Commercial Titan III Vehicle Overview
A complete overview of the Commercial Titan III launch vehicle, including launch stats, vehicle info and launch locations.
Basic Info
Name
Commercial Titan III
Family
Titan
Manufacturer
First Launch
1 Jan 1990
Successful Launches
4
Failed Launches
0
Rocket Info
Status
Inactive
Stages
2-3
Length
47.3 m
Diameter
3.05 m
Launch Mass
680 tons
Reusability
Not Reusable
Payload Info
LEO Capacity
14,742 kg
GTO Capacity
4,990 kg
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.
Launch Sites used by Commercial Titan III
Cape Canaveral Space Force Station
Historic U.S. military rocket launch site, pivotal in space exploration and national security.