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Saturn V-A

Saturn V-A was a proposed American orbital launch vehicle. It was studied by Marshall Space Flight Center in 1968. the Saturn V-A was identical to the Saturn INT-20, except it consisted of an ordinary S-IC first stage and S-IVB second stage. For deep-space missions, a Centaur third stage could also have been used.

Details

Details of Saturn V-A:

Gross mass: 2,478,120 kg (5,463,310 lb).

Payload: 60,000 kg (132,000 lb).

Height: 72.00 m (236.00 ft).

Diameter: 10.06 m (33.00 ft).

Thrust: 33,737.90 kN (7,584,582 lbf).

Apogee: 185 km (114 mi).

References

References

  1. (1968). "Saturn V Derivatives". [[SAE International]].
  2. "Saturn V-A".
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