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
R-36-0-2
Part of R-36-2
N2O4/UDMH propellant rocket stage. .

Status: Retired 1971. Thrust: 955.99 kN (214,915 lbf). Gross mass: 48,000 kg (105,000 lb). Unfuelled mass: 5,000 kg (11,000 lb). Specific impulse: 317 s. Burn time: 160 s. Height: 9.40 m (30.80 ft). Diameter: 3.00 m (9.80 ft). Span: 3.00 m (9.80 ft).

Cost $ : 2.000 million.



Country: Ukraine. Engines: RD-252. Launch Vehicles: R-36O 8K69, R-36O 8K69M. Propellants: N2O4/UDMH.

Back to top of page
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
© 1997-2019 Mark Wade - Contact
© / Conditions for Use