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
Centaur II
Part of Centaur stage series
LOx/LH2 propellant rocket stage. .

Status: Out of production. Thrust: 146.80 kN (33,002 lbf). Gross mass: 18,833 kg (41,519 lb). Unfuelled mass: 2,053 kg (4,526 lb). Specific impulse: 444 s. Burn time: 488 s. Height: 10.10 m (33.10 ft). Diameter: 3.05 m (10.00 ft). Span: 3.05 m (10.00 ft).

Cost $ : 25.000 million. No Engines: 2.



Family: Space Tugs. Country: USA. Engines: RL-10A-3A. Launch Vehicles: Atlas II. Propellants: Lox/LH2.

Back to top of page
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
© 1997-2019 Mark Wade - Contact
© / Conditions for Use