; ; These engines have had the manufacturers thrust curves massaged until the ; total impulse comes out correct. The total impulse, peak thrust, and ; average thrust are exactly as specified. The duration and thrust curve ; points may have been modified slightly to get the average correct. ; The thrust curves look as much like the graph as possible within the above ; constraints. ; As noted, NAR Standards and Testing Committee data has been applied to some ; motor types to correct the motor parameters. ; ; If you should make additions to this document for redistribution to the user ; community, please observe and follow the format for numerical data and data ; spacing. Please do NOT use tabs to achieve the proper data spacing. ; ; Kent Hoult, July 1990 ; Mark Johnson, July 1990 ; ; Engine manufacturer codes are as follows: ; E Estes ; F Flight Systems Inc ; A-nn Aerotech with nn propellant formula ; ISP-nn Aerotech reload with nn propellant formula ; (WL-white lightning BT-blue thunder BJ-black jack) ; V-TR2 Vulcan / Tracer-II ; P Apogee ; USR US Rockets ; ; Thrust Size (mm) Delays Weight (Kg) ; Type (Sec) (Nt) Dia x Len (sec) Fuel Total Mfg/Notes ;----- ------------ --------- ------- ---------------- --------- ; 1/4A3 modified 7/22 to match NAR published delivered impulse, as tested 1/7/79 1/4A3 13 45 0-2 0.00120 0.00575 E 0.050 0.85 0.100 3.25 0.150 4.75 0.175 5.10 0.240 0.0 ; 1/2A3 modified 7/22 to match NAR published delivered impulse, as tested 1/7/79 1/2A3 13 45 0-2-4 0.00200 0.0066 E 0.056 1.6 0.120 6.4 0.180 3.5 0.250 2.5 0.375 2.0 0.440 0.0 ; A3 modified 7/22 to match NAR published delivered impulse, as tested 1/7/79 A3 13 45 0-2-4-6 0.00330 0.0076 E 0.125 7.9 0.181 3.2 0.250 2.5 0.710 2.15 0.730 0.0 ; A10 modified 7/22 to match NAR published delivered impulse, as tested 1/7/79 A10 13 45 0-3 0.00380 0.0076 E 0.063 5.2 0.125 12.4 0.200 4.4 0.250 1.2 0.375 0.7 0.500 0.6 1.120 0.52 1.130 0.0 ; 1/2A6 modified 7/22 to match NAR published delivered impulse, as tested 1/7/79 1/2A6 18 70 0-2-4 0.0026 0.0150 E 0.050 1.5 0.100 4.0 0.184 8.5 0.220 4.15 0.320 0.0 ; A8 modified 7/22 to match NAR published delivered impulse, as tested 1/7/79 A8 18 70 0-3-5 0.00330 0.0162 E 0.150 8.3 0.180 9.6 0.200 9.7 0.224 9.6 0.229 8.9 0.250 6.2 0.314 3.97 0.335 3.85 0.415 3.75 0.450 0.0 ; B4 modified 7/22 to match NAR published delivered impulse, as tested 1/7/79 B4 18 70 2-4-6 0.006 0.0196 E 0.052 1.5 0.210 10.90 0.300 5.5 0.368 4.0 0.375 3.9 0.912 3.83 1.000 0.0 ; B6 modified 7/22 to match NAR published delivered impulse, as tested 1/7/79 B6 18 70 0-2-4-6 0.0056 0.0178 E 0.026 0.7 0.158 9.0 0.211 10.7 0.263 7.5 0.666 5.2 0.750 0.0 ; B8 modified 7/22 to match NAR published delivered impulse, as tested 4/80 B8 18 70 5 0.0055 0.0178 E 0.053 3.0 0.228 23.6 0.263 8.0 0.421 4.0 0.525 4.0 0.540 0.0 ; B14 modified 8/11 to match NAR published delivered impulse, as tested 1/79 B14 18 70 0-5-7 0.0053 0.0193 E 0.037 7.8 0.075 18.0 0.150 27.2 0.280 3.0 0.330 0.0 ; C5 modified 8/11 to match NAR published delivered impulse, as tested 4/80 C5 18 70 3 0.01130 0.0232 E 0.220 23.4 0.250 10.0 0.330 5.5 0.500 4.5 1.556 4.02 1.580 0.0 ; C6 modified 8/11 to match NAR published delivered impulse,as tested 10/78 C6 18 70 0-3-5-7 0.0108 0.0222 E 0.054 2.0 0.107 8.0 0.155 13.3 0.181 13.3 0.196 10.5 0.214 8.5 0.250 7.5 0.268 6.5 0.339 6.0 0.446 5.65 1.393 5.65 1.450 0.0 D12 24 70 0-3-5-7 0.0211 0.0438 E 0.040 1.0 0.080 3.0 0.120 5.0 0.160 10.0 