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Titan IIIA

Titan familyLockheed MartinRetired

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.

Titan IIIA vehicle

Specifications

Thrust
1,941 kN
Height
42 m
Diameter
3.05 m
Launch mass
161 t
Stages
3
LEO capacity
3,100 kg

Specifications from Launch Library. Figures the operator has not published are omitted.

Flight record

4flightswith a definitive outcome
75%success rate3 of 4
3success streakcurrent

Counted from padside's own launch record, the same basis as the stats page.

Flights

4 of 4