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R-36-2


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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-36-2 N2O4/UDMH propellant rocket stage. Verniers 4 x RD-69M, 54.3 kN, maximum 50 degree gimbal angle.

Status: Retired 1975. Thrust: 940.40 kN (211,410 lbf). Gross mass: 49,300 kg (108,600 lb). Unfuelled mass: 3,700 kg (8,100 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.

Subtopics R-36-0-2 N2O4/UDMH propellant rocket stage. . R-36M2-1 N2O4/UDMH propellant rocket stage. Surplus ICBMs; failures based on ICBM tests through 1994. R-36M-2 N2O4/UDMH rocket stage. 760.00 kN (170,855 lbf) thrust. Mass 49,000 kg (108,027 lb). R-36M2-2 N2O4/UDMH propellant rocket stage. Surplus ICBMs; failures based on ICBM tests through 1994. Country: Ukraine. Engines: RD-252. Launch Vehicles: R-36 8K67, Tsiklon, Tsiklon-2A, R-36 8K67M, R-36 8K67P, R-36 8K67MA, R-36 8K67PM. Propellants: N2O4/UDMH. Back to top of page Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
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