0.200 15.0 0.240 22.7 0.280 22.7 0.304 15.0 0.357 13.0 0.500 10.5 1.500 9.44 1.550 0.0 ; ; ; Apogee ---- ; Apogee B7 B7 13 44 4-6-8-10 0.00284 0.009 P 0.050 10.0 0.055 9.5 0.080 10.0 0.150 10.5 0.200 13.94 0.500 3.15 0.720 1.0 0.730 0.0 ; Apogee C10 C10 18 51 4-7-10 0.00484 0.0175 P 0.004 25.72 0.055 20.6 0.116 17.8 0.500 8.8 0.712 4.46 0.940 1.12 0.960 0.0 ; ; ;Flight Systems Inc ---- ;A6 modified 8/11 to match NAR published delivered impulse, as tested 9/88 A6 18 70 0-3-5 0.00300 0.0158 F 0.063 4.0 0.114 8.0 0.148 10.0 0.200 11.47 0.229 10.0 0.240 8.0 0.251 4.0 0.262 2.0 0.290 0.0 ;D18 modified 8/11 to match NAR published delivered impulse, as tested 10/78 ;D18 ignores the tailoff thrust of 1.2 nt which lasts 2.0 sec D18 21 95 0-4-6 0.0161 0.0403 F 0.033 5.0 0.133 11.0 0.266 22.0 0.367 30.48 0.433 35.2 0.466 35.2 0.533 30.0 0.583 20.0 0.650 10.0 0.700 5.0 0.750 0.0 ;D20 modified 8/11 to match NAR published delivered impulse, as tested 10/78 ;D20 ignores the tailoff thrust of 1.0 nt which lasts 1.0 sec D20 21 95 0-3-5-7 0.020 0.0444 F 0.036 10.0 0.150 13.0 0.270 21.0 0.360 33.0 0.500 47.15 0.560 31.0 0.580 20.1 0.610 10.0 0.680 7.0 0.720 3.0 0.810 0.0 ;E5 modified 8/11 to match NAR published delivered impulse, as tested 5/87 E5 21 95 0-4-6 0.021 0.0531 F 0.300 9.40 0.667 4.0 0.750 3.5 1.167 3.5 1.583 3.0 5.000 4.37 5.490 0.0 ;E60 modified 8/11 to match NAR published delivered impulse, as tested 10/79 E60 27 100 0-4-6 0.040 0.080 F 0.467 55.0 0.548 59.6 0.596 59.6 0.630 58.0 0.645 53.0 0.758 13.9 0.850 0.0 ;F7 modified 8/11 to match NAR published delivered impulse, as tested 3/80 F7 27 150 0-4-6-8 0.058 0.111 F 0.400 10.0 0.450 10.6 0.500 10.0 0.650 6.0 0.700 6.2 1.000 7.0 1.100 5.75 1.300 4.5 1.500 5.095 9.200 5.0 9.520 0.0 ;F100 modified 8/11 to match NAR published delivered impulse, as tested 7/86 F100 27 150 0-4-6-8-10 0.050 0.108 F 0.147 20.0 0.230 49.85 0.521 94.99 0.669 48.0 0.756 20.0 0.930 0.0 G60 26 134 0-6-8 0.060 0.110 F 0.200 89.0 0.210 70.0 1.500 70.0 1.700 52.0 2.000 0.0 ; ; ;Aerotech disposable and reloads ---- ;RMS B6 - preliminary B6A 18 70 2-4-6 0.0022 0.023 ISP-BT 0.005 8.9 0.100 12.8 0.200 9.2 0.300 8.0 0.400 5.8 0.600 2.7 0.800 0.0 ;Interim Aerotech RMS C4 - added 5/92 msj C4 18 70 3-5 0.0049 0.027 ISP-WL 0.005 9.0 0.200 11.0 1.000 4.5 1.400 1.0 2.000 0.0 ;RMS C6 - preliminary C6A 18 70 3-5 0.0049 0.027 ISP-WL 0.005 8.9 0.1 13.3 0.200 13.3 0.400 11.1 0.600 7.12 0.800 4.8 1.600 0.0 ;Interim Aerotech RMS C12 - added 5/92 msj C12 18 70 4-7-10 0.0044 0.026 ISP-BJ 0.005 22.0 0.200 16.5 0.90 0.0 ;D8 modified 9/16 to match NAR published delivered impulse, as tested 10/85 D8 18 70 2-4-8-12 0.0095 0.0190 A 0.05 13.97 0.051 12.95 0.190 15.0 0.350 15.35 0.510 15.0 0.73 12.5 0.85 10.5 0.90 7.5 1.15 5.5 2.000 4.5 2.42 0.0 ;D13 RMS - preliminary, 6/92 D13 18 70 4-7-10 0.0098 0.033 ISP-WL 0.01 22.25 0.200 22.25 0.400 20.0 0.800 12.5 1.000 8.0 1.400 1.335 1.7 0.0 ;D21 modified 9/16 to match factory thrust curve in old motor instructions D21 18 70 4-7-10 0.0096 0.0236 A-BT 0.06 26.7 0.16 27.81 0.36 28.35 0.50 23.36 0.81 13.35 0.87 2.67 0.90 2.25 0.91 0.0 ;D24 RMS - preliminary, 6/92 D24 18 70 4-7-10 0.0096 0.031 ISP-BT 0.01 41.28 0.1 36.38 0.200 30.15 0.400 25.26 0.600 19.92 0.7 16.8 0.75 2.56 0.9 0.0 ;E25 modified 9/16 to match factory thrust curve as published 6/89 E25 18 70 4-7-10 0.0110 0.0238 A-BT 0.02 31.15 0.04 30.6 0.18 31.71 0.30 30.6 0.50 26.7 0.64 22.25 0.80 11.125 0.86 4.45 0.93 0.0 ;E27 RMS - preliminary E27 18 70 4-7-10 0.0101 0.031 ISP-BT 0.02 41.15 0.04 35.6 0.18 31.71 0.30 30.6 0.50 26.7 0.64 22.25 0.80 11.125 0.86 4.45 0.93 0.0 ;D9 RMS - preliminary D9 24 70 4-7 0.0101 0.045 ISP-WL 0.05 14.0 0.200 15.0 0.400 15.0 0.800 14.0 1.200 8.2 1.800 2.2 2.25 0.0 ;D15 RMS - preliminary D15 24 70 4-7-10 0.0089 0.044 ISP-BT 0.005 26.0 0.1 28.5 0.400 23.0 0.800 11.2 1.000 4.5 1.400 0.0 ;E6 modified 9/16 to match NAR published average motor data, as tested 10/82 E6 24 70 2-4-8 0.0215 0.0397 A 0.04 20.20 0.08 20.20 0.12 20.80 0.16 20.80 0.32 18.36 0.44 18.08 0.48 7.23 0.56 5.54 1.000 4.21 7.0 4.21 7.45 0.0 ;E10 modified 9/22 to match NAR published average motor data as tested 12/84 E10 24 70 0-2-4-8 0.0210 0.0403 A 0.150 17.0 0.225 17.0 0.433 19.0 0.966 19.54 1.600 10.8 2.000 7.5 2.867 6.51 4.06 0.0 ;E11 RMS - preliminary E11 24 70 3-5 0.025 0.061 ISP-BJ 0.005 15.0 0.1 14.5 0.400 14.0 0.800 15.0 2.000 11.0 2.400 8.0 3.1 0.0 ;E15 modified 9/23 to match NAR published average motor data as tested 4/88 E15 24 70 4-7-10 0.0178 0.0452 A-WL 0.035 27.92 0.155 23.5 0.259 21.4 2.00 10.9 2.379 6.36 2.72 0.0 ;E16 - interim reloadable, thrust curve same as E15. Added 9/6/91 E16 29 121 4-7-10 0.0190 0.107 ISP-WL 0.035 27.92 0.155 23.5 0.259 21.4 2.00 10.9 2.379 6.36 2.72 0.0 ;E18 RMS - preliminary E18 24 70 4-7-10 0.0207 0.057 ISP-WL 0.035 31.0 0.40 30.0 0.80 26.7 1.200 19.1 1.600 8.0 2.000 2.2 2.200 0.0 ;E23 RMS - preliminary E23 29 121 4-7-10 0.0174 0.107 ISP-BJ 0.05 33.0 0.200 37.0 0.400 33.0 0.800 27.0 1.200 17.8 1.600 5.8 1.9 0.0 ;E28 RMS - preliminary E28 24 70 4-7-10 0.0184 0.055 ISP-BJ 0.030 52.0 1.012 19.0 1.400 0.0 E30 24 70 4-7-10 0.0192 0.0468 A-BT 0.030 52.0 1.012 21.0 1.333 0.0 ;F12 RMS - preliminary F12 24 70 3-5 0.0303 0.067 ISP-BJ 0.005 20.0 0.1 19.5 0.400 18.0 0.800 19.0 2.000 13.6 2.400 10.6 3.1 0.0 ;F22 RMS - preliminary F22 29 121 5-7 0.0463 0.133 ISP-BJ 0.1 17.8 0.200 26.7 0.400 28.0 0.800 26.5 1.200 25.5 1.600 24.9 2.000 21.3 2.400 16.9 2.800 8.4 3.5 0.0 ;F24 RMS - preliminary F24 24 70 4-7-10 0.019 0.062 ISP-WL 0.005 37.4 0.1 37.8 0.400 37.8 0.800 33.4 1.200 22.2 1.600 6.7 2.200 0.0 ;F39 RMS - preliminary F39 24 70 6-9-12 0.0227 0.059 ISP-BT 0.01 60.0 0.200 56.9 0.400 46.7 0.800 36.9 1.000 26.7 1.1 20.6 1.200 6.7 1.400 0.0 E50 24 70 5-10-15 0.0184 0.0384 A 0.05 47.0 0.40 55.0 0.70 54.0 0.79 44.0 0.80 0.0 F32 24 124 5-10-15 0.0434 0.0768 A-WL 0.096 47.0 1.000 47.0 2.5 0.0 ;Interim F40 RMS motor, using F44 thrust curve F40 29 121 4-7-10 0.040 0.126 ISP-WL 0.01 53.0 0.20 62.0 1.089 55.0 1.7 0.0 F44 24 124 5-10-15 0.0364 0.0735 A-WL 0.01 53.0 0.20 62.0 1.089 55.0 1.7 0.0 ;RMS F52 - preliminary F52 29 121 5-8-11 0.0366 0.123 A-WL 0.01 75.6 0.200 73.2 0.400 69.9 0.800 65.3 1.200 25.3 1.400 4.5 1.58 0.0 F72 24 124 5-10-15 0.0368 0.0731 A 0.02 93.0 0.41 98.0 0.91 57.0 0.998 6.0 1.10 0.0 G42 24 140 4-8-12 0.0488 0.0908 A-WL 0.02 62.0 0.10 67.0 0.60 64.5 0.80 61.4 1.00 56.5 1.20 50.0 1.50 25.5 1.65 9.0 2.1 0.0 G55 24 176 5-10-15 0.0625 0.1037 A-WL 0.048 107.0 0.20 111.0 0.50 85.0 1.509 34.0 2.182 0.0 ;RMS G33 - preliminary G33 29 121 5-7 0.0722 0.159 ISP-BJ 0.01 31.2 0.08 36.9 0.200 36.6 0.400 36.6 0.800 37.5 1.200 39.0 1.600 36.5 2.000 35.3 2.400 29.9 2.800 11.1 3.2 1.33 3.5 0.0 ;Interim G64 RMS motor using G60 thrust curve G64 29 121 4-7-10 0.0625 0.151 ISP-WL 0.20 89.0 0.21 70.0 1.50 70.0 1.70 52.0 2.00 0.0 F10 29 83 2-4-8 0.0407 0.0694 A 0.100 18.0 0.250 29.0 0.750 9.1 7.937 9.2 8.000 