RD-0124
Type: Upper Stage Engine
Country of Origin: Russia
Manufacturer: Voronezh Mechanical Plant
First Flight: December 27, 2006
Status: Active
Propellant (O/F): Liquid Oxygen/Kerosene
Mixture Ratio (O/F by mass):
Cycle: Staged Combustion
Chambers: 4
Thrust (vac.): 294.3 kN
Thrust (s.l.):
Throttle:
ISP (vac.): 359 s
ISP (s.l.):
Chamber Pressure:2280 psi
Nozzle Ratio:
Burn time: 300 sec; 424 sec (RD-0124A)
Ignitions: 1
Mass: 572 kg; 548 kg (RD-0124A)
Length: 1.575 m
Diameter: 2.4 m
Used in: Soyuz 2.1b, Soyuz 2.1v, Angara 1.2 (RD-0124A), Angara 5 (RD-0124A)
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