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
Angara Stage 2
LOx/LH2 propellant rocket stage. Unique configuration with oxidizer in core and fuel in two tanks strapped on in parallel - all of rail-transportable 3.9 m diameter. Built by NPO Energia to Khrunichev design (their own design for Angara and Energia-M were rejected in favor of Khrunichev version). Masses estimated based on engine selected and vehicle performance. Assumed that engine is throttled back to maintain constant 3-G acceleration.

Status: Development 2004. Thrust: 1,960.00 kN (440,620 lbf). Gross mass: 75,000 kg (165,000 lb). Unfuelled mass: 9,000 kg (19,800 lb). Specific impulse: 455 s. Specific impulse sea level: 352 s. Burn time: 225 s. Height: 16.00 m (52.00 ft). Diameter: 3.90 m (12.70 ft). Span: 12.00 m (39.00 ft).



Country: Russia. Engines: RD-0120M. Propellants: Lox/LH2.

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