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LGM-25C Titan II

Spacecraft and Launch Vehicles

The LGM-25C Titan II was a two-stage intercontinental ballistic missile developed by the Glenn L. Martin Company as the successor to its Titan I. It replaced the liquid oxygen and kerosene of the earlier missile with storable hydrazine-based hypergolic propellant, which cut the time needed to launch and allowed firing from a silo, and it carried the largest single warhead of any American ICBM. Its first flight was in March 1962 and it served in the United States nuclear deterrent from 1963 to 1987. Modified examples, designated Titan II GLV and Titan 23G, were adapted as medium-lift space launch vehicles that carried NASA's Gemini crewed capsules and satellites for the Air Force and NOAA, with launches from Vandenberg Air Force Base continuing until 2003.

Facts
Year
1962 1
Propulsion
Hydrazine 1
Engine Class
Rocket 1
Status
Retired from service 1
Comparison
Body Style
Launch vehicle 1
Connections

Ancestor Of

Titan IIIB, Vehicles
Source Titan IIIB (Wikipedia)

Exemplifies

Source LGM-25C Titan II (Wikipedia)

Of Make

Source LGM-25C Titan II (Wikipedia)
In the Other Atlases

Same As

Also in War and Military Atlas: the same subject.

Manufactured By

Also in Business Atlas: the manufacturer of this subject.

Source LGM-25C Titan II (Wikipedia)Lead, developer
Quote, Lead, developer
The Titan II was an intercontinental ballistic missile (ICBM) developed by the Glenn L. Martin Company from the earlier Titan I missile.

Originated In

Also in Geography Atlas: where this subject originated.

Source LGM-25C Titan II (Wikipedia)Titan II missile, warhead
Quote, Titan II missile, warhead
Titan II carried the largest single warhead of any American ICBM.
Sources
1. LGM-25C Titan II (Wikipedia)
  • Lead, space launch vehicle
    later adapted as a medium-lift space launch vehicle
  • Titan II missile, first flight
    The first flight of the Titan II was in March 1962
  • Service history
    The Titan II was in service from 1963 to 1987.
  • Titan II missile, propellant
    it used hydrazine-based hypergolic propellant
  • LGM-25C missile, engines
    two-stage, rocket engine powered vehicle
  • Lead, developer
    The Titan II was an intercontinental ballistic missile (ICBM) developed by the Glenn L. Martin Company from the earlier Titan I missile.
  • Titan II missile, warhead
    Titan II carried the largest single warhead of any American ICBM.
  • Exemplifies: Orbital Spaceflight, Lead, payloads to orbit
    to carry payloads to Earth orbit for the United States Air Force (USAF), National Aeronautics and Space Administration (NASA) and National Oceanic and Atmospheric Administration (NOAA)
View the Source
Titan IIIB (Wikipedia)
Ancestor Of: Titan IIIB, Lead
Quote, Ancestor Of: Titan IIIB, Lead
Titan IIIB was the collective name for a number of derivatives of the Titan II ICBM and Titan III launch vehicle
View the Source
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