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Titan · Lockheed Martin

Titan IIIA

retired
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Specifications

Status
retired
Height
42 m
Diameter
3.05 m
Mass
161,000 kg
Stages
3
Payload to LEO
3,100 kg
First flight
1964-09-01
Total launches
4
Success / Fail
3 / 1

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. The Transtage was mounted atop two core stages derived from the Titan II. The Titan IIIA was also used as the core of the Titan IIIC.

Payloads it launched · 3

LCS 1
MEO
LES-2
MEO
LES-1
MEO