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
Atlas G/H/I
Part of Atlas A stage Family
LOx/Kerosene propellant rocket stage. .

Status: Out of production. Thrust: 386.30 kN (86,844 lbf). Gross mass: 142,536 kg (314,238 lb). Unfuelled mass: 4,236 kg (9,338 lb). Specific impulse: 316 s. Specific impulse sea level: 220 s. Burn time: 266 s. Height: 22.20 m (72.80 ft). Diameter: 3.05 m (10.00 ft). Span: 4.90 m (16.00 ft).

Cost $ : 50.000 million.



Country: USA. Engines: LR105-7. Launch Vehicles: Atlas H, Atlas G Centaur, Atlas I. 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