Rocket Engines
Name↕ | Engine↕ | Origin↕ | Designer↕ | Vehicle↕ | Status↕ | Use↕ | Propellant↕ | Power cycle↕ | Specific impulse (s)↕ | Thrust (N)↕ | Chamber pressure (bar)↕ | Mass (kg)↕ | Thrust:weight ratio↕ | Oxidizer:fuel ratio↕ |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
Aeon-R | Aeon-R | USA | Relativity Space | Terran R | Development | 1st, 2nd | CH4 / LOX | Gas generator | 1,147,000 | |||||
AJ10-190 | AJ10-190 | USA | Aerojet | Space Shuttle, Orion, Apollo CSM | Active | Upper | N2O4 / MMH | Pressure-fed | 316 | 26,689 | 8.62 | 118 | 23.08 | |
Aquila SL | Aquila SL | Germany | Isar Aerospace | Spectrum | Development | 1st | C3H8 / LOX | Gas generator | 75,000 | |||||
Aquila VAC | Aquila VAC | Germany | Isar Aerospace | Spectrum | Development | 2nd | C3H8 / LOX | Gas generator | 94,000 | |||||
Archimedes | Archimedes | New Zealand USA | Rocket Lab | Neutron | Development | 1st, 2nd | CH4 / LOX | Staged, oxidizer-rich | 730,000 | |||||
BE-3U | BE-3U | USA | Blue Origin | New Glenn | Active | 2nd | LH2 / LOX | Expander, open | 445 | 941,500 | >90 | |||
BE-4 | BE-4 | USA | Blue Origin | New Glenn, Vulcan | Active | 1st | CH4 / LOX | Staged, oxidizer-rich | 340 | 2,846,900 | 138 | |||
BE-7 | BE-7 | USA | Blue Origin | Blue Moon | Development | 1st | LH2 / LOX | Expander, open | 44,500 | 5.5-7.1 | ||||
CE-20 | CE-20 | India | LPSC | GSLV Mk III | Active | Upper | LH2 / LOX | Gas generator | 434 | 196,500 | 60 | 588 | 34.1 | 5.05 |
CE-7.5 | CE-7.5 | India | LPSC | GSLV Mk II | Active | Upper | LH2 / LOX | Staged, fuel-rich | 454 | 73,500 | 58 | 445 | 16.85 | |
E2 | E2 | USA | ABL Space Systems | RS1 | Active | 1st | RP-1 / LOX // Jet-A / LOX | Gas generator | 53,800 | 64 | ||||
E2 Vacuum | E2 Vacuum | USA | ABL Space Systems | RS1 | Active | 2nd | RP-1 / LOX // Jet-A / LOX | Gas generator | 57,800 | |||||
Engine-2 | Engine-2 | USA | Vast | TBA | Development | 1st | RP-1 / LOX | Staged, oxidizer-rich | 327 290 (SL) | 100,000 | 100 | 2.62 | ||
Engine-2 Vacuum | Engine-2 Vacuum | USA | Vast | TBA | Development | 2nd | RP-1 / LOX | Staged, oxidizer-rich | 365 | 100,000 | 2.62 | |||
GEM 63 | GEM 63 | USA | Northrop Grumman | Atlas V | Active | Booster | HTPB | Solid fuel | 279.06 | 1,662,745 | 49,300 with fuel | |||
GEM 63XL | GEM 63XL | USA | Northrop Grumman | Vulcan | Active | Booster | HTPB | Solid fuel | 280.3 | 2,025,720 | 53,400 with fuel | |||
Hadley | Hadley | USA | Ursa Major Technologies | Rocket 4 | Active | 2nd | RP-1 / LOX | Staged, oxidizer-rich | 22,241 (SL) | 62 | ||||
Helix | Helix | Germany | Rocket Factory Augsburg | RFA One | Development | 1st, 2nd | RP-1 / LOX | Staged, oxidizer-rich | 350,325 (SL) | 100,000 | 100 | |||
HyPER-15 | HyPER-15 | South Korea | Innospace | Hanbit-Nano, -Micro, -Mini | Development | 1st | Paraffin / LOX | Electric pump | 292 | 150,000 | ||||
LE-5B-3 | LE-5B-3 | Japan | Mitsubishi, JAXA | H-3 | Active | Upper | LH2 / LOX | Expander, open | 447 | 137,000 | 36 | 269 | 51.93 | 5 |
LE-9 | LE-9 | Japan | Mitsubishi, JAXA | H-3 | Active | 1st | LH2 / LOX | Expander, open | 425 | 1,471,000 | 100 | 2,400 | 62.5 | 5.9 |
Lightning 1 | Lightning 1 | USA | Firefly Aerospace | Alpha | Active | 2nd | RP-1 / LOX | Combustion tap-off | 322 | 70,100 | ||||
