// From Internet RASP engines.dat Aerotech/C G42-4,8,12 89.6225 2.10 0.0919 0.0488 // masses from manuf data // From TMT results (masses from manuf data Aerotech/C F55-4,8,12 48.31 0.85 0.0457 0.0240 Aerotech/C G125-5,10,15 117.19 1.02 0.1050 0.0571 // from NAR results Aerotech/C D21-4 18.67 0.96 0.0233 0.0096 // 11/88 Aerotech/C D21-7 18.67 0.96 0.0237 0.0096 Aerotech/C D21-10 18.67 0.96 0.0237 0.0096 Aerotech/C E25-4 20.56 0.99 0.0243 0.0110 // 11/88 Aerotech/C E25-7 20.56 0.99 0.0243 0.0110 Aerotech/C E25-10 20.56 0.99 0.0245 0.0110 Aerotech/C E6-0 37.55 7.45 0.0397 0.0215 // 10/82 Aerotech/C E6-2 37.55 7.45 0.0397 0.0215 Aerotech/C E6-4 37.55 7.45 0.0397 0.0215 Aerotech/C E6-8 37.55 7.45 0.0415 0.0215 Aerotech/C E6-P 37.55 7.45 0.0397 0.0215 Aerotech/C E15-4 38.38 2.72 0.0449 0.0178 // 4/88 Aerotech/C E15-7 38.38 2.72 0.0452 0.0178 Aerotech/C E15-10 38.38 2.72 0.0468 0.0178 Aerotech/C E30-4 39.13 1.25 0.0461 0.0192 // 4/88 Aerotech/C E30-7 39.13 1.25 0.0459 0.0192 Aerotech/C E30-10 39.13 1.25 0.0458 0.0192 Aerotech/C E45-4 38.45 0.77 0.0364 0.0192 // 10/89 Aerotech/C E45-8 38.45 0.77 0.0368 0.0192 Aerotech/C E45-12 38.45 0.77 0.0366 0.0192 Aerotech/C F14-4 63.13 3.92 0.0975 0.0500 // 7/90 manuf prop mass Aerotech/C F14-6 63.13 3.92 0.0973 0.0500 Aerotech/C F14-9 63.13 3.92 0.0977 0.0500 Aerotech/C F14-P 63.13 3.92 0.0972 0.0500 Aerotech/C F44-0 79.8 1.8 0.0634 0.0377 // 11/83 Aerotech/C F44-5 79.8 1.8 0.0638 0.0377 Aerotech/C F44-10 79.8 1.8 0.0638 0.0377 Aerotech/C F44-15 79.8 1.8 0.0638 0.0377 Aerotech/C F44-20 79.8 1.8 0.0638 0.0377 Aerotech/C F10-0 74.64 7.34 0.0702 0.0407 // 1/83 Aerotech/C F10-2 74.64 7.34 0.0702 0.0407 Aerotech/C F10-4 74.64 7.34 0.0707 0.0407 Aerotech/C F10-8 74.64 7.34 0.0728 0.0407 Aerotech/C F72-5 76.51 1.08 0.0736 0.0368 // 3/89 Aerotech/C F72-10 76.51 1.08 0.0734 0.0368 Aerotech/C F72-15 76.51 1.08 0.0735 0.0368 Aerotech/C F32-5 75.82 2.94 0.0740 0.0377 // 11/88 Aerotech/C F32-10 75.82 2.94 0.0744 0.0377 Aerotech/C F32-15 75.82 2.94 0.0742 0.0377 Aerotech/C F25-6 79.57 3.40 0.0910 0.0356 // 6/88 Aerotech/C F25-9 79.57 3.40 0.0909 0.0356 Aerotech/C F25-12 79.57 3.40 0.0903 0.0356 Aerotech/C F50-6 78.05 1.62 0.0821 0.0379 // 2/88 Aerotech/C F50-9 78.05 1.62 0.0824 0.0379 // listed as F60 due Aerotech/C F50-12 78.05 1.62 0.0821 0.0379 // to typo in NAR data Aerotech/C G25-0 119.05 4.86 0.1032 