Application: R-36M UTTKh / RS-20B (SS-18 Mod 2) vehicle bus. Out of Production. Two thrust levels. The four thruster swing out of the stage housing before use. Chamber pressure 41 / 17 bar. Specific impulse 309 / 298 sec.
Status: Out of Production. Date: 1976-78. Thrust: 20.20 kN (4,541 lbf). Unfuelled mass: 199 kg (438 lb). Specific impulse: 309 s. Burn time: 600 s. Height: 1.42 m (4.65 ft). Diameter: 3.00 m (9.80 ft).
Diameter 3.0 / 4.02 m.
Chambers: 4. Throttled thrust(vac): 8.450 kN (1,900 lbf). Engine: 199 kg (438 lb). Chamber Pressure: 41.00 bar. Thrust to Weight Ratio: 10.35. Oxidizer to Fuel Ratio: 1.8.
Family: Storable liquid. Country: Ukraine. Propellants: N2O4/UDMH. Agency: Yuzhnoye. Bibliography: 348. Back to top of page Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9RetroSearch is an open source project built by @garambo | Open a GitHub Issue
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