Titan IIIA
In-activeLockheed Martin (LMT)
Sept. 1, 1964
Description
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.
Specifications
-
Stages
3 -
Length
42.0 m -
Diameter
3.05 m -
Fairing Diameter
3.05 m -
Launch Mass
161.0 T -
Thrust
1941.0 kN
Family
-
Name
Titan IIIA -
Family
― -
Variant
IIIA -
Alias
― -
Full Name
Titan IIIA
Payload Capacity
-
Launch Cost
― -
Low Earth Orbit
3100.0 kg -
Geostationary Transfer
Orbit
― -
Direct Geostationary
― -
Sun-Synchronous Capacity
―
Lockheed Martin
Commercial
None
LMT 1953Lockheed Martin's Space Division started in the production of missiles and later ICBM's in the 1950s. Their TITAN missile system was used for 12 Gemini spacecraft and the Voyager probes. They have worked largely in collaboration with NASA on many of their probes, landers, and spacecraft, and hope to play a key role in NASA's return to the moon in 2024.
Titan IIIA | LES 2
Lockheed Martin | United States of AmericaCape Canaveral SFS, FL, USA
Titan IIIA | LES 1
Lockheed Martin | United States of AmericaCape Canaveral SFS, FL, USA
Titan IIIA | Transtage 2
Lockheed Martin | United States of AmericaCape Canaveral SFS, FL, USA
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