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Must Be a Real Engine Which Does Not Fire on Launchpad During Nominal Launch Sequence. No Launch System Engi

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Must Be a Real Engine Which Does Not Fire on Launchpad During Nominal Launch Sequence. No Launch System Engi Inclusion criteria: must be a real engine which does not fire on launchpad during nominal launch sequence. No ion engines, manuvering thrusters or ullage motors - must be able to circularise a suborbital trajectory (in principle). Must be a real engine which flew at least once (flight is allowed to be a failure). Isp and Mass must be known. Launch system Engine Nationality Isp Thrust/kN Mass/kg Kosmos-3M 11D49 Russia 303 157.5 185 Buran 17D11 Russia 362 86.3 230 Buran 17D12 Russia 362 86.3 230 Delta AJ10-118F USA 306 41.4 95 AJ10-138 USA 311 35.6 110 Delta K AJ10-118K USA 321 43.4 98 AJ10-118D USA 278 33.7 90 AJ10-118 USA 271 33.8 90 One AJ-10 variantAJ10-104 was used inUSA Apollo service module 278 35.1 90 AJ10-118E USA 278 90 Astris Germany 310 23.3 68 ATE USA 347 20 58 Bell 8048 USA 276 68.9 127 Bell 8081 USA 285 71.2 130 Bell 8096 USA 293 71.2 132 Black Arrow-3UK 278 29.4 87 Castor 4B USA 281 430 1400 Castor 4BXL USA 267 429 1513 DFH-2 AKM China 288 43.46 70 EPKM China 292 190 541 FSW RetromotorChina 280 40.66 53 FW-4D USA 287 25 25 FW-4S TEM640USA 280 27.4 25 Gamma 2 UK 265 68.2 173 GCRC USA 230 11.6 31 GF-02 China 254 181 246 HM-10 France 443 61.8 145 HM7-A France 443 61.7 149 HM7-B France 447 70 155 Iris Italy 291 29.4 256 Saturn V J-2 USA 420 1033 1788.1 J-2S USA 436 1138 1400 Kestrel SpaceX 317 30.7 52 KRD-61 Russia 313 18.8 42 Soyuz TM, ProgressKTDU-425A Russia 315 18.9 70 KTDU-80 Russia 326 6.19 310 KTDU-417 Russia 314 18.92 81 Ariane 5 KTDU-5A Russia 287 45.5 48 L7 Germany 320 27.4 110 H-2 LE-5 Japan 450 103 245 LE-5A Japan 452 121.5 242 LE-5B Japan 447 137 269 LR91-11 USA 316 467 589 LR-91-3 USA 308 355.9 590 LR-91-5 USA 315 444.8 500 M-23-Mu Japan 285 542 2800 M-3B-Mu Japan 294 132.1 490 M-3B-J Japan 294 132.1 300 M-V-4 Japan 298 52 118 M24 Japan 288 1245.3 3410 M34 Japan 301 294 1000 M56A-1 Japan 297 228.5 466 Mage 1 France 295 14.9 34 Mage 2 France 293 45.5 40 MB-35 Japan 467 156 345 MB-60 Japan 467 266.7 591 MIHT-2 Russia 280 490.3 1500 MIHT-3 Russia 280 245.2 1000 MIHT-4 Russia 295 9.8 300 Nihka Canada 285 50.5 70 P4 France 273 176.5 1000 P6 France 211 29.4 120 Pegasus-3 USA 287 34.6 104 Pegasus XL-2USA 290 153.5 416 Pegasus-2 USA 290 118.2 345 Perigee Orbit ChinaTransfer Motor 280 222.84 496 Proton (Stage 3) PSLV-3 India 291 328.7 1100 Proton (Stage 2) RD-0213 Russia 328.6 19.62 95 RD-0211 Russia 326 582.1 566 RD-0105 Russia 316 49.4 125 RD-0107 Russia 326 297.9 