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Atlas V Growth Phase 2
Part of Atlas V Family
American orbital launch vehicle. Proposed growth variant of the heavy-lift version of the Atlas V launch vehicle with three parallel 5-m-diameter wide-body Common Core Boosters (CCB), each with 1 or 2 RD-180 engines; a 5-m-diameter new LOx/LH2 stage with 2 or 4 engines with a total thrust of 180,000 kgf; and a 5 m diameter payload fairing.

Status: Design 2003. Payload: 29,000 kg (63,000 lb). Thrust: 22,940.00 kN (5,157,110 lbf). Gross mass: 1,800,000 kg (3,900,000 lb). Height: 63.00 m (206.00 ft). Diameter: 5.00 m (16.40 ft). Span: 15.00 m (49.00 ft).

Payload: 29,000 kg (63,000 lb) to a earth escape.



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

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