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 and Further Reading

Rakhmanin, V F, Odnazhdy i Navsegda, NPO Energomash, Moscow 1998 via Dietrich Haeseler. Biography and history of development of the rocket motors of Glushko.

Siddiqi, Asif A, Soviet Space Web Page, 1999 via Dietrich Haeseler. Asif Siddiqi presents material that could not be fit into his monumental 'Challenge to Apollo'. Accessed at: http://home.earthlink.net/~cliched/main_space.html.

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