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-2
Part of RD-1 Family
Glushko Nitric acid/Kerosene rocket engine. experimental. Developed 1945-47. The RD-2 was based on the RD-1 engine. Used chemical ignition.

Status: Developed 1945-47. Date: 1945-47. Thrust: 6.00 kN (1,349 lbf). Unfuelled mass: 71 kg (156 lb). Specific impulse: 200 s.

Throttled thrust(vac): 2.000 kN (450 lbf). Engine: 71 kg (156 lb). Chamber Pressure: 20.60 bar. Thrust to Weight Ratio: 8.61.



Family: Storable liquid. Country: Russia. Propellants: Nitric acid/Kerosene. Agency: Glushko bureau. Bibliography: 342.

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
© 1997-2017 Mark Wade - Contact
© / Conditions for Use