0.0 F14 29 83 4-6-9 0.050 0.098 A-BJ 0.012 36.0 0.25 32.0 1.000 22.0 2.000 14.0 4.0 3.0 4.8 0.0 F15 29 83 2-4-8 0.0377 0.0685 A 0.050 16.0 0.200 18.0 0.400 14.5 4.800 15.1 5.209 21.0 5.333 0.0 F20 29 124 4-8-12 0.0361 0.0840 A-WL 0.010 30.0 0.500 43.0 0.900 43.0 1.800 12.0 3.153 12.0 3.500 4.0 4.000 0.0 F25 29 124 6-9-12 0.0356 0.0817 A-WL 0.100 44.0 2.000 21.0 3.071 8.0 3.200 0.0 F60 29 124 6-9-12 0.0379 0.0825 A 0.050 94.0 0.201 98.0 0.999 42.5 1.333 0.0 F80 29 124 5-10-12 0.0381 0.0850 A 0.200 107.0 0.736 107.0 0.947 5.0 1.000 0.0 G25 29 121 5-10-15 0.0541 0.1050 A-WL 0.012 25.0 0.100 31.0 0.200 25.0 0.549 33.0 2.500 34.0 4.800 0.0 G40 29 124 7-10-13 0.0551 0.1180 A-WL 0.100 67.0 2.500 25.0 3.000 0.0 G60 29 124 5-10-15 0.0559 0.1080 A-WL 0.010 70.0 0.650 93.0 0.700 93.0 1.500 46.0 1.750 6.0 2.000 0.0 G80 29 124 7-10-13 0.0569 0.1198 A-BT 0.100 134.0 0.117 134.0 1.000 75.0 1.500 0.0 H55 29 172 6-10-14 0.0829 0.140 A-WL 0.100 69.0 2.261 69.0 3.636 0.0 H120 29 200 6-10-14 0.0855 0.145 A 0.050 110.0 0.505 162.0 1.502 94.0 1.667 0.0 H70 29 197 6-10-14 0.1026 0.172 A-WL 0.100 107.0 1.000 75.0 2.496 61.0 2.857 0.0 H140 29 213 6-10-14 0.1057 0.180 A-BT 0.100 110.0 0.500 194.0 1.004 146.0 1.400 90.0 1.429 0.0 H90 29 265 5-10-15 0.1112 0.200 A-WL 0.100 125.0 0.693 125.0 1.000 95.0 2.500 95.0 3.000 75.0 3.556 0.0 H125 38 191 5-10-15 0.1462 0.225 A-WL 0.050 100.0 0.500 167.0 1.530 129.0 2.000 145.0 2.560 0.0 H45 38 191 5-10-15 0.1662 0.320 A-WL 0.050 89.0 0.500 128.0 0.735 63.0 3.500 50.0 7.111 0.0 H65 38 191 5-10-15 0.1660 0.320 A-WL 0.100 111.0 1.001 80.0 4.015 55.0 4.923 0.0 H100 38 191 5-10-15 0.1774 0.309 A-BT 0.050 89.0 0.500 172.0 1.000 100.0 1.500 100.0 2.000 115.0 3.007 49.0 3.200 0.0 H145 38 191 5-10-15 0.1711 0.312 A-BT 0.050 89.0 0.500 200.0 1.000 180.0 1.995 113.0 2.207 0.0 I95 38 235 5-10-15 0.2163 0.371 A-WL 0.050 89.0 0.900 169.0 1.185 160.0 4.263 0.0 I210 38 235 5-10-15 0.2228 0.377 A-BT 0.050 89.0 1.400 334.0 1.592 334.0 2.000 0.0 I132 38 330 5-10-15 0.3244 0.557 A-WL 0.059 89.0 1.498 227.0 3.000 143.0 4.848 0.0 H35 54 127 10-15 0.1855 0.427 A 0.055 65.0 0.490 85.0 1.000 61.0 9.143 0.0 I32 54 191 10-15 0.3969 0.641 A-WL 0.100 85.0 1.000 68.0 3.007 85.0 4.000 25.0 19.90 20.0 20.00 0.0 I65 54 216 5-10-15 0.3375 0.714 A-WL 0.050 89.0 0.797 156.0 2.000 104.0 9.045 6.0 9.846 0.0 I115 54 216 5-10-15 0.3419 0.677 A-WL 1.000 178.0 1.800 200.0 2.033 200.0 5.565 0.0 I140 54 216 5-10-15 0.3478 0.691 A-BT 0.050 89.0 1.753 254.0 3.000 133.0 4.570 0.0 I220 54 216 5-10-15 0.33519 0.695 A-WL 0.050 89.0 0.684 245.0 2.801 245.0 2.909 0.0 J100 54 257 5-10-15 0.4395 0.827 A-WL 1.000 195.0 2.945 165.0 5.987 118.0 12.80 0.0 J125 54 353 5-10-15 0.6433 1.115 A-WL 1.000 214.0 3.000 200.0 4.015 142.0 7.000 120.0 10.24 0.0 J285 54 257 5-10-15 0.6630 1.095 A-BT 1.000 350.0 2.025 400.0 3.532 340.0 4.491 0.0 J700 54 327 5-10-15 0.6091 1.055 A-BT 0.250 750.0 0.799 868.0 1.702 680.0 1.829 0.0 K125 99 245 0 1.252 2.350 A-WL 1.500 222.0 9.042 164.0 20.48 0.0 K325 99 245 0 1.288 2.390 A-WL 0.050 350.0 0.500 400.0 1.438 300.0 3.800 528.0 7.877 0.0 L1500 54 762 0 1.644 2.300 A 0.200 1800.0 0.500 2381.0 0.510 2372.0 2.000 1072.0 2.411 0.0 L250 99 397 0 2.504 4.300 A-WL 0.100 445.0 5.000 380.0 5.100 375.0 18.00 0.0 L500 99 397 0 2.576 4.400 A 0.102 530.0 0.500 580.0 1.500 482.0 4.000 846.0 9.700 0.0 M500 99 702 0 4.531 7.200 A-WL 0.100 1000.0 1.382 900.0 1.550 900.0 4.000 1424.0 6.000 400.0 16.30 0.0 M1000 99 702 0 4.661 7.300 