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S-IC

Saturn S-IC

First stage of the Saturn V rocket.

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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
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