S-IC

S-IC
The Apollo 10 S-IC stage is hoisted in the VAB for stacking
ManufacturerBoeing
Country of originUnited States
Used onSaturn V
General characteristics
Height42 m (138 ft)
Diameter10 m (33 ft)
Gross mass5,030,000 lb (2,280,000 kg)
Empty mass290,000 lb (130,000 kg)
Launch history
StatusRetired
Total launches13
Successes
(stage only)
13
First flightNovember 9, 1967 (Apollo 4)
Last flightMay 14, 1973 (Skylab 1)
Engine details
Powered by5 F-1
Maximum thrust34,500 kN (7,750,000 lbf) sea level[1]
Specific impulse263 seconds (2.58 km/s)
Burn time150 s
PropellantRP-1/LOX

The S-IC (pronounced S-one-C[2][3]) was the first stage of the American Saturn V rocket. The S-IC stage was manufactured by the Boeing Company. Like the first stages of most rockets, most of its mass of more than 2,000 t (4,400,000 lb) at launch was propellant, in this case RP-1 rocket fuel and liquid oxygen (LOX) oxidizer. It was 42 m (138 ft) tall and 10 m (33 ft) in diameter. The stage provided 34,500 kN (7,750,000 lbf)[1] of thrust at sea level to get the rocket through the first 61 km (38 mi) of ascent. The stage had five F-1 engines in a quincunx arrangement. The center engine was fixed in position, while the four outer engines could be hydraulically gimballed to control the rocket.

  1. ^ a b Thorne, Muriel, ed. (May 1983). NASA, The First 25 Years: 1958-1983 (PDF). Washington, D.C.: National Aeronautics and Space Administration. p. 69.
  2. ^ Murray, Charles A.; Cox, Catherine Bly (Jul 1989). Apollo, the race to the moon. Simon and Schuster. p. 54. ISBN 9780671611019.
  3. ^ Woods, W. David (2011-08-08). How Apollo Flew to the Moon. Springer Science & Business Media. p. 24. ISBN 9781441971791.

© MMXXIII Rich X Search. We shall prevail. All rights reserved. Rich X Search