This page no longer updated from 31 October 2001. Latest version can be found at www.astronautix.com

astronautix.com RD-0105


Manufacturer Name: RD-0105. Government Designation: 8D714. Other Designations: RO-5, RD-428. Designer: Kosberg. Developed in: 1957-59. Application: R-7 8K72 Luna stage 3 (block E-Luna). Used on stages: Luna 8K72-2, Vostok 8K72-2. Used on launch vehicles: Luna 8K72, Vostok 8K72. Propellants: Lox/Kerosene Thrust(vac): 5,000 kgf. Thrust(vac): 49.40 kN. Isp: 316 sec. Burn time: 440 sec. Mass Engine: 125 kg. Diameter: 2.6 m. Chambers: 1. Chamber Pressure: 45.00 bar. Country: Russia. Status: Out of Production. First Flight: 1958. Last Flight: 1960. Flown: 13. References: 174 , 307 , 344 . Comments: RD-0105 was developed jointly with OKB-1 on the basis of a steering chamber from RD-107 engine, which was developed by OKB-1. Developed in nine months.
Back to Index
Last update 12 March 2001.
Definitions of Technical Terms.
Contact Mark Wade with any corrections or comments.
Conditions for use of drawings, pictures, or other materials from this site..
© Mark Wade, 2001 .