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Atlas V Growth Phase 3
Part of Atlas V Family
American orbital launch vehicle. Proposed Saturn-V class variant of the heavy-lift version of the Atlas V launch vehicle with five parallel 5-m-diameter wide-body Common Core Boosters (CCB), each with 1 or 2 RD-180 engines; a 7-m-diameter new LOx/LH2 stage; and a 7 m diameter payload fairing.

Status: Design 2003. Payload: 44,000 kg (97,000 lb). Thrust: 35,300.00 kN (7,935,700 lbf). Gross mass: 2,900,000 kg (6,300,000 lb). Height: 63.00 m (206.00 ft). Diameter: 5.00 m (16.40 ft). Span: 15.00 m (49.00 ft).

Payload: 44,000 kg (97,000 lb) to a earth escape.



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

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