Titan 402A IUS
In-activeLockheed Martin (LMT)
June 14, 1989
Description
Titan IV was a family of heavy-lift space launch vehicles developed by Martin Marietta and operated by the United States Air Force from 1989 to 2005.
Specifications
-
Stages
3 -
Length
54.0 m -
Diameter
3.05 m -
Fairing Diameter
3.05 m -
Launch Mass
910.0 T -
Thrust
14200.0 kN
Family
-
Name
Titan 402A IUS -
Family
― -
Variant
402A IUS -
Alias
― -
Full Name
Titan 402A IUS
Payload Capacity
-
Launch Cost
― -
Low Earth Orbit
21680.0 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 402A IUS | DSP 17
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Titan 402A IUS | DSP 15
Lockheed Martin | United States of AmericaCape Canaveral SFS, FL, USA
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