Encyclopedia Astronautica
Atlas V Growth Phase 3


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.

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

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

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Associated Countries
See also
  • Atlas V The Atlas V launch vehicle system was a completely new design that succeeded the earlier Atlas series. Atlas V vehicles were based on the 3.8-m (12.5-ft) diameter Common Core Booster (CCB) powered by a single Russian RD-180 engine. These could be clustered together, and complemented by a Centaur upper stage, and up to five solid rocket boosters, to achieve a wide range of performance. More...

Associated Manufacturers and Agencies
  • Martin American manufacturer of rockets, spacecraft, and rocket engines. Martin Marietta Astronautics Group (1956), Denver, CO, USA. More...

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