Lockheed Martin

Commercial Titan III

III

Commercial Titan III
Retired

Overview

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The Commercial Titan III, also known as CT-3 or CT-III, was an American expendable launch system, developed by Martin Marietta during the late 1980s and flown four times during the early 1990s. It was derived from the Titan 34D, and was originally proposed as a medium-lift expendable launch system for the US Air Force, who selected the Delta II instead. Development was continued as a commercial launch system, and the first rocket flew in 1990. Due to higher costs than contemporary rockets such as the Ariane 4, orders were not forthcoming, and the CT-3 was retired in 1992.

Manufacturer

Lockheed Martin

Variant

III

Alias

N/A

Maiden Flight

January 1, 1990

Technical Specifications

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47.3 m

Length

3.05 m

Diameter

1 t

Launch Mass

Liftoff Thrust

14742 kg

LEO Capacity

4990 kg

GTO Capacity

Launch Record

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4

Total Launches

4

Successful

0

Failed

100.0%

Success Rate

0

Attempted Landings

0

Successful Landings

0

Failed Landings

0

Consecutive Successes

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