Engine Model: RD-0102. Manufacturer Name: RD-0102. Other Designations: SK1K. Designer: Kosberg. Developed in: 1954-58. Application: Yak-27V aircraft by Yakovlev. Propellants: Lox/Kerosene. Thrust(vac): 39.200 kN (8,813 lbf). Throttled thrust(vac): 14.700 kN (3,305 lbf). Isp: 260 sec. Burn time: 330 sec. Chambers: 1. Chamber Pressure: 41.20 bar. Country: Russia. Status: Out of Production. Based on RD-0101. Two ignitions possible. Chamber pressure 41,2 - 16,4 bar.
Bibliography:- Golubev, A A, KB KhimAvtomatiki - Straniy Istorii, Vol. 1, Voronezh 1995 via Dietrich Haeseler.
- Siddiqi, Asif A, Soviet Space Web Page, 1999 via Dietrich Haeseler. Web Address when accessed: http://home.earthlink.net/~cliched/main_space.html.
- Ivanenko, V N, Issled. Po Ist. I Teorii Razv. Aviat. i Raketo-Kosm. Nauki i Tekhniki, "O Zhizn i Deyatelnosti S.A. Kosberg", AN SSSR, Moscow 1986.