RD-0235 (original) (raw)

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RD-0235

Part of RD-0216

RD-0235
Credit: KBKhA

Kosberg N2O4/UDMH rocket engine. UR-100N / RS-18 (SS-19) stage 2. Main engine based on RD-0217 with larger nozzle for altitude operation. Staged combustion cycle. First flight 1972.

Date: 1969-74. Number: 315 . Thrust: 240.00 kN (53,950 lbf). Specific impulse: 320 s.

Chamber Pressure: 175.00 bar.

Family: Storable liquid. Country: Russia. Launch Vehicles: UR-100N, Rokot. Propellants: N2O4/UDMH. Stages: UR-100N Stage 2N. Agency: Kosberg bureau. Bibliography: 339, 353, 7488.

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