The Wayback Machine - https://web.archive.org/web/20161228034545/http://astronautix.com/r/rd-0105.html
RD-0105

Encyclopedia Astronautica
Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z
RD-0105
Part of S1 Family
RD-0105
RD-0105
Credit: KBKhA
Kosberg LOx/Kerosene rocket engine. Luna 8K72, Vostok 8K72 upper stage. Out of production. Developed jointly with OKB-1 in nine months on the basis of OKB-1's steering chamber from the RD-107 engine. First flight 1958.
See More

AKA: 8D714; RD-428; RO-5; RO-5, RD-428. Status: Out of production. Date: 1957-59. Number: 13 . Thrust: 49.40 kN (11,106 lbf). Unfuelled mass: 125 kg (275 lb). Specific impulse: 316 s. Burn time: 440 s. Diameter: 2.56 m (8.39 ft).

Engine: 125 kg (275 lb). Chamber Pressure: 45.00 bar. Thrust to Weight Ratio: 40.

Country: Russia. Launch Vehicles: Vostok 8K72, Vostok-L 8K72. Propellants: Lox/Kerosene. Stages: Luna 8K72-2, Vostok 8K72-2. Agency: Kosberg bureau. More at: 7463. Bibliography: 174, 307, 344.

Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z
� 1997-2016 Mark Wade - Contact
� / Conditions for Use