcurve.org/Loki_M3464.eng Normal file
View File

@ -0,0 +1,25 @@
M3400LB 76 1038.2 P 4.464 7.597 Loki
0.007 4907.495
0.02 4008.216
0.047 3866.9
0.35 3866.9
0.502 3866.9
0.579 3892.594
1.239 4277.999
1.808 4303.693
1.886 4303.693
1.919 4188.071
2.0 3404.414
2.064 2916.234
2.152 2569.369
2.242 2569.369
2.283 2440.901
2.347 1965.567
2.384 1541.621
2.434 1104.829
2.485 835.045
2.545 719.423
2.596 475.333
2.717 205.55
2.862 51.387
2.976 0.0

35
core/resources-src/datafiles/thrustcurves/thrustcurve.org/Quest_Micro_Maxx.eng Normal file
View File

@ -0,0 +1,35 @@
; @File: q003.txt, @Pts-I: 769, @Pts-O: 31, @Sm: 0, @CO: 0%
; @TI: 0.1991613, @TIa: 0.1991608, @TIe: +0.1%, @ThMax: 1.624927, @ThAvg: 0.255335, @Tb: 0.78
; Exported using ThrustCurveTool, www.ThrustGear.com
MAXXII 0 0 0.76 0.0 0.0 QUEST
0.026 0.0394607
0.036 0.1214556
0.04 0.206028
0.05 0.444676
0.056 0.680251
0.06 0.899565
0.066 1.358816
0.068 1.475611
0.07 1.56653
0.074 1.624927
0.088 1.190166
0.112 0.830955
0.126 0.439917
0.134 0.319751
0.144 0.248959
0.174 0.1656754
0.206 0.1918503
0.258 0.1262147
0.342 0.1601231
0.366 0.1386081
0.384 0.1794569
0.494 0.218422
0.546 0.1540751
0.56 0.178168
0.608 0.1523896
0.682 0.209499
0.698 0.1837202
0.712 0.220206
0.742 0.209003
0.768 0.040353
0.785 0

35
core/resources-src/datafiles/thrustcurves/thrustcurve.org/Quest_Micro_Maxx_1.eng Normal file
View File

@ -0,0 +1,35 @@
; @File: q0016.txt, @Pts-I: 815, @Pts-O: 31, @Sm: 0, @CO: 3%
; @TI: 0.1497473, @TIa: 0.1488623, @TIe: -0.06%, @ThMax: 2.09889, @ThAvg: 0.1862529, @Tb: 0.804
; Exported using ThrustCurveTool, www.ThrustGear.com
1/8A0.2 0 0 0.81 0.0 0.0 QUEST
0.016 0.0530363
0.02 0.0985533
0.024 0.176654
0.03 0.415869
0.032 0.434918
0.038 0.657991
0.052 1.247306
0.058 1.453536
0.064 1.700872
0.066 1.755612
0.07 1.951716
0.074 2.06541
0.076 2.09889
0.078 2.09889
0.08 2.02811
0.082 1.911814
0.084 1.619262
0.086 1.151861
0.088 0.728272
0.09 0.433614
0.092 0.292953
0.098 0.217459
0.154 0.224377
0.172 0.150186
0.196 0.0998567
0.23 0.078602
0.414 0.0625608
0.7559 0.082111
0.8219 0.0607562
0.8339 0.0208536
0.834 0

49
core/resources-src/datafiles/thrustcurves/thrustcurve.org/Quest_Micro_Maxx_1.rse Normal file
View File

@ -0,0 +1,49 @@
<engine-database>
<engine-list>
<engine FDiv="10" FFix="1" FStep="-1." Isp="60.9" Itot="0.299" Type="single-use" auto-calc-cg="1" auto-calc-mass="1" avgThrust="0.452" burn-time="0.66" cgDiv="10" cgFix="1" cgStep="-1." code="Micro Maxx II" delays="1" dia="6." exitDia="0." initWt="1.2" len="26." mDiv="10" mFix="1" mStep="-1." massFrac="41.67" mfg="Quest" peakThrust="3.21" propWt="0.5" tDiv="10" tFix="1" tStep="-1." throatDia="0.">
<comments>QUEST MICROMAXX II RASP.ENG file made from NAR published data
File produced Dec 29, 2001
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="13." f="0." m="0.5" t="0."/>
<eng-data cg="13." f="0.16" m="0.498928" t="0.008"/>
<eng-data cg="13." f="0.482" m="0.493554" t="0.018"/>
<eng-data cg="13." f="0.993" m="0.486144" t="0.024"/>
<eng-data cg="13." f="1.534" m="0.473451" t="0.03"/>
<eng-data cg="13." f="2.032" m="0.461509" t="0.034"/>
<eng-data cg="13." f="2.397" m="0.454093" t="0.036"/>
<eng-data cg="13." f="2.543" m="0.43755" t="0.04"/>
<eng-data cg="13." f="3.025" m="0.40958" t="0.046"/>
<eng-data cg="13." f="3.21" m="0.37826" t="0.052"/>
<eng-data cg="13." f="2.864" m="0.342664" t="0.059"/>
<eng-data cg="13." f="2.191" m="0.300344" t="0.069"/>
<eng-data cg="13." f="1.094" m="0.270091" t="0.08"/>
<eng-data cg="13." f="0.539" m="0.260521" t="0.087"/>
<eng-data cg="13." f="0.378" m="0.256683" t="0.092"/>
<eng-data cg="13." f="0.304" m="0.248689" t="0.106"/>
<eng-data cg="13." f="0.26" m="0.233107" t="0.139"/>
<eng-data cg="13." f="0.303" m="0.215196" t="0.177"/>
<eng-data cg="13." f="0.287" m="0.192474" t="0.223"/>
<eng-data cg="13." f="0.243" m="0.176944" t="0.258"/>
<eng-data cg="13." f="0.198" m="0.165868" t="0.288"/>
<eng-data cg="13." f="0.27" m="0.143143" t="0.346"/>
<eng-data cg="13." f="0.298" m="0.116513" t="0.402"/>
<eng-data cg="13." f="0.254" m="0.112354" t="0.411"/>
<eng-data cg="13." f="0.312" m="0.10335" t="0.43"/>
<eng-data cg="13." f="0.282" m="0.0859449" t="0.465"/>
<eng-data cg="13." f="0.238" m="0.0694017" t="0.503"/>
<eng-data cg="13." f="0.281" m="0.0637531" t="0.516"/>
<eng-data cg="13." f="0.28" m="0.0421482" t="0.562"/>
<eng-data cg="13." f="0.294" m="0.0137954" t="0.621"/>
<eng-data cg="13." f="0.279" m="0.00420109" t="0.641"/>
<eng-data cg="13." f="0.176" m="0.00191552" t="0.647"/>
<eng-data cg="13." f="0." m="-0." t="0.66"/>
</data>
</engine>
</engine-list>
</engine-database>

39
core/resources-src/datafiles/thrustcurves/thrustcurve.org/Quest_Micro_Maxx_2.eng Normal file
View File

@ -0,0 +1,39 @@
; Traced from NAR certification data dated 1-29-2009
MicroMaxxII 6 26 NE-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

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

Binary file not shown.