Titan II

Titan2 The Titan II vehicles are decommissioned intercontinental ballistic missiles that have been refurbished and equipped with hardware required for use as space launch vehicles. The Martin Marietta Astronautics Group was awarded a contract in January 1986 to refurbish, integrate, and launch fourteen Titan II ICBMs for government space launch requirements. These modifications allow for launches of medium-class payloads to polar orbit.

The Titan family was established in October 1955, when the U.S. Air Force awarded the then Martin Company a contract to build an intercontinental ballistic missile (ICBM). It became known as the Titan I, the nation’s first two-stage ICBMs and first underground silo-based ICBM. Over 140 Titan II ICBMs, once the vanguard of America’s strategic deterrent force, were built. Titan IIs also were flown in NASA’s Gemini manned space program in the mid-1960s.
Tasks involved in converting the Titan II ICBMs into space launch vehicles include modifying the forward structure of the second stage to accommodate payload; manufacturing a new 10-foot diameter payload fairing with variable lengths plus payload adapters; refurbishing the Titan’s liquid rocket engines; upgrading the inertial guidance system; developing command, destruct and telemetry systems; modifying Vandenberg Air Force Base, Calif., Space Launch Complex-4 West to conduct the launches; and performing payload integration.

The Air Force successfully launched the first Titan II space launch vehicle from Vandenberg on Sept. 5, 1988.

The Titan II space launch vehicle is a two-stage liquid fueled booster, designed to provide a small-to-medium weight class capability. It is able to lift approximately 4,200 pounds into a polar low-Earth circular orbit.

Deactivation of the Titan II ICBM system began in July 1982 and was completed in June 1987. Deactivated missiles are in storage at Davis-Monthan Air Force Base, Ariz.

Specifications

Launch site:

First stage:



Second stage:



Guidance:


Payload fairing:




Liquid rocket:

Engine:

Vandenberg Air Force Base, Calif.

Length:
Diameter:
Engine Thrust:

Length:
Diameter:
Engine Thrust:

Inertial with Digital Computer
Subcontractor:

Diameter:
Lengths:
Skin & Stringer Construction--
Subcontractor--

Refurbished Titan II ICBM Engines

Subcontractor--



70 feet
10 feet
474,000 pounds (vacuum)

24 feet
10 feet
100,000 pounds (vacuum)


Delco Electronics

10 feet
20 feet
Tri Sector Design
McDonnell Douglas



Aerojet Techsystems Co.

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(Current as of March 1997)

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