RD-302

RD-302

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Engine Model: RD-302. Manufacturer Name: RD-302. Government Designation: 11D130F. Other Designations: 11D130F. Designer: Glushko. Developed in: 1960-69. Propellants: LF2/Ammonia. Thrust(vac): 98.000 kN (22,031 lbf). Isp: 405 sec. Chambers: 1. Chamber Pressure: 117.60 bar. Country: Russia. Status: Developed 1960-69.

Successor to RD-303 and predecessor to RD-301. Staged combustion cycle.

Bibliography:

Rakhmanin, V F, Odnazhdy i Navsegda, NPO Energomash, Moscow 1998 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.

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