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 A-2
Part of R-7 Block I stage series Family
LOx/Kerosene propellant rocket stage. Two thrust levels. Propellant ration 2.6:1, chamber pressure 162 bar.

Status: In development. Thrust: 294.00 kN (66,093 lbf). Gross mass: 25,200 kg (55,500 lb). Unfuelled mass: 2,355 kg (5,191 lb). Specific impulse: 359 s. Burn time: 300 s. Height: 6.70 m (21.90 ft). Diameter: 2.66 m (8.72 ft). Span: 2.66 m (8.72 ft).



Country: Russia. Engines: RD-0124. Launch Vehicles: Angara-1.2PP, Angara 3A. Propellants: Lox/Kerosene.

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