Merge pull request #190 from kruland2607/master

Updated AT F44, G74, J170 and GR O2700 thrustcurves.
This commit is contained in:
kruland2607 2014-03-18 14:01:56 -05:00
commit 790999ea68
5 changed files with 134 additions and 0 deletions

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; F44W Economax
F44W 24 70 4-8 0.0197 0.048 AT
0.02 2.676
0.026 6.02
0.034 11.204
0.063 24.917
0.135 59.031
0.15 61.372
0.2 63.212
0.299 65.218
0.4 65.051
0.5 63.379
0.6 58.529
0.668 55.017
0.686 53.68
0.687 54.014
0.7 49.165
0.719 43.813
0.774 22.074
0.795 13.211
0.812 7.86
0.825 4.515
0.854 2.007
0.899 0.167
0.998 0.0

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; G74W Economax
G74W 29 83 4-6-9 0.039299999999999995 0.08700000000000001 AT
0.023 6.551
0.05 21.838
0.088 44.852
0.124 67.362
0.135 71.561
0.148 74.417
0.197 80.128
0.248 85.0
0.298 87.52
0.397 89.704
0.499 91.215
0.6 90.375
0.699 90.375
0.751 89.536
0.8 87.856
0.9 84.496
0.954 82.144
0.971 81.808
0.987 79.96
1.002 76.433
1.023 67.194
1.065 44.516
1.094 22.174
1.107 15.287
1.126 6.887
1.138 3.36
1.157 1.344
1.18 0.168
1.192 0.0

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; By: J.M.Recuenco (c)2014
; Software: ThrustCurve Tracer v1.0.
; Source: Curve from www.thrustcurve.org
; Propellant: Hybrid
; Trademark: Aerotech High Power Reload
; Hardware: RMS-54/1280-3-JET
J170H 54 709 1000 0.4713 1.497 Aerotech
0.005 432.068
0.054 383.542
0.114 334.083
0.188 353.68
0.316 362.079
0.405 353.68
0.508 348.081
0.637 326.618
0.721 313.553
0.775 311.686
0.903 294.889
0.997 290.223
1.111 300.488
1.199 276.225
1.397 268.76
1.51 274.359
1.594 261.294
1.742 256.628
1.91 248.229
1.999 238.897
2.098 210.902
2.192 157.71
2.305 139.046
2.399 123.181
2.601 105.451
2.695 101.718
2.887 85.854
3.011 78.388
3.1 63.457
3.164 61.591
3.302 50.392
3.411 52.259
3.519 47.593
3.613 37.328
3.82 38.261
3.993 29.862
4.107 29.862
4.205 26.129
4.294 16.797
4.487 0.0

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O2700BL 152.4 1206.5 P 15.149000000000001 33.339 Gorilla
0.037 446.335
0.056 612.765
0.121 627.895
0.26 1210.4
0.261 1331.44
0.501 1739.95
0.734 2322.455
0.994 2594.795
2.006 3147.04
3.008 3646.33
3.519 3805.195
4.318 3888.41
4.494 3850.585
4.995 3691.72
5.478 3578.245
6.193 3162.17
6.249 3245.385
6.314 3101.65
7.001 2345.15
7.456 1777.775
7.864 1210.4
7.994 1051.535
8.208 839.715
8.431 605.2
8.598 506.855
8.821 355.555
9.044 234.515
9.331 143.735
9.443 121.04
9.499 0.0