0.0625 // 1/87 Aerotech/C G25-5 119.05 4.86 0.1032 0.0625 Aerotech/C G25-10 119.05 4.86 0.1035 0.0625 Aerotech/C G25-15 119.05 4.86 0.1037 0.0625 Aerotech/C G40-7 114.10 3.03 0.1070 0.0551 // 2/88 Aerotech/C G40-10 114.10 3.03 0.1066 0.0551 Aerotech/C G40-13 114.10 3.03 0.1072 0.0551 Aerotech/C G80-7 115.99 1.42 0.1048 0.0569 // 2/88 Aerotech/C G80-10 115.99 1.42 0.1059 0.0569 Aerotech/C G80-13 115.99 1.42 0.1059 0.0569 Aerotech/C G55-5 121.79 2.59 0.1037 0.0625 // 3/89 Aerotech/C G55-10 121.79 2.59 0.1043 0.0625 Aerotech/C G55-15 121.79 2.59 0.1040 0.0625 // From Internet RASP engines.dat Aerotech/B H35 320.004000 9.143 0.427 0.185500 Aerotech/B K125 2560.022000 20.48 2.350 1.252000 // From manufacturer data Aerotech/B J220 1280.0 5.8 1.075 0.7103 Aerotech/B J355 1280.0 3.6 1.030 0.6783 Aerotech/B K250 2560.0 10.2 2.080 1.533 Aerotech/B K400 2560.0 6.4 1.937 1.390 Aerotech/B K900 1800.0 2.0 1.397 0.9274 Aerotech/B K1500 1500.0 1.0 1.258 0.7917 // From Internet RASP engines.dat (masses from manuf data) Aerotech/B H45 319.990000 7.111 0.340 0.1861 Aerotech/B H100 320.002500 3.20 0.336 0.1816 Aerotech/B H125 320.005000 2.56 0.325 0.1677 Aerotech/B H140 200.013000 1.429 0.207 0.1061 Aerotech/B I210 420.014000 2.00 0.377 0.2228 Aerotech/B J100 1280.010000 12.80 0.781 0.4901 // From old (4/91) TMT results (masses from manuf data) Aerotech/B I115-5,10 684.5 8.00 0.638 0.3822 Aerotech/B J125-10 1233.0 11.00 1.099 0.7345 // From TMT results (masses from manuf data) Aerotech/B H35-6,10,14 163.98 3.43 0.204 0.1050 Aerotech/B H55-10 157.02 2.10 0.182 0.0928 Aerotech/B H65-10,15 308.855 4.304 0.336 0.1816 Aerotech/B H70-10,14 192.94 2.07 0.221 0.1110 Aerotech/B H90-12 250.02 1.91 0.269 0.1444 Aerotech/B H120-10 156.69 1.29 0.175 0.0855 Aerotech/B H145-10 317.410 2.128 0.301 0.1711 Aerotech/B I65-10,15 636.107 9.223 0.625 0.3697 Aerotech/B I95-10,15 419.344 4.172 0.397 0.2423 Aerotech/B I132-10,15 610.245 4.245 0.596 0.3633 Aerotech/B I140-10,15 579.228 5.121 0.583 0.3272 Aerotech/B I220-5,15 605.204 3.217 0.586 0.3303 Aerotech/B J285-10,15 1149.355 5.015 1.014 0.6499 Aerotech/B J455-10,15 1124.570 2.989 0.961 0.5965 Aerotech/B J700-15,20 1285.683 1.851 0.952 0.6002 // From TMT results (masses from Internet RASP engines.dat // From Internet RASP engines.dat (masses from manuf data Aerotech/RMS/C B6 4.823000 0.80 0.023 0.0022 Aerotech/RMS/C