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The S-II was the second stage of the Saturn V rocket. It was built by North American Aviation. Using liquid hydrogen (LH2) and liquid oxygen (LOX) it had five J-2 engines in a quincunx pattern. The second stage accelerated the Saturn V through the upper atmosphere with 1,000,000 pounds-force (4,400 kN) of thrust.
From Wikipedia
Specifications
General Characteristics
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- Wingspan 22.9ft (7.0m)
- Length 27.1ft (8.2m)
- Height 49.2ft (15.0m)
- Empty Weight 71,619lbs (32,486kg)
- Loaded Weight 92,247lbs (41,842kg)
Performance
- Power/Weight Ratio 2.192
- Wing Loading 53.1lbs/ft2 (259.5kg/m2)
- Wing Area 1,735.7ft2 (161.3m2)
- Drag Points 91571
Parts
- Number of Parts 1570
- Control Surfaces 0
- Performance Cost 2,647
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7,262 Zing2000Yet again... Just awesome9.0 years ago
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2,965 600548@THEaviator9.0 years ago
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2,965 600548@Zing20009.0 years ago
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2,965 600548@qwert13357 yes9.1 years ago
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18.4k TeusNice!9.1 years ago
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2,965 600548Thanks @ElijiTheGeat :)9.1 years ago
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13.9k ElijtheGeatpretty sweet9.1 years ago
