RD-217

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RD-217

Part of RD-215

Glushko Nitric acid/UDMH rocket engine. R-16 stage 1. Out of Production. Original intended use unknown. Three RD-217 clustered to make RD-218. First flight 1961.

AKA: 8D515. Status: Out of Production. Date: 1958-61. Thrust: 865.00 kN (194,459 lbf). Unfuelled mass: 980 kg (2,160 lb). Specific impulse: 289 s. Specific impulse sea level: 246 s.

Chambers: 2. Engine: 980 kg (2,160 lb). Chamber Pressure: 73.60 bar. Area Ratio: 18.8. Propellant Formulation: AK27I/UDMH. Thrust to Weight Ratio: 90. Oxidizer to Fuel Ratio: 2.5.

Family: Storable liquid. Country: Russia. Propellants: Nitric acid/UDMH. Stages: R-16-1. Agency: Glushko bureau. Bibliography: 320.

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