Category:Titan IIIA

From Wikimedia Commons, the free media repository
Jump to navigation Jump to search
English: Titan IIIA - The Titan IIIA or Titan 3A was an American expendable launch system, launched four times in 1964 and 1965,[1] to test the Transtage upper stage which was intended for use on the larger Titan IIIC.
<nowiki>Titan IIIA; Титан-3A; Titan IIIA; Titan IIIA; Титан IIIA; Titan IIIA; 泰坦三A運載火箭; 大力神三A运载火箭; Titan IIIA; Titan 3A; טיטן 3A; 泰坦三A運載火箭; 大力神三A运载火箭; 泰坦三A運載火箭; Titan IIIA; タイタンIIIA; 泰坦三A运载火箭; Titan IIIA; model of Titan III launch vehicle; Titan 3A; SLV-5A; Titan IIIA; 泰坦IIIA運載火箭; 泰坦3A運載火箭; 大力神-3A运载火箭; 泰坦三A型運載火箭; 泰坦IIIA; 泰坦3A型火箭; 大力神IIIA火箭; 大力神IIIA运载火箭; 泰坦三A火箭; 泰坦3A; 泰坦三A; 泰坦三A號運載火箭; 大力神三A运载火箭; 大力神3A运载火箭; 泰坦IIIA火箭; 泰坦3A火箭; Titan 3A</nowiki>
Titan IIIA 
model of Titan III launch vehicle
Upload media
Instance of
  • rocket model
Subclass of
Country of origin
Has part(s)
Manufacturer
First flight
  • 1 September 1964
Service retirement
  • 6 May 1965
Mass
  • 161,730 kg (gross weight)
Diameter
  • 3.05 m
Height
  • 42 m
Cost
  • 30,740,000 United States dollar (1985)
Authority file
Edit infobox data on Wikidata

Subcategories

This category has the following 3 subcategories, out of 3 total.

Media in category "Titan IIIA"

This category contains only the following file.