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RD-0216


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RD-0216
Credit: KBKhA Kosberg N2O4/UDMH rocket engine. UR-100 stage 1. Staged combustion cycle. Includes tank pressurization system (RD-0217 without tank press.). First launch November 1963, manufactured until 1974, operational until 1991. First flight 1965.

AKA: 15D2. Status: Design 1964. Date: 1963-66. Number: 1128 . Thrust: 219.00 kN (49,233 lbf). Specific impulse: 313 s.

Chamber Pressure: 147.00 bar.

Subtopics RD-0217 Kosberg N2O4/UDMH rocket engine. UR-100, UR-100K stage 1. Out of Production. Staged combustion cycle. Version of RD-0216 without tank pressurization system. Manufacturing until 1974, operational use until 1991. RD-0235 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. Family: Storable liquid. Country: Russia. Launch Vehicles: Taran, UR-100M SLBM, UR-100, UR-100M. Propellants: N2O4/UDMH. Stages: 8S816. Agency: Kosberg bureau. Bibliography: 342, 344, 7484. Back to top of page Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
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