RD-0211 (original) (raw)

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-0211

Part of RD-0202

Kosberg N2O4/UDMH rocket engine. Proton stage 2. Out of Production. Variant of RD-0210 providing tank pressurization. Staged combustion cycle.

AKA: 8D412K;RD-468. Status: Out of Production. Date: 1962-65. Thrust: 582.10 kN (130,861 lbf). Unfuelled mass: 566 kg (1,247 lb). Specific impulse: 327 s. Burn time: 230 s. Height: 2.33 m (7.64 ft). Diameter: 1.47 m (4.82 ft).

Thrust (sl): 421.900 kN (94,847 lbf). Thrust (sl): 43,020 kgf. Engine: 566 kg (1,247 lb). Chamber Pressure: 147.00 bar. Area Ratio: 81.3. Thrust to Weight Ratio: 104.87.

Family: Storable liquid. Country: Russia. Propellants: N2O4/UDMH. Stages: Proton K-2. Agency: Kosberg bureau. Bibliography: 307, 95, 7480.

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