Titan 402A IUS

In-active

Lockheed 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 1953

Lockheed 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.

Previous Flights

flew on three previous launch(es).

Titan 402A IUS | DSP 17

Lockheed Martin | United States of America
Cape Canaveral SFS, FL, USA
Dec. 22, 1994, 10:19 p.m.
Status: Launch Successful
Mission:

Early warning satellite

Geostationary Orbit
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Titan 402A IUS | DSP 15

Lockheed Martin | United States of America
Cape Canaveral SFS, FL, USA
Nov. 13, 1990, 12:37 a.m.
Status: Launch Successful
Mission:

Early warning satellite

Geostationary Orbit
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Titan 402A IUS | DSP 14

Lockheed Martin | United States of America
Cape Canaveral SFS, FL, USA
June 14, 1989, 1:18 p.m.
Status: Launch Successful
Mission:

Early warning satellite

Geostationary Orbit
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