A 0.100 1200.0 0.750 2559.0 2.000 1900.0 6.000 203.0 6.990 100.0 8.500 0.0 N3050 81 1143 0 5.579 7.400 A 0.100 3000.0 0.500 5340.0 0.749 5225.0 1.000 5108.0 3.785 0.0 ;interim RMS29/180 with simplified thrust curve (H128) H128 29 192 6-10-14 0.0922 0.2145 ISP-WL 0.005 120.0 0.1 130.0 0.3 140.0 0.400 150.0 0.600 155.0 0.800 155.0 1.000 140.0 1.200 120.0 1.25 100.0 1.30 20.0 1.41 0.0 ;interim RMS29/240 with simplified thrust curve (H180) H180 29 240 6-10-14 0.12298 0.26355 ISP-WL 0.005 160.0 0.200 185.0 0.400 210.0 0.7 216.9 1.000 200.0 1.15 180.0 1.25 20.0 1.32 0.0 ;RMS 38/240 with simplified thrust curve (H123) H123 38 150 6-10-14 0.125 0.2933 ISP-WL 0.005 140.0 0.1 145.0 0.200 148.0 0.3 150.0 0.400 152.0 0.5 155.9 0.600 153.0 0.800 150.0 1.000 140.0 1.200 130.0 1.400 108.0 1.600 100.0 1.78 85.0 1.9 20.0 1.98 0.0 ;RMS 38/240 with simplified thrust curve (H242) H242 38 152 6-10-14 0.111 0.279 ISP-BT 0.100 240.0 0.200 295.0 0.900 285.0 1.000 230.0 1.200 0.0 ;RMS 38/360 with simplified thrust curve (I161) I161 38 200 6-10-14 0.1875 0.3848 ISP-WL 0.005 180.0 0.100 190.0 0.200 195.0 0.300 198.0 0.400 200.0 0.500 202.8 0.600 202.0 0.800 198.0 1.000 190.0 1.200 172.0 1.400 160.0 1.600 147.0 1.800 135.0 1.920 115.0 2.000 35.0 2.160 0.0 ;RMS 38/360 with simplified thrust curve (I357) I357 38 199 6-10-14 0.167 0.364 ISP-BT 0.100 240.0 0.200 400.0 0.900 465.0 1.000 400.0 1.200 0.0 ;RMS 38/480 with simple thrust curve (I211) I211 38 250 6-10-14 0.250 0.4773 ISP-WL 0.005 237.0 0.100 242.0 0.200 250.0 0.300 255.0 0.400 260.0 0.500 263.8 0.600 263.0 0.700 260.0 0.800 255.0 0.900 250.0 1.000 245.0 1.200 230.0 1.400 210.0 1.600 190.0 1.800 170.0 1.920 155.0 2.000 35.0 2.130 0.0 ;RMS 38/480 with estimated thrust curve (I154) I154 38 247 6 0.288 0.514 ISP-BJ 0.100 100.0 0.200 160.0 0.300 180.0 0.500 180.0 1.000 180.0 1.500 180.0 2.000 175.0 2.500 150.0 3.000 100.0 3.200 0.0 ;RMS 38/600 with estimated thrust curve (I284) I284 38 300 6-10-14 0.3125 0.5698 ISP-WL 0.005 312.0 0.100 317.0 0.200 327.0 0.300 340.0 0.400 342.0 0.500 341.0 0.600 337.0 0.700 335.0 0.800 329.0 0.900 324.0 1.000 319.0 1.200 299.0 1.400 277.0 1.600 232.0 1.800 227.0 1.920 206.0 2.000 50.0 2.150 0.0 ;RMS 54/852 with estimated thrust curve (J180) J180 54 238 6-10-14 0.420 0.974 ISP-BT 0.100 250.0 0.700 250.0 1.000 225.0 1.500 175.0 2.000 175.0 2.500 150.0 3.000 125.0 3.500 125.0 4.000 125.0 4.500 100.0 5.000 0.0 ;RMS 54/852 with estimated thrust curve (J275) J275 54 240 6-10-14-18 0.4439 0.8829 ISP-WL 0.005 254.0 0.200 276.0 0.400 298.0 0.600 306.0 0.800 320.0 1.000 325.0 1.200 326.34 1.400 326.0 1.600 311.0 1.800 306.0 2.000 298.0 2.200 289.0 2.400 276.0 2.600 262.0 2.700 250.0 2.750 60.0 2.900 0.0 ;RMS 54/852 with estimated thrust curve (J460) J460 54 238 6-10-14 0.393 0.947 ISP-BT 0.100 400.0 0.250 500.0 0.500 500.0 0.750 500.0 1.000 550.0 1.250 550.0 1.500 500.0 1.550 400.0 1.800 0.0 ;RMS 54/1280 with simple thrust curve (J415) J415 54 325 6-10-14-18 0.666 1.1988 ISP-WL 0.005 371.0 0.200 397.0 0.400 428.0 0.600 450.0 0.800 464.0 1.000 472.0 1.200 484.0 1.400 481.0 1.600 473.0 1.800 463.0 2.000 455.0 2.200 437.0 2.400 415.0 2.600 406.0 2.800 383.0 2.900 87.0 2.990 0.0 ;RMS 54/1280 with simple thrust curve (J800) J800 54 322 6-10-14 0.590 1.245 ISP-BT 0.100 700.0 0.250 750.0 0.500 850.0 0.750 950.0 1.000 1000.0 1.250 1000.0 1.500 950.0 1.550 750.0 1.800 0.0 ;RMS 54/1706 with simple thrust curve (K550) K550 54 410 6-10-14-18 0.8876 1.5151 ISP-WL 0.005 