Titan 34D IUS
In-activeLockheed Martin (LMT)
Oct. 30, 1982
Description
The Titan 34D was a United States expendable launch vehicle used to launch a number of satellites for military applications.
Specifications
-
Stages
2 -
Length
52.4 m -
Diameter
3.05 m -
Fairing Diameter
3.05 m -
Launch Mass
725 T -
Thrust
11279 kN
Family
-
Name
Titan 34D IUS -
Family
― -
Variant
34D IUS -
Alias
― -
Full Name
Titan 34D IUS
Payload Capacity
-
Launch Cost
― -
Low Earth Orbit
― -
Geostationary Transfer
Orbit
5000 kg -
Direct Geostationary
1900 kg -
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.
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