410 RD-0109 Russia 324 54.52 121 RD-0110 Russia 326 297.9 408 RD-0205 Russia 322 606.4 552 RD-161P Russia 319 24.5 105 RD-113 Russia 360 1138 1100 RD-119 Russia 352 105.5 168 RD-115 Russia 357 1726 1250 RD-252 Russia 317 940.5 715 RD-262 Russia 317 941 728 RD-219 Russia 293 883 760 RD-223 Russia 314 1697 1240 RD-221 Russia 318 1118 1070 RD-58MF Russia 353 83.4 230 RD-58 Russia 349 83.4 300 RD-57A-1 Russia 460 395 550 RD-58S Russia 361 86.3 230 RD-58Z Russia 361 71 300 RD-704 Russia 407 1966 2422 RD-859 Russia 312 20.05 57 RD-868 Ukraine 325 23.25 203 RD-866 Ukraine 306 5.2 125 RD-864 Ukraine 309 20.2 199 Vega RD-862 Ukraine 331 142.63 192 RD-861G Italy 325 76.45 185 RD-869 Ukraine 313 8.58 196 RD-861K Ukraine 330 77.63 194 RD-858 Ukraine 315 20.1 53 RD-8 Ukraine 342 78.4 380 RD-852 Ukraine 255 48.25 133 RD-854 Ukraine 312 75.5 100 RD-852 Ukraine 280 54.23 113 RD-857 Ukraine 329 137.3 190 RL-10C USA 450 155.7 317 Centaur RL-10A-4-2 USA 451 99.1 167 RL-10A-3A USA 444 73.4 141 RL-10A-3 USA 444 65.6 131 RL-10 USA 410 66.7 131 RL-10A-1 USA 425 66.7 131 RL-10A-4 USA 449 92.5 168 S1.5400 Russia 340 66.7 153 S1.5400A Russia 342 67.3 148 S5.92 Russia 327 19.6 75 S5.98M Russia 326 19.62 95 Sergeant USA 235 6.66 42 SLV-2 India 267 267 1750 SLV-3 India 277 90.7 440 SLV-4 India 283 26.8 98 SR-19 USA 288 267.7 795 SRM-1 USA 296 181.5 1134 SRM-2 USA 304 78.4 1170 Star 37FM USA 290 47.9 81 Star 37S USA 287 45 53 Star 37XFP USA 290 31.5 71 Star 37F USA 286 55.5 67 Star 37E USA 284 68 83 Star 37D USA 266 45 64 Star 37C USA 286 45 83 Star 37B USA 291 45 64 Star 75 USA 288 242.8 565 Star 5C USA 260 43.5 63 Star 43A USA 298 77.11 144 Star 48B s USA 286 77.11 124 Star 48B USA 286 66 126 Star 31 USA 294 80 98 Star 20 USA 287 27.14 28 Star 17A USA 287 16.01 14 Star 17 USA 286 10.9 9 Star 20B USA 289 24.47 33 Star 24 USA 283 20 18 Star 13B USA 286 7.6 6 Star 13A USA 287 5.87 5 Star 13 USA 273 3.8 5 Star 12A USA 270 7.25 11 Falcon 9 Merlin 1D VacSpaceX 348 801 490 Star 10 USA 251 3.35 6 Star 30E USA 291 35.4 45 Star 30C USA 287 32.6 39 Star 30BP USA 292 27 38 Star 27 USA 288 27 27 Star 26C USA 272 35 32 Star 26B USA 272 34.63 23 Star 26 USA 271 39.1 37 Star 24C USA 282 21.47 19 Topaze France 255 120.1 306 Lunar Module AscentTR-201 Stage USA 301 41.9 113 Vexin A France 277 68.6 175 Viking 4 France 296 721 850 Viking 4B France 296 805 850 Ariane V Vinci France 467 180 280 X-248A USA 255 13.8 181 X-248 USA 256 12.4 30 X-254 USA 256 60.5 294 X-259 USA 293 93.1 300 X-259A USA 295 80.8 352 YF-73 China 425 44 236 Zefiro 9 USA 294 313 1000 Zefiro 23 USA 289 1200 3000 Falcon 9 Merlin 1D VacSpaceX FT 348 934 490 Space Shuttle SSME USA 452.3 2279 3500 N-1, Soyuz NK-33 Russia 331 1680 1240 Falcon 9 Merlin 1D VacSpaceX 348 801 490 Falcon 9 