516.0 0.200 556.0 0.400 587.0 0.600 622.0 0.800 631.0 1.000 662.0 1.200 670.0 1.400 676.0 1.600 658.0 1.800 636.0 2.000 627.0 2.200 591.0 2.400 578.0 2.600 533.0 2.650 528.0 2.700 90.0 2.810 0.0 ;RMS 54/1706 with simple thrust curve (K1100) K1100 54 406 6-10-14 0.787 1.547 ISP-BT 0.100 750.0 0.250 1250.0 0.500 1250.0 0.750 1300.0 1.000 1300.0 1.250 1225.0 1.500 1000.0 1.750 800.0 1.800 0.0 ;RMS 98/2560 with simple thrust curve (K458) K458 98 290 6-10-14-18 1.3304 3.1062 ISP-WL 0.005 480.0 0.600 535.0 1.200 547.0 1.800 547.0 2.400 523.0 3.000 474.0 3.600 451.0 4.200 433.0 4.800 372.0 5.100 332.0 5.200 76.0 5.400 0.0 ;RMS 98/5120 with simple thrust curve (L952) L952 98 445 6-10-14-18 2.6607 5.0265 ISP-WL 0.005 920.0 0.600 1005.0 1.200 1105.0 1.800 1135.0 2.400 1120.0 3.000 1070.0 3.600 960.0 4.200 810.0 4.800 750.0 4.900 735.0 5.100 110.0 5.240 0.0 ;RMS 98/7680 with simple thrust curve (M1419) M1419 98 600 6-10-14-18 3.9911 6.9307 ISP-WL 0.005 1349.0 0.600 1504.0 1.200 1571.0 1.800 1645.0 2.400 1615.0 3.000 1572.0 3.600 1525.0 4.200 1394.0 4.800 1215.0 5.000 145.0 5.210 0.0 ;RMS 98/10240 with simple thrust curve (M1939) M1939 98 750 6-10-14-18 5.3214 8.8445 ISP-WL 0.005 1884.0 0.600 1989.0 1.200 2122.0 1.800 2189.0 2.400 2167.0 3.000 2078.0 3.600 2033.0 4.200 1766.0 4.800 1655.0 5.000 229.0 5.070 0.0 ; ; ; Vulcan ---- E25 29 77 5-7-10 0.02004 0.072 V-TR2 0.100 17.6 0.400 31.7 0.818 31.7 1.500 19.6 1.600 0.0 F50 29 115 5-7-10-12 0.04007 0.112 V-TR2 0.100 43.1 0.400 61.1 0.926 61.1 1.500 37.2 1.600 0.0 G80 29 147 5-7-10-12 0.0625 0.142 V-TR2 0.100 54.0 0.180 86.8 1.420 86.8 1.500 77.8 1.563 0.0 ; ; ; US Rockets ---- ;US Rockets D6 D6USR 24 70 0-4-8 0.0110 0.0350 USR 0.000 10.0 1.000 10.0 3.000 0.0 ;US Rockets D12 D12USR 24 70 4-8 0.0110 0.0345 USR 0.000 13.0 1.590 12.0 1.600 0.0 ;US Rockets D24 D24USR 24 70 4-8 0.0110 0.0345 USR 0.000 27.0 0.790 23.0 0.800 0.0 ;US Rockets E12 E12USR 24 70 0-4-8 0.0200 0.0420 USR 0.000 21.0 3.400 0.0 ;US Rockets E25 E25USR 24 70 4-8 0.0200 0.0415 USR 0.000 27.0 1.590 23.0 1.600 0.0 ;US Rockets E50 E50USR 24 70 4-8 0.0200 0.0415 USR 0.000 53.0 0.790 46.0 0.800 0.0 ;US Rockets F20 F20USR 29 114 0-4-8-12 0.0420 0.0940 USR 0.000 32.0 0.500 32.0 4.200 0.0 ;US Rockets F25 F25USR 24 140 0-4-8-12 0.0420 0.0760 USR 0.000 38.0 0.500 38.0 3.400 0.0 ;US Rockets F40 firestarter F40FSUSR 29 114 0 0.0450 0.0950 USR 0.000 26.0 2.900 26.0 3.000 0.0 ;US Rockets F40 F40USR 29 114 4-8-12 0.0420 0.0890 USR 0.000 44.0 1.790 44.0 1.800 0.0 ;US Rockets F50 F50USR 24 140 4-8-12 0.0420 0.0760 USR 0.000 53.0 1.590 46.0 1.600 0.0 ;US Rockets F80 F80USR 29 114 4-8-12 0.0450 0.0950 USR 0.000 89.0 0.890 89.0 0.900 0.0 ;US Rockets F100 F100USR 24 140 4-8-12 0.0450 0.0820 USR 0.000 107.0 0.790 93.0 0.800 0.0 ;US Rockets G8 G8USR 29 127 4-8 0.0600 0.0900 USR 0.000 28.0 1.500 6.0 15.000 6.0 15.010 0.0 ;US Rockets G15-U G15-U 29 0 4-8 0.0620 0.1020 USR 0.000 30.0 0.400 37.0 0.800 37.0 1.000 34.0 1.600 18.0 1.720 17.0 2.000 14.0 3.400 13.0 4.200 12.0 6.800 12.0 7.400 4.0 8.200 0.0 ;US Rockets G25-U G25-U 29 0 0 0.0625 0.1050 USR 0.000 28.0 0.300 40.0 0.400 35.0 1.200 37.0 2.000 37.0 2.400 34.0 4.000 7.0 5.000 0.0 ;US Rockets G30 G30USR 29 140 4-8 0.0620 0.1080 USR 0.000 48.0 0.500 48.0 4.200 0.0 ;US Rockets G35 G35USR 24 190 4-8-12 0.0620 0.1060 USR 0.000 57.0 0.500 57.0 3.400 0.0 ;US Rockets G40 G40USR 29 178 4-8 0.0880 0.1350 USR 0.000 64.0 0.500 64.0 4.200 0.0 ;US Rockets G60 firestarter G60FSUSR 29 140 