RD-0110
Type: Upper Stage Engine
Country of Origin: Soviet Union
Manufacturer: Voronezh Mechanical Plant
First Flight: October 5, 1965
Status: Active
Propellant (O/F): Liquid Oxygen/Kerosene
Mixture Ratio (O/F by mass): 2.2
Cycle: Gas Generator
Chambers: 4
Thrust (vac.): 298 kN
Thrust (s.l.):
Throttle:
ISP (vac.): 326 s
ISP (s.l.):
Chamber Pressure: 990 psi
Nozzle Ratio:
Burn time: 250 sec
Ignitions: 1
Mass: 408.5 kg
Length: 1.575 m
Diameter: 2.24 m
Used in: Molniya-M, Soyuz
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