RD-0215

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RD-0215

Part of RD-0202

Kosberg N2O4/UDMH rocket engine. Developed 1962-65 for heavy Chelomei launcher (UR-900?) stage 1. Engine unit consisting of 1 RD-0217 for tank pressurization and three RD-0216. Hardware not hot-tested.

Status: Developed 1962-65. Date: 1962-65. Thrust: 2,450.00 kN (550,780 lbf). Specific impulse: 310 s. Specific impulse sea level: 280 s. Burn time: 102 s. Diameter: 2.00 m (6.50 ft).

Engine unit (DU) consisting of 1 RD-0217 for tank pressurization and three RD-0216. Intended for stage 1 of heavy launcher by Chelomei. Development stopped, hardware not hot-tested. Staged combustion cycle with ox.-rich gas generator.

Chambers: ?.

Family: Storable liquid. Country: Russia. Launch Vehicles: UR-100. Propellants: N2O4/UDMH. Stages: 8S816. Agency: Kosberg bureau. Bibliography: 309.

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