Şablon:Infobox rocket stage/doc
Code
bıvurne{{Infobox rocket stage |name = S-II |image = ap6-MSFC-6758331.jpg |caption = The [[Apollo 6]] S-II stage during stacking operations in the [[Vehicle Assembly Building|VAB]] |manufacturer = [[North American Aviation|North American]] |country = USA |rockets = [[Saturn V]] (stage 2)<br>[[Saturn INT-21]] (stage 2) |height = 24.9 m |alt-height = 82 ft |diameter = 10 m |alt-diameter = 33 ft |mass = 480,900 kg |alt-mass = 1,060,000 lb |engines = 5 [[J-2 (rocket engine)|J-2]] engine |thrust = 5,115 kN |alt-thrust = 1,150,000 lbf |time = 367 seconds |fuel = [[Liquid oxygen|LOX]]/[[Liquid hydrogen|LH<sub>2</sub>]] }}
How it looks
bıvurneManufacturer | North American |
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Country of origin | USA |
Rockets |
Saturn V (stage 2) Saturn INT-21 (stage 2) |
Size | |
Height | 24.9 m (82 ft) |
Diameter | 10 m (33 ft) |
Mass | 480,900 kg (1,060,000 lb) |
Engine details | |
Engines | 5 J-2 engine |
Thrust | 5,115 kN (1,150,000 lbf) |
Burn time | 367 seconds |
Fuel | LOX/LH2 |
See also
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