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S-IC
Saturn S-IC
First stage of the Saturn V rocket.
Wikipedia | S-IC
Statements about
S-IC
Part Of
Saturn V
Manufacturer
Boeing
Country of Origin
United States
Image
Schematic
Subclass Of
Liquid-Propellant Rocket
Mass
2,175,939 kilogram
Nature of Statement
:
Minimum
Applies to Part
:
Apollo 8
Criterion Used
:
Launch Weight
2,288,088 kilogram
Nature of Statement
:
Maximum
Applies to Part
:
Apollo 16
Criterion Used
:
Launch Weight
129,822 kilogram
Nature of Statement
:
Minimum
Applies to Part
:
Apollo 15
Criterion Used
:
Dry Weight
138,451 kilogram
Nature of Statement
:
Maximum
Applies to Part
:
Apollo 8
Criterion Used
:
Dry Weight
1,492,464 kilogram
Nature of Statement
:
Average
Applies to Part
:
Liquid Oxygen
644,296 kilogram
Nature of Statement
:
Average
Applies to Part
:
RP-1
Height
42.07 metre
Diameter
10.06 metre
Instance Of
Rocket Stage