Merlin 1D VacSpaceX 348 934 490 467 180 280 317 30.7 52 Inclusion criteria: must be a real engine which does not fire on launchpad during nominal launch sequence. No ion engines, manuvering thrusters or ullage motors - must be able to circularise a suborbital trajectory (in principle). Must be a real engine which flew at least once (flight is allowed to be a failure). Isp and Mass must be known. Hypergolic Fuel Type Isp Thrust/kN Mass/kg Nitric Acid/UDMH 303 157.5 185 Kerolox Kerolox Nitric Acid/UDMH 306 41.4 95 N2O4/Aerozine-50 311 35.6 110 N2O4/Aerozine-50 321 43.4 98 Nitric acid/UDMH 278 33.7 90 Nitric acid/UDMH 271 33.8 90 Nitric acid/UDMH 278 35.1 90 Nitric acid/UDMH 278 0 90 N2O4/Aerozine-50 310 23.3 68 N2O4/MMH 347 20 58 Nitric acid/UDMH 276 68.9 127 Nitric acid/UDMH 285 71.2 130 Nitric acid/UDMH 293 71.2 132 Solid Solid Solid Solid Solid Solid Solid Solid H2O2/Kerosene Solid Solid Hydrolox Hydrolox Hydrolox Solid Hydrolox Hydrolox Kerolox N2O4/UDMH 313 18.8 42 N2O4/UDMH 315 18.9 70 N2O4/UDMH 326 6.19 310 Nitric acid/UDMH 314 18.92 81 Nitric acid/Amine 287 45.5 48 N2O4/MMH 320 27.4 110 Hydrolox Hydrolox Hydrolox N2O4/Aerozine-50 316 467 589 Kerolox N2O4/Aerozine-50 315 444.8 500 Solid Solid Solid Solid Solid Solid Solid Solid Solid Hydrolox Hydrolox Solid Solid Solid Solid Solid Solid Solid Solid Solid Solid Solid N2O4/UDMH 328.6 19.62 95 N2O4/UDMH 326 582.1 566 Kerolox Kerolox Kerolox Kerolox N2O4/UDMH 322 606.4 552 H2O2/Kerosene lox/udmh lox/udmh lox/udmh N2O4/UDMH 317 940.5 715 N2O4/UDMH 317 941 728 Nitric acid/UDMH 293 883 760 Nitric acid/UDMH 314 1697 1240 Nitric acid/UDMH 318 1118 1070 Kerolox Kerolox Hydrolox Kerolox Kerolox Lox/Kerosene/LH2 N2O4/UDMH 312 20.05 57 N2O4/UDMH 325 23.25 203 N2O4/UDMH 306 5.2 125 N2O4/UDMH 309 20.2 199 N2O4/UDMH 331 142.63 192 N2O4/UDMH 325 76.45 185 N2O4/UDMH 313 8.58 196 N2O4/UDMH 330 77.63 194 N2O4/UDMH 315 20.1 53 Kerolox Nitric acid/UDMH 255 48.25 133 N2O4/UDMH 312 75.5 100 N2O4/UDMH 280 54.23 113 N2O4/UDMH 329 137.3 190 Hydrolox Hydrolox Hydrolox Hydrolox Hydrolox Hydrolox Hydrolox Kerolox Kerolox N2O4/UDMH 327 19.6 75 N2O4/UDMH 326 19.62 95 Solid Solid Solid Solid Solid Solid Solid Solid Solid Solid Solid Solid Solid Solid Solid Solid Solid Solid Solid Solid Solid Solid Solid Solid Solid Solid Solid Solid Solid Solid Kerolox Solid Solid Solid Solid Solid Solid Solid Solid Solid N2O4/UDMH 255 120.1 306 N2O4/Aerozine-50 301 41.9 113 N2O4/UDMH 277 68.6 175 N2O4/UDMH 296 721 850 N2O4/UDMH 296 805 850 Hydrolox Solid Solid Solid Solid Solid Hydrolox Solid Solid Kerolox Hydrolox Kerolox Kerolox Kerolox Inclusion criteria: must be a real engine which does not fire on launchpad during nominal launch sequence.
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