RD-0124-14D23
Engine · Russia
Original archive entry. The text, images and links below are kept as they were written.
Kosberg LOx/Kerosene rocket engine. Proposed in 1993 for Angara stage 2 verniers, Kvant-1 stage 1 vernier. Designed 1986-1990. 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. Also proposed by RKK Energia in initial studies in 1993 for Angara upper stage.
Chambers: 4. Chamber Pressure: 173.50 bar. Oxidizer to Fuel Ratio: 2.6.
Related
- Country
- Russia
- Launch Vehicles
- Kvant-1
- Propellants
- Lox/Kerosene
- Stages
- Kvant-1-1
- Agency
- Kosberg bureau