LRBA     Propellant: HNO3 / Turpentine Thrust: 3,895 kgf (sl) Specific impulse: 198 s (sl) Launch vehicles: Veronique-N

LRBA     Propellant: HNO3 / Turpentine Specific impulse: 189 s (sl) Launch vehicles: Parca

LRBA     Propellant: HNO3 / Turpentine Thrust: 4,099 kgf (sl) Specific impulse: 189 s (sl) Launch vehicles: Veronique-AGI

LRBA     Propellant: HNO3 / Turpentine Thrust: 5,853 kgf (sl) Specific impulse: 189 s (sl) Launch vehicles: Veronique-61

LRBA     Propellant: HNO3 / Turpentine Thrust: 14,255kgf (sl) Specific impulse: 189 s (sl) Launch vehicles: Vesta First flight: 1965

Vexin     Propellant: HNO3 / Turpentine Thrust: 27,909 kgf (sl) Specific impulse: 203 s (sl) Launch vehicles: Emeraude, Saphir, Diamant-A First flight: 1962

Vexin A (1)     Propellant: N2O4 / (CH3)2NNH2 Launch vehicles: Cora First flight: 1966

Vexin A (2)     Propellant: N2O4 / (CH3)2NNH2 Thrust: 26,716 kgf (v) Specific impulse: 281 s (v) Launch vehicles: Europa First flight: 1969

Valois 1     Propellant: N2O4 / (CH3)2NNH2 Thrust: 35,750 (sl) Specific impulse: 221 (sl) Launch vehicles: Amethyste, Diamant-B First flight: 1964

Valois 2     Propellant: N2O4 / (CH3)2NNH2 Thrust: 32,294 kgf (sl) Specific impulse: 212 s (sl) Launch vehicles: Diamant-BP First flight: 1975

Gamma 2     Propellant: H2O2 / Kerosen Thrust: 6,950 kgf Burn time: 113 s Specific impulse: 265 s (v) Launch vehicles: Black Arrow First flight: 1969

Gamma 8        Thrust: 23,942 kgf (sl) Burn time: 142 s Specific impulse: 265 s (v) Launch vehicles: Black Arrow First flight: 1969

RZ.2     Propellant: O2 / Kerosene Thrust: 68,422 kgf (sl) Specific impulse: 248 s (sl) Launch vehicles: Blue Strike First flight: 1964    RZ.2     Thrust: 75,000 kgf Launch vehicles: Europa First flight:1966

Viking 1     Propellant: N2O4 / (CH3)2NNH2 Thrust: 55,003 kgf (sl) Launch vehicles: Europe3 First flight: ?

Viking 2     Propellant: N2O4 / (CH3)2NNH2 Launch vehicles: L3S First flight: ?

Viking 3     Propellant: N2O4 / (CH3)2NNH2 Launch vehicles: L3S First flight: ?

Viking 4     Propellant: N2O4 / (CH3)2NNH2 Thrust: 72,705 (v) Specific impulse: 290 s (v) Launch vehicles: Ariane 1 First flight: 1990

Viking 4B     Propellant: N2O4 / (CH3)2NNH2 Thrust: 80,027 kgf (v) Specific impulse: 290 s (v) Launch vehicles: Ariane 2 / 3 First flight: 1984    Viking 4B+     Propellant: N2O4 / (CH3)2NNH2 Thrust: 82,372 kgf (v) Specific impulse: 292 s (sl)) Launch vehicles: Ariane 4 First flight: 1990

Viking 5     Propellant: N2O4 / (CH3)2NNH2 Thrust: 68,066 kgf (v) Thrust: 60,826 kgf (sl) Specific impulse: 267 s (v) Specific impulse: 239 s (sl)) Launch vehicles: Ariane 1 First flight: 1979

Viking 5B     Propellant: N2O4 / (CH3)2NNH2 Thrust: 73,419 kgf (v) Thrust: 65,771 kgf (sl) Specific impulse: 270 s (v) Specific impulse: 242 s (sl) Launch vehicles: Ariane 2 / 3 First flight: 1984

Viking 5C     Propellant: N2O4 / (CH3)2NNH2 Thrust: 77,498 kgf (v) Thrust: 69,218 kgf (sl) Specific impulse: 278 s (v) Specific impulse: 248 s (sl) Launch vehicles: Ariane 4 First flight: 1990

Viking 6     Propellant: N2O4 / (CH3)2NNH2 Thrust: 76,376 kgf (v) Thrust: 68,320 kgf (sl) Specific impulse: 274 s (v) Specific impulse: 245 s (sl) Launch vehicles: Ariane 4 First flight: 1990

Astris 1     Propellant: N2O4 / Aerozine-50 Thrust: 2,304 kgf (v) Burn time: 330 s Specific impulse: 300 s (v) Launch vehicles: Europa I First flight: 1966

Astris 2     Propellant: N2O4 / Aerozine-50 Thrust: 2,375 kgf (v) Burn time: 330 s Specific impulse: 310 s (v) Launch vehicles: Europa 2 First flight: 1970

Aestus     Propellant: N2O4 / (CH3)NHNH2 Thrust: 2,997 kgf (v) Burn time: 1,000 s Specific impulse: 321 s (v) Launch vehicles: Ariane 5G First flight: 1996

Aestus+     Propellant: N2O4 / (CH3)NHNH2 Thrust: 3,059 kgf (v) Burn time: 1,000 s Specific impulse: 323 s (v) Launch vehicles: Ariane 5G+ First flight: 2004

HM-7A     Propellant: O2 / H2 Thrust: 6,363 (v) Burn time: 563 s Specific impulse: 440 (v) Launch vehicles: Ariane 1 First flight: 1979

HM-7B     Propellant: O2 / H2 Thrust: 6,546 (v) Specific impulse: 442 (v) Launch vehicles: Ariane 2 / 3 / 4 First flight: 1984

HM-7B+     Propellant: O2 / H2 Thrust: 6,587 (v) Specific impulse: 444 (v) Launch vehicles: Ariane 4 (+) First flight: 1992

HM-7B++     Propellant: O2 / H2 Thrust: 6,607 (v) Specific impulse: 446 (v) Launch vehicles: Ariane 4 (3) First flight: 1994

HM-7B++     Propellant: O2 / H2 Thrust: 6,607 (v) Burn time:  731 s Specific impulse: 446 (v) Launch vehicles: Ariane 5E First flight: 2002

Vulcain     Propellant: O2 / H2 Thrust: 114,720 kgf Thrust: 90,244 kgf (sl) Burn time: 605 s Specific impulse: 43 s (v) Specific impulse: 33 s (sl) Launch vehicles: Ariane 5G First flight: 1996

Vulcain +     Propellant: O2 / H2 Thrust: 116,250 kgf Thrust: 91,468 kgf (sl) Burn time: 605 s Specific impulse: 431 s (v) Specific impulse: 339 s (sl) Launch vehicles: Ariane 5G+ First flight: 2004

Vulcain 2     Propellant: O2 / H2 Thrust: 138,170 kgf (v) Thrust: 108,910 kgf (sl) Specific impulse: 414 s (v) Specific impulse: 362 s (sl) Launch vehicles: Ariane 5E First flight: 2002

Vulcain 3     Propellant: O2 / H2 Thrust: 154,590 kgf (v) Thrust: 135,210 kgf (sl) Specific impulse: 414 s (v) Specific impulse: 362 s (sl) Launch vehicles: Ariane 6

Vinci     Propellant: O2 / H2 Thrust: 18,354 (v) Specific impulse: 465 (v) Launch vehicles: Ariane 5ECB / ME