0 0.0620 0.1080 USR 0.000 37.0 2.990 37.0 3.000 0.0 ;US Rockets G60 G60USR 29 140 4-8-12 0.0620 0.1070 USR 0.000 66.0 1.790 66.0 1.800 0.0 ;US Rockets G62 G62USR 29 0 0 0.0567 0.0955 USR 0.000 76.0 0.200 76.0 0.600 89.0 0.900 89.0 1.450 61.0 1.600 6.0 1.750 0.0 ;US Rockets G70 G70USR 24 190 4-8-12 0.0620 0.1060 USR 0.000 80.0 1.590 69.0 1.600 0.0 ;US Rockets G80 G80USR 29 178 4-8-12 0.0880 0.1350 USR 0.000 89.0 1.790 85.0 1.800 0.0 ;US Rockets G120 G120USR 29 140 4-8-12 0.0620 0.1070 USR 0.000 150.0 0.790 150.0 0.800 0.0 ;US Rockets G160 G160USR 29 178 4-8-12 0.0880 0.1350 USR 0.000 182.0 0.890 178.0 0.900 0.0 ;US Rockets G240 G240USR 29 140 8-12 0.0620 0.1100 USR 0.000 258.0 0.490 240.0 0.500 0.0 ;US Rockets G280 G280USR 24 190 0 0.0620 0.1120 USR 0.000 320.0 0.390 278.0 0.400 0.0 ;US Rockets H55 H55USR 38 203 4-8-12 0.1600 0.3000 USR 0.000 80.0 1.000 76.0 7.000 0.0 ;US Rockets H60 H60USR 29 229 4-8-12 0.1240 0.1820 USR 0.000 96.0 0.500 96.0 4.200 0.0 ;US Rockets H80 H80USR 29 0 4-8-12 0.1600 0.2100 USR 0.000 102.0 1.500 120.0 3.000 62.0 3.500 0.0 ;US Rockets H100 H100USR 24 406 8-12 0.1600 0.2120 USR 0.000 129.0 0.500 129.0 3.400 0.0 ;US Rockets H110 firestarter H110FSUS 38 203 0 0.1600 0.3000 USR 0.000 54.0 4.900 54.0 5.000 0.0 ;US Rockets H110 H110USR 38 203 4-8-12 0.1600 0.3000 USR 0.000 110.0 2.890 110.0 2.900 0.0 ;US Rockets H120 H120USR 29 229 4-8-12 0.1200 0.1820 USR 0.000 136.0 1.790 133.0 1.800 0.0 ;US Rockets H160 H160USR 29 0 4-8-12 0.1600 0.2100 USR 0.000 534.0 2.000 890.0 2.010 0.0 ;US Rockets H220 H220USR 38 203 8-12 0.1710 0.3100 USR 0.000 266.0 1.190 266.0 1.200 0.0 ;US Rockets H240 H240USR 29 0 4-8-12 0.1200 0.2300 USR 0.000 222.0 0.020 185.0 0.300 694.0 0.400 694.0 0.500 222.0 0.950 0.0 ;US Rockets H320 H320USR 29 305 4-8-12 0.1700 0.2300 USR 0.000 360.0 0.890 351.0 0.900 0.0 ;US Rockets H440 H440USR 29 0 0 0.2100 0.3450 USR 0.000 222.0 0.600 445.0 1.000 445.0 1.200 89.0 1.500 0.0 ;US Rockets H640 H640USR 29 305 4-8-12 0.1600 0.2300 USR 0.000 640.0 0.490 640.0 0.500 0.0 ;US Rockets I40 I40USR 54 203 4-8 0.3200 0.5120 USR 0.000 196.0 3.500 22.0 14.900 22.0 15.000 0.0 ;US Rockets I65 I65USR 54 203 4-8-12 0.3200 0.5000 USR 0.000 116.0 1.500 116.0 9.000 0.0 ;US Rockets I70 I70USR 38 330 4-8-12 0.3200 0.4780 USR 0.000 151.0 1.000 151.0 7.000 0.0 ;US Rockets I110 I110USR 29 406 4-8-12 0.2400 0.3160 USR 0.000 194.0 0.500 194.0 4.200 0.0 ;US Rockets I130 I130USR 54 0 0 0.3198 0.5679 USR 0.000 142.0 0.200 167.0 3.000 133.0 6.000 0.0 ;US Rockets I140 firestarter I140FSUS 54 203 0 0.3200 0.5120 USR 0.000 109.0 4.900 109.0 5.000 0.0 ;US Rockets I140 I140USR 54 203 4-8-12 0.3200 0.5200 USR 0.000 165.0 4.000 151.0 4.100 0.0 ;US Rockets I150 I150USR 29 508 4-8-12 0.3090 0.4010 USR 0.000 249.0 0.500 249.0 4.000 0.0 ;US Rockets I200 I200USR 38 0 0 0.3198 0.4200 USR 0.000 142.0 1.350 200.0 2.200 284.0 2.500 262.0 2.800 249.0 3.000 42.0 3.200 0.0 ;US Rockets I220 I220USR 38 330 4-8-12 0.3200 0.5050 USR 0.000 221.0 2.890 209.0 2.900 0.0 ;US Rockets I250 I250USR 54 0 8-12 0.3198 0.5679 USR 0.000 178.0 1.350 445.0 1.700 436.0 2.100 58.0 2.450 0.0 ;US Rockets I330 I330USR 29 0 0 0.1650 0.2650 USR 0.000 178.0 0.600 356.0 1.000 356.0 1.200 0.0 ;US Rockets I440 I440USR 38 330 8-12 0.3200 0.5500 USR 0.000 543.0 1.190 525.0 1.200 0.0 ;US Rockets J125-J J125-J 29 0 0 0.6400 1.2800 USR 0.000 187.0 0.100 222.0 0.200 178.0 0.800 178.0 3.000 222.0 4.000 222.0 5.000 205.0 8.000 116.0 10.000 0.0 ;US Rockets J125 