C4 9.572500 2.00 0.027 0.0049 Aerotech/RMS/C C6 9.780750 1.60 0.027 0.0049 Aerotech/RMS/C C12 9.583750 0.90 0.026 0.0044 Aerotech/RMS/C D9 19.380000 2.25 0.045 0.0101 Aerotech/RMS/C D15 19.688750 1.40 0.044 0.0089 Aerotech/RMS/C E11 33.713750 3.10 0.061 0.0250 Aerotech/RMS/C E16 38.380900 2.72 0.107 0.0190 Aerotech/RMS/C E18 39.855000 2.20 0.057 0.0207 Aerotech/RMS/C E23 39.625000 1.90 0.104 0.0174 Aerotech/RMS/C E27 22.078800 0.93 0.031 0.0101 Aerotech/RMS/C E28 39.327000 1.40 0.055 0.0184 Aerotech/RMS/C F12 43.061250 3.10 0.067 0.0303 Aerotech/RMS/C F22 64.845000 3.50 0.133 0.0463 Aerotech/RMS/C F24 48.155500 2.20 0.062 0.0190 Aerotech/RMS/C F39 49.245500 1.40 0.059 0.0227 Aerotech/RMS/C F40 79.999000 1.70 0.126 0.0400 Aerotech/RMS/C F52 77.369000 1.58 0.123 0.0366 Aerotech/RMS/C G33 97.775000 3.50 0.159 0.0722 Aerotech/RMS/C G64 119.995000 2.00 0.151 0.0625 // From TMT results (masses from manuf data) Aerotech/RMS/C D13-7 19.62 1.35 0.0330 0.0098 Aerotech/RMS/C D24-10 18.73 0.83 0.0310 0.0087 Aerotech/RMS/C F37-S,M,L 51.55 1.54 0.1122 0.0282 Aerotech/RMS/C F62-S,M,L 51.00 0.93 0.1090 0.0250 Aerotech/RMS/C G54-S,M,L 78.05 1.44 0.1408 0.0460 Aerotech/RMS/C G75-S,M 161.43 2.07 0.2279 0.1056 Aerotech/RMS/C G104-S,M,L 82.86 0.87 0.1356 0.0408 // From Internet RASP engines.dat (masses from manufacturer data) Aerotech/RMS/B K1100 1982.500000 1.80 1.3680 0.7333 Aerotech/RMS/B K458 2495.002500 5.43 3.1062 1.3300 Aerotech/RMS/B M1419 7412.265000 5.21 6.9307 3.9900 Aerotech/RMS/B M1939 9859.542500 5.07 8.8445 5.3200 // From TMT results (masses from manufacturer data) Aerotech/RMS/B H73-S,M 180.06 3.48 0.3083 0.1400 Aerotech/RMS/B H97-S,M 185.26 2.25 0.2815 0.1409 Aerotech/RMS/B H123-S,M,L 211.4 2.43 0.2933 0.1250 Aerotech/RMS/B H128-S,M,L 155.79 1.32 0.2145 0.0922 Aerotech/RMS/B H180-S,M,L 212.04 1.22 0.2636 0.1230 Aerotech/RMS/B H238-S,M,L 163.20 0.73 0.2021 0.0798 Aerotech/RMS/B H242-S,M,L 234.22 1.12 0.2791 0.1108 Aerotech/RMS/B I112-S,M 294.37 3.12 0.4073 0.2100 Aerotech/RMS/B I154-S,M 385.33 3.32 0.5063 0.2800 Aerotech/RMS/B I161-S,M,L 333.51 2.03 0.3848 0.1875 Aerotech/RMS/B I211-S,M,L 440.46 1.95 0.4763 0.2500 Aerotech/RMS/B I284-S,M,L 554.23 1.73 0.5678 0.3125 Aerotech/RMS/B I357-S,M,L 341.01 1.01 0.3635 0.1662 Aerotech/RMS/B J180-S,L 778.96 3.40 0.8409 0.3982 // odd result Aerotech/RMS/B J180-S,M 825.77 4.00 0.8409 0.3982 