Saturn INT-12
From EverybodyWiki Bios & Wiki
| Function | Launch vehicle for Apollo |
|---|---|
| Country of origin | United States |
| Size | |
| Height | 167 feet (51 m) (w/o payload) |
| Diameter | 21.68 feet (6.61 m) |
| Mass | 3,327,280 pounds (1,509,230 kg) gross (to LEO) |
| Capacity | |
| Payload to LEO | 74,000 pounds (34,000 kg) |
| Associated rockets | |
| Family | Saturn |
| Launch history | |
| Status | Study, not developed |
| Launch sites | Kennedy Space Center |
Template:Infobox rocket/Stage
Template:Infobox rocket/StageTemplate:Infobox rocket/Stage | |
The Saturn INT-12 was an unflown member of the Saturn family of launch vehicles. It was conceptualized as a variant of the Saturn IB, with the S-IB first stage only having four engines instead of the usual eight, and four UA1205 solid rocket motors being attached to the side.
See also
References
- Bibliography
Encyclopedia Astronautica Saturn INT-12
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