RD-0124-14D23

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RD-0124-14D23

Part of RD-0106

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.

AKA: 14D23. Status: Designed 1986-1990. Thrust: 298.64 kN (67,137 lbf). Specific impulse: 331 s. Burn time: 300 s.

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.

Country: Russia. Launch Vehicles: Kvant-1. Propellants: Lox/Kerosene. Stages: Kvant-1-1. Agency: Kosberg bureau. Bibliography: 21, 312.

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