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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 〔() Saturn V-A〕 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 == 抄文引用元・出典: フリー百科事典『 ウィキペディア(Wikipedia)』 ■ウィキペディアで「Saturn V-A」の詳細全文を読む スポンサード リンク
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