MB-3-3    Propellant: O2 / Kerosene Thrust (sl): 88,378 kgf (v) Thrust (sl): 77,104 kgf (sl) Burn time: 270 s Specific impulse: 290 s (v) Specific impulse: 253 s (sl) Launch vehicles: N-1, N-2, H-1 First flight: 1975

AJ10-118E    Propellant: HNO3 / (CH3)2NNH2 Thrust: 3,579 kgf (v) Burn time: 400 s Specific impulse: 278 s (v) Launch vehicles: N-1 First flight: 1975

AJ10-118FJ    Propellant: N2O4 / (CH3)2NNH2 Thrust: 4,425 kgf (v) Burn time:  444 s Specific impulse: 321  s (v) Launch vehicles: N-2 First flight: 1981

LE-5     Propellant: O2 / H2 Thrust: 10.503 (v) Specific impulse: 450 (v) Launch vehicles: H1 First flight: 1986

LE-5A     Propellant: O2 / H2 Thrust: 12,430 (v) Specific impulse: 452 (v) Launch vehicles: H2 First flight: 1994

LE-5B     Propellant: O2 / H2 Thrust: 13,970 (v) Specific impulse: 447 (v) Launch vehicles: H-IIA / H3 First flight: 2001

LE-7     Propellant: O2 / H2 Thrust: 110.050 (v) Thrust: 86,002 (sl) Specific impulse: 445 (v) Specific impulse: 348 (sl) Launch vehicles: H2 First flight: 1994

LE-7A     Propellant: O2 / H2 Thrust: 109.500 (v) Thrust: 83,096 (sl) Specific impulse: 429 (v) Specific impulse: 325 (sl) Launch vehicles: H2A First flight: 2001

LE-7A     Propellant: O2 / H2 Thrust: 111,658 (v) Thrust: 85,452 (sl) Specific impulse: 442 (v) Specific impulse: 338 (sl) Launch vehicles: H2B First flight: 2009

LE-9     Propellant: O2 / H2 Thrust: 300,000 (v) Thrust: 249.120 (sl) Specific impulse: 425 (v) Specific impulse: 353 (sl) Launch vehicles: H3