This page no longer updated from 31 October 2001. Latest version can be found at RD-0124-14D23

Manufacturer Name: RD-0124-14D23. Government Designation: 14D23. Designer: Kosberg. Application: Kvant-1 stage 1 vernier. Propellants: Lox/Kerosene Thrust(vac): 30,453 kgf. Thrust(vac): 298.64 kN. Isp: 331 sec. Burn time: 300 sec. Chambers: 4. Chamber Pressure: 173.50 bar. Oxidizer to Fuel Ratio: 2.60. Country: Russia. Status: Developed 1990's. Comments: Variant of RD-0124 with shortened nozzle for sea-level operation. Proposed for small launcher Kvant-1 by RKK Energia for stage 1 steering engine.
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Last update 12 March 2001.
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© Mark Wade, 2001 .