RD-107
Propellant: O2 / Kerosene
Thrust: 99,014 kgf (v)
Thrust: 80,884 kgf (sl)
Burn time: 140 s
Specific impulse: 306 s (v)
Specific impulse: 250 s (sl)
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RD-108
Propellant: O2 / Kerosene
Thrust: 92,998 kgf (v)
Thrust: 72,768 kgf (sl)
Burn time: 340 s
Specific impulse: 308 s (v)
Specific impulse: 241 s (sl)
Launch vehicles: R-7, Vostok, Voskhod, Molniya, Soyuz
First flight: 1957
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S1.35800
Propellant: O2 / Kerosene
Thrust: 2,865 kgf (sl)
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