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S-II - Ontify
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S-II
Second stage of the Saturn V rocket.
Wikipedia | S-II
Statements about
S-II
Part Of
Saturn V
Manufacturer
North American Aviation
Image
Schematic
Country of Origin
United States
Subclass Of
Liquid-Propellant Rocket
Mass
471,114 kilogram
493,536 kilogram
35,356 kilogram
40,143 kilogram
375,826 kilogram
72,001 kilogram
Height
24.84 metre
Diameter
Instance Of
10.06 metre
Rocket Stage
Nature of Statement
:
Minimum
Applies to Part
:
Apollo 8
Criterion Used
:
Launch Weight
Nature of Statement
:
Maximum
Applies to Part
:
Apollo 16
Criterion Used
:
Launch Weight
Nature of Statement
:
Minimum
Applies to Part
:
Apollo 13
Criterion Used
:
Dry Weight
Nature of Statement
:
Maximum
Applies to Part
:
Apollo 8
Criterion Used
:
Dry Weight
Nature of Statement
:
Average
Applies to Part
:
Liquid Oxygen
Nature of Statement
:
Average
Applies to Part
:
Liquid Hydrogen