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RD-0244


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RD-0244
Credit: KBKhA Kosberg N2O4/UDMH rocket engine. R-29RM / RSM-54 (SS-N-23) stage 1. Out of Production. Main engine in system RD-0243. Staged combustion cycle. Submerged in propellant tank. First flight 1985.

Status: Out of Production. Date: 1977-85. Thrust: 682.00 kN (153,319 lbf). Specific impulse: 310 s. Specific impulse sea level: 280 s. Burn time: 74 s.

Chamber Pressure: 275.00 bar. Area Ratio: 2. Oxidizer to Fuel Ratio: 2.6.

Family: Storable liquid. Country: Russia. Launch Vehicles: R-29RM. Propellants: N2O4/UDMH. Stages: R-29-1. Agency: Kosberg bureau. Bibliography: 309, 312, 342, 96, 7492. Back to top of page Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
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