RD-0103

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RD-0103

Part of RD-0100 engine series

Kosberg LOx/Kerosene rocket engine. T-3, P-1 aircraft by Sukhoi. Out of Production. Based on RD-0102. Chamber pressure 37.3 - 15.7 bar.

Status: Out of Production. Date: 1957. Thrust: 34.60 kN (7,778 lbf). Specific impulse: 277 s.

Throttled thrust(vac): 13.700 kN (3,080 lbf). Chamber Pressure: 37.30 bar. Propellant Formulation: LOX/TS1.

Country: Russia. Propellants: Lox/Kerosene. Agency: Kosberg bureau. Bibliography: 309.

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