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RD-102
Part of Model 39
Glushko LOx/Alcohol rocket engine. R-3A. Development ended 1951. Project for R-3A experimental missile. Stopped in favor of RD-103.

AKA: RD-3A. Status: Development ended 1951. Thrust: 428.00 kN (96,218 lbf). Specific impulse: 235 s. Specific impulse sea level: 214 s. Burn time: 83 s.

Propellant Formulation: Lox/Alcohol-96%.

Country: Russia. Launch Vehicles: R-3A. Propellants: Lox/Alcohol. Stages: R-3A stage. Agency: Glushko bureau. Bibliography: 283.
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