Saturn V-A

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 ^[1] 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

↑ Saturn V-A

Saturn launch vehicle family

Early proposals	Juno V Saturn A-1 A-2 B-1

"C" series	Saturn C-1 C-2 C-3 C-4 C-5 C-5N C-8

Saturn I series	Saturn I IB IB-CE IB-A IB-B IB-C IB-D INT-05 INT-11 INT-12 INT-13 INT-14 INT-15 INT-16 INT-27 LCB

Saturn II series	Saturn II INT-17 INT-18 INT-19

Saturn V series	Saturn V MLV V ELV INT-20 INT-21 INT-23 INT-24 INT-25 Saturn-Shuttle Saturn V-3 V-A V-B V-C V-D V-Centaur Jarvis

This article is issued from Wikipedia - version of the Friday, June 21, 2013. The text is available under the Creative Commons Attribution/Share Alike but additional terms may apply for the media files.