Category:Titan IIIA

**Titan IIIA**
	model of Titan III launch vehicle
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Instance of	rocket model;
Subclass of	Titan III;
Country of origin	United States of America;
Has part(s)	Titan 3A-1 (1); Titan 3A-2 (2); Transtage (3);
Manufacturer	Martin Marietta;
First flight	1 September 1964;
Service retirement	6 May 1965;
Mass	161,730 kg (gross weight);
Diameter	3.05 m;
Height	42 m;
Capital cost	30,740,000 United States dollar (1985);
Authority file
	Q1187393;
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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.