Atlas V Growth Phase 1

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 V Growth Phase 1

Part of Atlas V

American orbital launch vehicle. Proposed growth variant of the heavy-lift version of the Atlas V launch vehicle with three parallel 3.8-m-diameter Common Core Boosters (CCB), a 5-m-diameter wide body version of the Centaur upper stage with a single-engine, and a 5 m diameter payload fairing. Another variant would use a stretched wide body version of the Centaur upper stage with 2 or 4 motors, allowing payloads of up to 13,500 kg to be lofted to earth escape velocity.

Status: Design 2003. Payload: 12,000 kg (26,000 lb). Thrust: 11,470.00 kN (2,578,550 lbf). Gross mass: 960,000 kg (2,110,000 lb). Height: 60.00 m (196.00 ft). Diameter: 3.81 m (12.49 ft). Span: 11.50 m (37.70 ft).

Payload: 12,000 kg (26,000 lb) to a earth escape.

Family: orbital launch vehicle. Country: USA. Agency: Martin.

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