Engine Model: RD-102. Manufacturer Name: RD-102. Other Designations: RD-3A. Designer: Glushko. Application: R-3A. Propellants: Lox/Alcohol. Thrust(vac): 428.000 kN (96,218 lbf). Isp: 235 sec. Isp (sea level): 214 sec. Burn time: 83 sec. Chambers: 1. Country: Russia. Status: Development ended 1951. Project for R-3A experimental missile. Stopped in favor of RD-103.
RD-102 used on Rocket Stages
- Used on stage: R-3A. on launch vehicle: R-3A.
Bibliography:- Vetrov, G S, S. P. Korolev i evo delo, Nauka, Moscow, 1998.