J125USR 54 330 4-8-12 0.6400 0.9750 USR 0.000 222.0 1.500 222.0 9.000 0.0 ;US Rockets J160 J160USR 29 610 4-8-12 0.3750 0.4860 USR 0.000 307.0 0.500 307.0 4.000 0.0 ;US Rockets J200 J200USR 54 0 8-12 0.4999 0.7702 USR 0.000 200.0 0.500 311.0 0.700 311.0 1.000 178.0 3.000 178.0 6.500 0.0 ;US Rockets J220 J220USR 38 610 8-12 0.6400 1.1000 USR 0.000 302.0 1.000 302.0 7.000 0.0 ;US Rockets J250 firestarter J250FSUS 54 330 0 0.6400 0.9600 USR 0.000 204.0 4.900 204.0 5.000 0.0 ;US Rockets J250 J250USR 54 330 4-8-12 0.6400 0.9600 USR 0.000 276.0 4.400 267.0 4.500 0.0 ;US Rockets J285 J285USR 54 0 0 0.4999 0.7702 USR 0.000 178.0 3.490 391.0 3.500 0.0 ;US Rockets J360 J360USR 54 0 0 0.5502 0.7752 USR 0.000 203.0 1.350 612.0 1.700 587.0 2.100 58.0 2.250 0.0 ;US Rockets J440 J440USR 38 610 8-12 0.6400 1.1000 USR 0.000 414.0 2.890 414.0 2.900 0.0 ;US Rockets J500 J500USR 54 330 8-12 0.6400 0.9600 USR 0.000 578.0 2.150 556.0 2.200 0.0 ;US Rockets J880 J880USR 38 610 8-12-16 0.6400 1.1000 USR 0.000 1023.0 1.190 1000.0 1.200 0.0 ;US Rockets J1000 J1000USR 54 330 16 0.6400 0.9600 USR 0.000 1134.0 1.080 1068.0 1.100 0.0 ;US Rockets K150 K150USR 95 254 0 1.2247 1.9504 USR 0.000 285.0 2.500 285.0 15.000 0.0 ;US Rockets K250 K250USR 54 610 8-12 1.2800 1.7920 USR 0.000 440.0 2.000 440.0 9.000 0.0 ;US Rockets K300 K300USR 95 254 0 1.2247 1.9504 USR 0.000 368.0 6.890 363.0 6.900 0.0 ;US Rockets K375 K375USR 54 0 0 1.0002 1.3608 USR 0.000 375.0 5.590 375.0 5.600 0.0 ;US Rockets K400 K400USR 54 0 0 0.9498 1.7672 USR 0.000 543.0 0.030 418.0 0.200 494.0 0.600 618.0 0.800 636.0 1.000 601.0 1.180 485.0 3.000 334.0 3.400 302.0 4.000 200.0 4.400 100.0 4.600 40.0 5.000 0.0 ;US Rockets K450 K450USR 54 0 0 0.8999 1.7999 USR 0.000 454.0 0.280 730.0 0.330 730.0 0.370 667.0 0.470 632.0 0.670 614.0 1.210 649.0 1.620 627.0 2.390 458.0 3.600 151.0 4.340 49.0 4.700 0.0 ;US Rockets K500 K500USR 54 610 8-12-16 1.2800 1.7920 USR 0.000 560.0 4.450 547.0 4.500 0.0 ;US Rockets K600 K600USR 95 254 0 1.2247 1.9504 USR 0.000 823.0 3.090 805.0 3.100 0.0 ;US Rockets K675 K675USR 54 0 0 0.8999 1.7999 USR 0.000 645.0 0.850 1254.0 1.000 1294.0 2.000 129.0 3.000 0.0 ;US Rockets K1000 K1000USR 54 610 8-12-16 1.2800 1.7920 USR 0.000 1157.0 2.180 1112.0 2.200 0.0 ;US Rockets K1200 K1200USR 95 254 0 1.2247 1.9504 USR 0.000 1528.0 1.690 1439.0 1.700 0.0 ;US Rockets L225 L225USR 95 0 0 1.9999 2.3002 USR 0.000 1001.0 0.800 1112.0 2.300 1112.0 3.500 667.0 4.500 0.0 ;US Rockets L950 L950USR 54 0 0 1.4252 2.6268 USR 0.000 703.0 0.030 667.0 0.400 836.0 0.800 1001.0 1.000 1085.0 1.400 1170.0 1.600 1183.0 2.000 1201.0 2.200 1201.0 2.400 1134.0 2.500 667.0 2.600 503.0 3.000 0.0 ;US Rockets M600 M600USR 95 813 0 4.8988 7.3482 USR 0.000 1139.0 2.500 1139.0 15.000 0.0 ;US Rockets M1200 M1200USR 95 813 0 4.8988 7.3482 USR 0.000 1471.0 6.890 1450.0 6.900 0.0 ;US Rockets M2400 M2400USR 95 813 0 4.8988 7.3482 USR 0.000 3292.0 3.090 3221.0 3.100 0.0 ;US Rockets M4800 M4800USR 95 813 0 4.8988 7.3482 USR 0.000 6112.0 1.690 5756.0 1.700 0.0 ;US Rockets N1200 N1200USR 95 1524 0 9.7976 12.7459 USR 0.000 2306.0 2.500 2306.0 15.000 0.0 ;US Rockets N2400 N2400USR 95 1524 0 9.7976 12.7459 USR 0.000 2945.0 6.890 2900.0 6.900 0.0 ;US Rockets N4800 N4800USR 95 1524 0 9.7976 12.7459 USR 0.000 6583.0 3.090 6441.0 3.100 0.0 ;US Rockets N9600 N9600USR 95 1524 0 9.7976 12.7459 USR 0.000 12224.0 1.690 11512.0 1.700 0.0 ; ;---- ;no engine - used for boosted darts NONE 0 0 0 0.0 0.0 n/a 0.000 0.0 0