Liquid engines:
MON is N2H4 with an NO admixture.
Engine | Manu. | Type | Thrust/kN | SI/s | Time | Notes | Size |
RL10A-1 | P&W | LOX/LH2 | ? | 425.0 | |||
RL10A-3 | P&W | LOX/LH2 | 66.6 | 431.0 | |||
RL10A-3S | P&W | LOX/LH2 | 66.6 | 431.0 | SIV, no restart | ||
RL10A-3-1 | P&W | LOX/LH2 | 66.6 | 444.0 | AC, no restart | ||
RL10A-3-3 | P&W | LOX/LH2 | 66.6 | 444.0 | AC, restart | ||
RL10A-3-3A | P&W | LOX/LH2 | 73.4 | 444.4 | |||
RL10A-4 | P&W | LOX/LH2 | 92.5 | 448.9 | |||
RL10A-4-1 | P&W | LOX/LH2 | 99.2 | 451.0 | |||
RL10A-4-2 | P&W | LOX/LH2 | 99.2 | 451.0 | |||
RL10B-2 | P&W | LOX/LH2 | 110.1 | 462.4 | |||
J-2S | Rocketdyne | LOX/LH2 | 900? | Aerospike | |||
RS-68 | Rocketdyne | LOX/LH2 | |||||
Vulcain (C1000K) | Snecma,SEP/DASA | LOX/LH2 | 1145 | 440.4 | 1.85d 3.07l | ||
Vulcain Mk 2 | Snecma | LOX/LH2 | 1350 | ||||
HM-7 (C70K) | ?/DASA | LOX/LH2 | 70 | 443.4 | 1.0d 1.8l | ||
RL-50 | P&W | LOX/LH2 | 260.0 | 470? | |||
HM-7B | ? | LOX/LH2 | AR5C-A | ||||
LE-7 | LOX/LH2 | 844 | H-II St1 | ||||
LE-7A | LOX/LH2 | H-2A St1 | |||||
LE-5 | LOX/LH2 | H-I st2 | |||||
LE-5A | LOX/LH2 | 137 | H-II st2 | ||||
LE-5B | LOX/LH2 | 137 | H-2A St2 | ||||
Vinci | Snecma | LOX/LH2 | 155 | 464.0 | AR5C-B | ||
KVD-1 | Khimmash | LOX/LH2 | 70 | 463 | GSLV, Angara | ||
YF-75 | CALT | LOX/LH2 | 78 | 437 | CZ-3A | ||
YF-73 | CALT | LOX/LH2 | 44 | 420 | CZ-3 | ||
RS-27 | Rocketdyne | LOX/Ker | 912 | 224s | EELT | ||
X-405 | GE | LOX/Ker | 124 | 250 | Vanguard | ||
RD-180 | Energomash | LOX/RP-1 | 4152v | 337 | |||
RS-27A | Rocketdyne | LOX/RP-1 | 1054 | 302 | 265s | ||
MA-5A | Rocketdyne | LOX/RP-1 | 2150 | ||||
MA-5A (S) | Rocketdyne | LOX/RP-1 | 2065v | 293 | |||
MA-5A (B) | Rocketdyne | LOX/RP-1 | 381v | 311 | |||
MB-3 (DM18A) | Rocketdyne | LOX/RP-1 | 676 | ||||
MB-3 (DM21 ) | Rocketdyne | LOX/RJ-1 | 765 | ||||
SR-S | Microcosm | LOX/Ker | 22 | Scorpius | |||
Fastrac | MSFC | LOX/RP-1 | 265 | X-34 | |||
XLR-10-RM-2 | LOX/Alcohol | 93 | 109s | Viking | |||
YF-3 | SLREC | NA27S/UDMH | 320 | 287 | - | CZ-1 S2 | |
YF-1 | SLREC | NA27S/UDMH | 255 | 240 | - | CZ-1 (4x) | |
AJ10-37 | Aerojet | WIFNA/UDMH | 33.4 | 265 | 110s | Vanguard St2 | |
AJ10-101 | Aerojet | 34.7 | 275 | Able | |||
AJ10-104 | Aerojet | 36.3 | 287 | Ablestar | |||
AJ10-118 | Aerojet | WIFNA/UDMH | 33.4 | 110s | Delta | ||
AJ10-118A | Aerojet | IRFNA/UDMH | 34.3 | 110s | Delta B | ||
YF-20 | SLREC | N2O4/UDMH | 696 | 259 | - | CZ-2C St1 | |
YF-20B | SLREC | N2O4/UDMH | 740 | 260 | - | CZ-3A St1 | |
YF-22 | SLREC | N2O4/UDMH | 720 | 289 | - | CZ-2C St2 | |
YF-22B | SLREC | N2O4/UDMH | 720 | 289 | - | CZ-3A St2 | |
YF-40 | SLREC | N2O4/UDMH | 100 | 306 | CZ-4 St3 | ||
AJ10-118D | Aerojet | N2O4/AZ-50 | 33.4 | 165s | Delta B | ||
AJ10-118K | Aerojet | N2O4/AZ-50 | 43.7 | 319 | 445s | Delta ITIP | |
LR87-AJ-5 | Aerojet | N2O4/AZ-50 | 1913 | 296 | 158s | ||
LR91-AJ-5 | Aerojet | N2O4/AZ-50 | 445 | 316 | 175s | ||
RD-861 | Yuzhnoe | N2O4/UDMH | [7] | ||||
Vikas | ISRO | N2O4/UDMH | 725 | 295 | 149s | PS2 | |
PS4 Engine | ISRO | N2O4/MMH | 7.5 | 308 | 425s | PS4 | |
Aestus | DASA | N2O4/MMH | 29.8 | 324.2 | 1100s | 1.32d 2.2l | |
S400/1 | DASA | MON/MMH | 0.40 | 303.2 | 0.25d 0.53l | ||
S400/2 | DASA | MON/MMH | 0.40 | 318.3 | 0.25d 0.53l | ||
TR-201 | TRW | N2O4/AZ-50 | 41.9 | 301.3 | 350s | Delta | |
TR-306 | TRW | N2O4/N2H4 | 0.45 | 314.5 | - | Anik E | |
TR-308 | TRW | N2O4/N2H4 | 0.47 | 322.3 | - | Chandra | |
MRE-50 | TRW | Hyd | 0.23 | 230 | - | Mariner 69 | |
CHT-400 | DASA | Hyd | 0.40 | 228.5 | 0.09d 0.32l | ||
MRE-5.0 | TRW | N2H4 | 0.036 | 235 | - | GRO | |
SPD-50 | Fakel | Xe | 20mN | 1250 | 2250hr | Meteor; Hall eff. | |
SPD-60 | Fakel | Xe | 30mN | 1250 | 2500hr | Meteor | |
SPD-70 | Fakel | Xe | 40mN | 1500? | 3100hr | Plazma, Geizer/Luch | |
SPD-100 | Fakel | Xe | 83mN | 1600 | 7500hr | Gals/Ekspress | |
NSTAR | Hughes/Torrance | Xe | 90mN | 2500W | DS1 |