Category:Saturn V

**Saturn V**
	American human-rated launch vehicle
	Upload media
	Wikipedia
Instance of	rocket model;
Subclass of	Saturn; super heavy-lift launch vehicle;
Country of origin	United States of America;
Has part(s)	S-IC; S-II; S-IVB; Saturn IB/V Instrument Unit;
Start point	Kennedy Space Center Launch Complex 39;
Manufacturer	Boeing (S-IC); North American Aviation (S-II); Douglas (S-IVB); IBM (Saturn IB/V Instrument Unit);
First flight	9 November 1967;
Service retirement	14 May 1973;
Significant event	maiden flight (Apollo 4, unmanned spaceflight, 1967); maiden flight (human spaceflight, Apollo 8, 1968); last flight (Skylab 1, 1973);
Mass	2,822,171 kg (minimum, launch weight, Apollo 8); 2,965,241 kg (maximum, launch weight, Apollo 16); 238,229 kg (minimum, dry weight, Apollo 13); 245,819 kg (maximum, dry weight, Apollo 8); 1,955,691 kg (average, liquid oxygen); 736,079 kg (average, rocket propellant);
Diameter	10.06 m;
Height	110.65 m (Apollo Command and Service Module);
Authority file
	Q54363;
	Reasonator; Scholia; PetScan; statistics; WikiMap; Locator tool; KML file; Search depicted;

Subcategories

This category has the following 25 subcategories, out of 25 total.

Apollo 4‎ (7 C, 1 P, 25 F)
Apollo 6‎ (8 C, 10 F)
Apollo 8‎ (14 C, 1 P, 34 F)
Apollo 9‎ (14 C, 1 P, 40 F)
Apollo 10‎ (12 C, 1 P, 84 F)
Apollo 11‎ (33 C, 2 P, 469 F)
Apollo 12‎ (22 C, 1 P, 109 F)
Apollo 13‎ (21 C, 1 P, 72 F)
Apollo 14‎ (23 C, 1 P, 208 F)
Apollo 15‎ (21 C, 1 P, 125 F)
Apollo 16‎ (18 C, 1 P, 128 F)
Apollo 17‎ (22 C, 1 P, 304 F)
Skylab 1‎ (2 C, 7 F)

The following 18 files are in this category, out of 18 total.