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
UR-700-2
N2O4/UDMH propellant rocket stage. .

Status: Development ended 1968. Thrust: 20,182.00 kN (4,537,094 lbf). Gross mass: 1,072,000 kg (2,363,000 lb). Unfuelled mass: 75,600 kg (166,600 lb). Specific impulse: 322 s. Specific impulse sea level: 301 s. Burn time: 306 s. Height: 34.20 m (112.20 ft). Diameter: 8.30 m (27.20 ft). Span: 8.30 m (27.20 ft).

No Engines: 3.



Country: Russia. Engines: RD-270. Launch Vehicles: UR-700. Propellants: N2O4/UDMH.

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