Aerotech/RMS/B J275-S,M,L 818.688 3.328 0.8829 0.4402 Aerotech/RMS/B J415-M,L 1201.32 3.10 1.1989 0.6603 Aerotech/RMS/B J460-L,X 812.67 1.85 0.8329 0.3902 Aerotech/RMS/B J800-L,X 1264.79 1.638 1.105 0.617 // TMT masses Aerotech/RMS/B K550-M,L 1594.46 2.96 1.5151 0.8804 Aerotech/RMS/B L952-X 5097.808 6.244 5.0265 2.6600 // obsolete Aerotech engines // From Internet RASP engines.dat // Aerotech/C G60 120.010000 2.000000 0.108000 0.055900 // Aerotech/B I32* 640.000500 20.000000 0.641000 0.396900 // Aerotech/B K325* 2559.996000 7.877000 2.390000 1.288000 // Aerotech/B L250 4500.000000 18.000000 4.300000 2.504000 // Aerotech/B L500 4850.020000 9.700000 4.400000 2.576000 // Aerotech/B L1500 3616.991000 2.411000 2.300000 1.644000 // Aerotech/B M500 8150.000000 16.300000 7.200000 4.531000 // Aerotech/B M1000* 8500.035000 8.500000 7.300000 4.661000 // Aerotech/B N3050* 11543.024000 3.785000 7.400000 5.579000 // from NAR results Aerotech/C D7-0 19.93 3.12 0.0256 0.0110 // 3/83 Aerotech/C D7-2 19.93 3.12 0.0258 0.0110 Aerotech/C D7-4 19.93 3.12 0.0266 0.0110 Aerotech/C D7-8 19.93 3.12 0.0278 0.0110 Aerotech/C D8-0 18.84 2.42 0.0185 0.0095 // 10/85 Aerotech/C D8-2 18.84 2.42 0.0186 0.0095 Aerotech/C D8-4 18.84 2.42 0.0188 0.0095 Aerotech/C D8-8 18.84 2.42 0.0197 0.0095 Aerotech/C D8-12 18.84 2.42 0.0207 0.0095 Aerotech/C E10-0 39.80 4.06 0.0396 0.0210 // 12/84 Aerotech/C E10-2 39.80 4.06 0.0400 0.0210 Aerotech/C E10-4 39.80 4.06 0.0403 0.0210 Aerotech/C E10-8 39.80 4.06 0.0414 0.0210 Aerotech/C E28-0 39.14 1.40 0.0391 0.0189 // 8/84 Aerotech/C E28-4 39.14 1.40 0.0395 0.0189 Aerotech/C E28-8 39.14 1.40 0.0395 0.0189 Aerotech/C E28-12 39.14 1.40 0.0397 0.0189 Aerotech/C E50-0 37.35 0.76 0.0385 0.0189 // 4/85 Aerotech/C E50-5 37.35 0.76 0.0388 0.0189 Aerotech/C E50-10 37.35 0.76 0.0388 0.0189 Aerotech/C E50-15 37.35 0.76 0.0389 0.0189 Aerotech/C F9-0 49.76 5.05 0.0427 0.0245 // 6/85 Aerotech/C F9-2 49.76 5.05 0.0424 0.0245 Aerotech/C F9-4 49.76 5.05 0.0426 0.0245 Aerotech/C F9-8 49.76 5.05 0.0426 0.0245 Aerotech/C F30-0 56.87 2.0 0.0601 0.0283 // 8/84 Aerotech/C F30-4 56.87 2.0 0.0604 0.0283 Aerotech/C F30-7 56.87 2.0 0.0606 0.0283 Aerotech/C F30-10 56.87 2.0 0.0602 0.0283 Aerotech/C F15-0 75.96 5.33 0.0624 0.0377 // 5/83 Aerotech/C F15-2 75.96 5.33 0.0628 0.0377 Aerotech/C F15-4 75.96 5.33 0.0629 0.0377 Aerotech/C F15-8 75.96 5.33 0.0642 