RD-262 (original) (raw)

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RD-262

Part of RD-215

Glushko N2O4/UDMH rocket engine. Tsyklon 3 stage 2. In production. Based on RD-252 First flight 1977.

Status: In production. Date: 1967-69. Number: 121 . Thrust: 941.00 kN (211,545 lbf). Unfuelled mass: 728 kg (1,604 lb). Specific impulse: 318 s. Burn time: 160 s. Height: 2.19 m (7.17 ft). Diameter: 1.28 m (4.20 ft).

Chambers: 2. Engine: 728 kg (1,604 lb). Chamber Pressure: 89.50 bar. Area Ratio: 46.1. Thrust to Weight Ratio: 131.86. Oxidizer to Fuel Ratio: 2.6.

Family: Storable liquid. Country: Russia. Launch Vehicles: Tsiklon-3. Propellants: N2O4/UDMH. Stages: Tsyklon 3-2. Agency: Glushko bureau. Bibliography: 342, 344, 349.

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