M10 | M10 | Europe | Avio | Vega-E | Development | Upper | CH4 / LOX | Expander, closed | 362 | 98,000 | 3.4 | |||
Merlin 1D FT | Merlin 1D FT | USA | SpaceX | Falcon 9 B5, Heavy | Active | 1st | RP-1 / LOX | Gas generator | 311 | 914,000 845,000 (SL) | 108 | 470 | 194.5 | |
Merlin Vacuum 1D | Merlin Vacuum 1D | USA | SpaceX | Falcon 9 B5, Heavy | Active | 2nd | RP-1 / LOX | Gas generator | 348 | 981,000 | 2.36 | |||
Miranda | Miranda | USA | Firefly Aerospace | Antares 300 Series, MLV | Development | 1st | RP-1 / LOX | Combustion tap-off | 305 | 1,023,000 | ||||
NK-33A (AJ26-62), 11Д111 / 14Д15 | NK-33A (AJ26-62), 11Д111 / 14Д15 | Soviet Union | JSC Kuznetsov | Antares 100, Soyuz-2-1v | Retired | 1st | RP-1 / LOX | Staged, oxidizer-rich | 331297 (SL) | 1,680,000 1,510,000 (SL) | 145 | 1,222 | 136.8 | |
P120 | P120 | Italy France | Avio | Ariane 6, Vega-C | Active | Booster, 1st | HTPB | Solid fuel | 279 | 4,650,000 | 105 | 153,000 with fuel | ||
Raptor | Raptor | USA | SpaceX | Starship | Development | 1st, 2nd | CH4 / LOX | Staged, full-flow | 350 327 (SL) | 2,750,000 (SL) | 350 | 1,525 | 184 | 3.6 |
Raptor Vacuum | Raptor Vacuum | USA | SpaceX | Starship | Development | 2nd | CH4 / LOX | Staged, full-flow | 380 est. | >2,750,000 | 350 | >1,525 | <184 | 3.6 |
RD-0124, 14Д23 | RD-0124, 14Д23 | Russia | KBKhA | Soyuz-2.1b, Soyuz-2-1v, Angara | Active | 2nd, 3rd | RP-1 / LOX | Staged, oxidizer-rich | 359 | 294,300 | 160 | 520 | 57.7 | |
RD-0146D | RD-0146D | Russia | KBKhA | Angara | Development | Upper | LH2 / LOX | Expander, closed | 470 | 68,600 | 59 | |||
RD-107A, 14Д22 | RD-107A, 14Д22 | Russia | NPO Energomash | Soyuz-FG, -2 | Active | 1st | RP-1 / LOX | Gas generator | 320.2 263.3 (SL) | 1,019,892 839,449 (SL) | 61.2 | 1,090 | 78.53 | |
RD-108A, 14Д21 | RD-108A, 14Д21 | Russia | NPO Energomash | Soyuz-FG, -2 | Active | 2nd | RP-1 / LOX | Gas generator | 320.6 257.7 (SL) | 921,825 792,377 (SL) | 55.5 | 1,075 | 75.16 | |
RD-171M, 11Д520 | RD-171M, 11Д520 | Russia | NPO Energomash | Soyuz-5, Zenit-2M, -3SL, -3SLB, -3SLBF | Active | 1st | RP-1 / LOX | Staged, oxidizer-rich | 337.2 309.5 (SL) | 7,904,160 7,256,921 (SL) | 250 | 9,300 | 79.57 | |
RD-180 | RD-180 | Russia | NPO Energomash | Atlas V, III | Active | 1st | RP-1 / LOX | Staged, oxidizer-rich | 338.4 311.9 (SL) | 4,152,136 3,826,555 (SL) | 261.7 | 5,480 | 71.2 | 2.72 |
RD-191 | RD-191 | Russia | NPO Energomash | Angara | Active | 1st | RP-1 / LOX | Staged, oxidizer-rich | 337.5 311.2 (SL) | 2,084,894 1,922,103 (SL) | 262.6 | 2,200 | 89.09 | |
RD-276, 14Д14М | RD-276, 14Д14М | Russia | NPO Energomash | Proton-M | Active | 1st | N2O4 / UDMH | Staged, oxidizer-rich | 315.8 288 (SL) | 1,831,882 1,671,053 (SL) | 168.5 | 1,120 | 171.2 | |
RD-801 | RD-801 | Ukraine | Pivdenne/Pivdenmash | Mayak | Development | 1st | RP-1 / LOX | Staged, oxidizer-rich | 336 300.7 (SL) | 1,339,255 1,198,608 (SL) | 180 | 1,630 | 2.65 | |
RD-809K | RD-809K | Ukraine | Pivdenne/Pivdenmash | Mayak | Development | Upper | RP-1 / LOX | Staged, oxidizer-rich | 352 | 98,067 | 330 | 2.62 |
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This dataset contains 85 entries, each with multiple sortable, filterable columns. The full table is visible on this page and can be downloaded as a CSV, JSON, or Excel file.
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