RD-0245 (original) (raw)

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RD-0245

Kosberg N2O4/UDMH rocket engine. R-29RM / RSM-54 (SS-N-23) stage 1 vernier. Out of Production. Four-chamber steering engine in system RD-0243 driven by turbine exhaust gas. First flight 1985.

Status: Out of Production. Date: 1977-85. Thrust: 211.00 kN (47,434 lbf). Specific impulse: 300 s. Specific impulse sea level: 280 s. Burn time: 79 s.

Chambers: 4. Chamber Pressure: 147.00 bar. Area Ratio: 14. Oxidizer to Fuel Ratio: 2.6.

Subtopics

RD-0245-HC Kosberg LOx/Kerosene rocket engine. Design concept 1990's. Proposed variant of RD-0245 engine using LOX-kerosene instead of N2O4/UDMH as propellants.

Family: Storable liquid. Country: Russia. Launch Vehicles: R-29RM. Propellants: N2O4/UDMH. Agency: Kosberg bureau. Bibliography: 309, 312, 342, 96, 7493.

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