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I read the reference and it did not say 10 tons which is HIGHLY implausible.
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|country = United States
|country = United States
|rockets = [[Saturn I]] (stage 2)
|rockets = [[Saturn I]] (stage 2)
|height = 12.19 m
|height = {{convert|12.19|m|ft|abbr=on}}
|diameter = {{convert|5.49|m|ft|abbr=on}}
|alt-height = 40 ft
|diameter = 5.49 m
|alt-diameter = 18 ft
|mass =
|mass =
|alt-mass =
|engines = 6 [[RL-10 (rocket engine)|RL-10]] engines
|engines = 6 [[RL-10 (rocket engine)|RL-10]] engines
|thrust = 400 kN
|thrust = {{convert|400|kN|lbf|abbr=on}}
|alt-thrust = 90,000 lbf
|time = ~410 seconds
|time = ~410 seconds
|fuel = [[LOX]]/[[LH2]]
|fuel = [[LOX]]/[[LH2]]

Revision as of 23:16, 15 February 2017

S-IV
Schematics of the S-IV
ManufacturerDouglas Aircraft Company
Country of originUnited States
Used onSaturn I (stage 2)
General characteristics
Height12.19 m (40.0 ft)
Diameter5.49 m (18.0 ft)
S-IV
Powered by6 RL-10 engines
Maximum thrust400 kN (90,000 lbf)
Burn time~410 seconds
PropellantLOX/LH2

The S-IV was the second stage of the Saturn I rocket used by NASA for early flights in the Apollo program.

The S-IV was manufactured by the Douglas Aircraft Company and later modified by them to the S-IVB, a similar but distinct stage used on the Saturn IB and Saturn V rockets.[1]

The S-IV stage was a large LOX/LH2-fueled rocket stage used for the early test flights of the Saturn I rocket. It formed the second stage of the Saturn I and was powered by a cluster of six RL-10A-3 engines. Each one of the engines supplied 66.7 kilonewtons (15,000 lbf) of thrust for a total of about 400 kilonewtons (90,000 lbf). The cryogenic LH2 (liquid hydrogen) and LOX (liquid oxygen) tanks were separated by a common bulkhead. The forward bulkhead of the LOX tank formed the aft bulkhead of the LH2 tank. This saved up to 20% of structural weight.[2][3]

References

  • Bilstein, Roger E. (1999). "6". Stages to Saturn: A Technological History of the Apollo/Saturn Launch. DIANE Publishing. Retrieved 2010-05-04.
  • NASA (April 1975). "Apollo Program Summary Report (Large file)" (PDF).