Category:Saturn S-IB

**S-IB**
	first stage of the Saturn IB rocket
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Instance of	rocket stage;
Subclass of	liquid-propellant rocket;
Part of	Saturn IB;
Country of origin	United States of America;
Manufacturer	Stellantis North America;
Location of creation	Michoud Assembly Facility;
Powered by	H-1 (8, liquid oxygen, RP-1);
Mass	450,831 kg (launch weight, Apollo 7); 38,342 kg (Apollo 7, dry weight); 286,353 kg (Apollo 7, liquid oxygen); 125,600 kg (Apollo 7, RP-1);
Diameter	6.6 m (top); 6.55 m (bottom);
Height	24.44 m;
Authority file
	Q11242284;
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First stage of the Saturn IB rocket

Subcategories

This category has the following 9 subcategories, out of 9 total.

The following 7 files are in this category, out of 7 total.