0.0377 Aerotech/C F20-0 74.88 4.07 0.0657 0.0377 // 12/84 Aerotech/C F20-4 74.88 4.07 0.0658 0.0377 Aerotech/C F20-8 74.88 4.07 0.0680 0.0377 Aerotech/C F20-12 74.88 4.07 0.0705 0.0377 Aerotech/C F80-0 75.34 0.97 0.0691 0.0377 // 1/85 Aerotech/C F80-5 75.34 0.97 0.0701 0.0377 Aerotech/C F80-10 75.34 0.97 0.0698 0.0377 Aerotech/C F80-15 75.34 0.97 0.0699 0.0377 Aerotech/C F80-20 75.34 0.97 0.0700 0.0377 Aerotech/C F41-0 79.57 1.8 0.0733 0.0377 // 8/84 Aerotech/C F41-6 79.57 1.8 0.0740 0.0377 Aerotech/C F41-9 79.57 1.8 0.0733 0.0377 Aerotech/C F41-14 79.57 1.8 0.0740 0.0377 // from NAR certification data Apogee 1/4A3-2T 0.55 0.19 0.0061 0.0012 // 3/91 Apogee 1/4A3-4T 0.55 0.19 0.0057 0.0012 Apogee A3-2T 2.02 0.69 0.0081 0.0033 // 3/91 Apogee A3-6T 2.02 0.69 0.0085 0.0033 Apogee B7-4 4.90 0.73 0.0087 0.0024 // 7/90 prop mass from AT data Apogee B7-6 4.90 0.73 0.0088 0.0024 Apogee B7-8 4.90 0.73 0.0089 0.0024 Apogee B7-10 4.90 0.73 0.0089 0.0024 Apogee C4-3 8.92 2.35 0.0172 0.0045 // 8/93 est initial mass Apogee C4-5 8.92 2.35 0.0173 0.0045 Apogee C4-7 8.92 2.35 0.0174 0.0045 Apogee C10-4 9.56 0.96 0.0175 0.00484 // 2/91 prop mass from AT data Apogee C10-7 9.56 0.96 0.0176 0.00484 Apogee C10-10 9.56 0.96 0.0177 0.00484 Apogee D3-3 18.36 6.39 0.0188 0.0098 // 8/93 est initial mass Apogee D3-5 18.36 6.39 0.0188 0.0098 Apogee D3-7 18.36 6.39 0.0188 0.0098 // from NAR test results Estes 1/4A3-2T 0.61 0.24 0.0054 0.0012 // 1/79 Estes 1/4A3-4T 0.61 0.24 0.0061 0.0012 // 1/79 Estes 1/2A3-2T 1.15 0.44 0.0064 0.0020 // 1/79 Estes 1/2A3-4T 1.15 0.44 0.0068 0.0020 // 1/79 Estes A3-2T 2.09 0.73 0.0075 0.0033 // 1/79 Estes A3-4T 2.09 0.73 0.0076 0.0033 // 1/79 Estes A3-6T 2.09 0.73 0.0079 0.0033 // 1/79 Estes A10-0T 2.03 1.13 0.0072 0.0038 // 1/79 Estes A10-3T 2.03 1.13 0.0079 0.0038 // 1/79 Estes 1/2A6-0 1.14 0.32 0.0134 0.0026 // 1/79 Estes 1/2A6-2 1.14 0.32 0.0147 0.0026 // 1/79 Estes 1/2A6-4 1.14 0.32 0.0160 0.0026 // 1/79 Estes A8-0 2.30 0.45 0.0134 0.0033 // 1/79 Estes A8-3 2.30 0.45 0.0158 0.0033 // 1/79 Estes A8-5 2.30 0.45 0.0172 0.0033 // 1/79 Estes B4-2 4.35 1.00 0.0188 0.0060 // 1/79 Estes B4-4 4.35 1.00 0.0196 0.0060 // 1/79 Estes B4-6 4.35 1.00 0.0199 0.0060 // 1/79 Estes B6-0 4.42 0.75 0.0154 0.0056 // 1/79 Estes B6-2 4.42 0.75 0.0176 0.0056 // 1/79 Estes B6-4 4.42 0.75 0.0178 0.0056 // 1/79 Estes B6-6 4.42 0.75 0.0185 0.0056 // 1/79 Estes B8-0 4.35 0.54 0.0150 0.0055 // 4/80 Estes B8-5 4.35 0.54 0.0175 0.0055 // 4/80 Estes B8-7 4.35 0.54 0.0181 0.0055 // 4/80 Estes C6-0 8.52 1.45 0.0201 0.0108 // 10/78 Estes C6-3 8.52 1.45 0.0223 0.0108 // 10/78 Estes C6-5 8.52 1.45 0.0222 0.0108 // 10/78 Estes C6-7 8.52 1.45 0.0231 0.0108 // 10/78 Estes C5-3 9.03 1.58 0.0232 0.0113 // 4/80 Estes D11-9 12.63 1.27 0.0424 0.0175 // 10/79 Estes D11-P 17.49 1.86 0.0448 0.0245 // 4/92 Estes E15-4 29.50 2.63 0.0425 0.0355 // 6/93 prop mass from Estes data Estes E15-6 29.50 2.63 0.0573 0.0355 // 6/93 masses from Estes data Estes E15-8 29.50 2.63 0.0440 0.0355 // 6/93 prop mass from Estes data Estes E15-P 29.50 2.63 0.0449 0.0372 // 6/93 prop mass from Estes data Estes D12-0 15.80 1.55 0.0371 0.0211 // 10/78 Estes D12-3 15.80 1.55 0.0429 0.0211 // 10/78 Estes D12-5 15.80 1.55 0.0438 0.0211 // 10/78 Estes D12-7 15.80 1.55 0.0443 0.0211 // 10/78 Estes B14-0 4.37 0.23 0.0158 0.0053 // 1/79 Estes B14-5 4.37 0.23 0.0209 0.0053 // 1/79 Estes B14-7 4.37 0.23 0.0199 0.0053 // 1/79 // from NAR test results FSI A6-3 1.83 0.29 0.0154 0.0030 // 9/88 FSI A6-5 1.83 0.29 0.0160 0.0030 // 9/88 FSI B6-0 4.35 0.56 0.0163 0.0060 // 9/88 FSI B6-3 4.35 0.56 0.0180 0.0060 // 9/88 FSI B6-5 4.35 0.56 0.0188 0.0060 // 9/88 FSI C6-0 8.55 1.40 0.0220 0.0120 // 9/88 FSI C6-3 8.55 1.40 0.0235 0.0120 // 9/88 FSI C6-5 8.55 1.40 0.0251 0.0120 // 9/88 FSI D18-0 14.00 0.75 0.0371 0.0161 // 10/78 see test report-- FSI D18-4 14.00 0.75 0.0371 0.0161 // 10/78 tail thrust not in tt FSI D18-6 14.00 0.75 0.0371 0.0161 // 10/78 making delays around 8 sec FSI D20-0 15.29 0.81 0.0416 0.0200 // 1/83 see test report-- FSI D20-3 15.29 0.81 0.0434 0.0200 // 1/83 tail thrust not in tt FSI D20-5 15.29 0.81 0.0444 0.0200 // 1/83 FSI D20-7 15.29 0.81 0.0449 0.0200 // 1/83 FSI E5-0 20.65 4.48 0.0478 0.0210 // 5/87 FSI E5-4 20.65 5.49 0.0531 0.0210 // 5/87 FSI E5-6 20.65 5.49 0.0537 0.0210 // 5/87 FSI E60-0 27.60 0.85 0.0801 0.0400 // 10/79 FSI E60-4 27.60 0.85 0.0793 0.0400 // 10/79 FSI E60-6 27.60 0.85 0.0801 0.0400 // 10/79 FSI E60-8 27.60 0.85 0.0805 0.0400 // 10/79 FSI F7-4 48.80 9.52 0.1113 0.0580 // 3/80 FSI F7-6 48.80 9.52 0.1110 0.0580 // 3/80 FSI F100-0 40.72 0.93 0.1046 0.0500 // 7/86 FSI F100-4 40.72 0.93 0.1051 0.0500 // 7/86 FSI F100-6 40.72 0.93 0.1073 0.0500 // 7/86 FSI F100-8 40.72 0.93 0.1089 0.0500 // 7/86 FSI F100-10 40.72 0.93 0.1058 0.0500 // 7/86 // FSI G60 119.995000 2.000000 0.110000 0.060000 // from NAR test results //MRC FX 0.00 7.00 ?????? 