Titan III
In-activeLockheed Martin (LMT)
Feb. 11, 1974
Description
Specifications
-
Minimum Stage
3 -
Max Stage
4 -
Length
48.8 m -
Diameter
3.05 m -
Fairing Diameter
― -
Launch Mass
632.0 T -
Thrust
12991.0 kN
Family
-
Name
Titan III -
Family
― -
Variant
E -
Alias
― -
Full Name
Titan IIIE
Payload Capacity
-
Launch Cost
― -
Low Earth Orbit
15400.0 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.
Flight Record
No spaceflights found for .
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