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- Saturn_V-A abstract "American orbital launch vehicle. 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, although in random cases, a Centaur third stage would be fine for deep space missions.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).".
- Saturn_V-A wikiPageID "11097656".
- Saturn_V-A wikiPageRevisionID "560919689".
- Saturn_V-A hasPhotoCollection Saturn_V-A.
- Saturn_V-A subject Category:Saturn_(rocket_family).
- Saturn_V-A comment "American orbital launch vehicle. 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, although in random cases, a Centaur third stage would be fine for deep space missions.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).".
- Saturn_V-A label "Saturn V-A".
- Saturn_V-A label "Saturn V-A".
- Saturn_V-A sameAs Saturn_V-A.
- Saturn_V-A sameAs m.02q_y8w.
- Saturn_V-A sameAs Q3950835.
- Saturn_V-A sameAs Q3950835.
- Saturn_V-A wasDerivedFrom Saturn_V-A?oldid=560919689.
- Saturn_V-A isPrimaryTopicOf Saturn_V-A.