0.0007 // 11/89 MRC A8-3 2.30 0.42 0.0154 0.0030 // 1/87 MRC B4-2 4.73 1.19 0.0188 0.0060 // 1/87 MRC B4-4 4.73 1.19 0.0189 0.0060 // 1/87 MRC B6-4 3.60 0.81 0.0181 0.0060 // 1/87 MRC C6-3 8.25 1.89 0.0232 0.0120 // 1/87 MRC C6-5 8.25 1.89 0.0235 0.0120 // 1/87 // from NAR test results Quest A6-4 2.12 0.41 0.0153 0.0035 // 11/91 Quest B6-0 4.63 0.75 0.0148 0.0065 // 11/91 Quest B6-4 4.63 0.75 0.0178 0.0065 // 11/91 Quest C6-3 8.10 1.71 0.0218 0.0110 // 2/92 Quest C6-5 8.10 1.71 0.0229 0.0110 // 2/92 // from NAR test results //SMI B4-2 4.90 1.18 0.0174 ?????? // 2/91 //SMI B4-4 4.90 1.18 0.0181 ?????? // 2/91 //SMI B4-6 4.90 1.18 0.0189 ?????? // 2/91 // From TMT listing (estimated masses) Energon L1100-18 5196.2 5.01 3 2 // From TMT listing (masses from manuf data) Rocketflite F50-0,9 58.38 0.60 .180 .0625 Rocketflite F50-0,9SS 56.38 0.55 .180 .0625 Rocketflite G160-0,5,7SS 185.75 0.80 .400 .180 Rocketflite H220-0,9 251.61 0.93 .506 .240 Rocketflite H220-0,9SS 264.66 0.80 .506 .240 // From Internet RASP engines.dat Vulcan E25 39.998900 1.600000 0.072000 0.020040 Vulcan F50 79.995700 1.600000 0.112000 0.040070 Vulcan G80 124.998700 1.563000 0.142000 0.062500 // From NAR test results Vulcan E26-5 39.54 1.41 0.0582 0.0192 // 7/86 Vulcan E26-7 39.54 1.41 0.0594 0.0192 // 7/86 Vulcan E26-10 39.54 1.41 0.0600 0.0192 // 7/86 Vulcan G50-7 125.87 2.57 0.1367 0.0617 // 4/88 Vulcan G50-10 125.87 2.57 0.1383 0.0617 // 4/88 Vulcan G50-13 125.87 2.57 0.1408 0.0617 // 4/88 // From TMT listing (estimated masses) // Vulcan F50-7 Vulcan G200-7,10 130.810 0.729 0.142 0.0625 // Vulcan G210-5,10,12 Vulcan H80-7,10 247.65 3.48 0.3 0.1238 Vulcan H100-10,12 222.33 2.21 0.3 0.1112 Vulcan H115-10,15 271.40 2.22 0.3 0.1351 Vulcan H142-10,15 295.85 2.26 0.3 0.1479 Vulcan H260-5,10 290.71 1.21 0.3 0.1454 Vulcan H300-7,12 314.09 0.91 0.3 0.1570 Vulcan I160-5,10 519.92 3.51 0.5 0.2599 // Vulcan I230-10 Vulcan I250-10,15 526.48 2.28 0.5 0.2632 Vulcan I283-7,10 582.99 2.24 0.5 0.2915 Vulcan I500-7,10 563.04 1.76 0.5 0.2816 Vulcan J250-15 986.21 4.66 1.0 0.4931 Vulcan J340-7 810.91 3.10 1.0 0.4055 Vulcan K500-10,15 2042.19 4.21 1.8 1.0211 Vulcan L750-35 2281.65 5.81 3.0 1.1408 Vulcan L750-20 3098 5.2 3.0 1.5049