మూస:Infobox rocket stage
Code
[మార్చు]{{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
|propmass = 444,000 kg
|alt-propmass = 970,000 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
[మార్చు] The Apollo 6 S-II stage during stacking operations in the VAB | |
| Manufacturer | North American |
|---|---|
| Country of origin | USA |
| Used on | Saturn V (stage 2) Saturn INT-21 (stage 2) |
| General Characteristics | |
| Height | 24.9 m (82 ft) |
| Diameter | 10 m (33 ft) |
| Mass | 480,900 kg (1,060,000 lb) |
| Propellant mass | 444,000 kg (970,000 lb) |
| Engine details | |
| Engines | 5 J-2 engine |
| Thrust | 5,115 kN |
| Burn time | 367 seconds |
| Fuel | LOX/LH2 |
See also
[మార్చు]| Generic |  | |
|---|---|---|
| Human spaceflight | ||
| Rocketry | ||
| Other | ||