28,900 lb (13,100 kg) into a low Earth orbit with 28 degrees inclination. Up to 6,600 lb (3,000 kg) into a geosynchronous transfer orbit when launched from Cape Canaveral Air Force Station, FL. Maximum takeoff weight: 626,190 kg Cost: Date deployed: June 1965. Launch sites: Cape Canaveral Air Force Station, FL., and Vandenberg Air Force Base, CA. Launch history References External links Titan III: Research and Development for Today And Tomorrow Titan3C Titan III & variations Future Space Booster Requirements - January–February 1969 Air University Review 1971 in spaceflight 1973 in spaceflight 1974 in spaceflight Lockheed Martin Titan (rocket family) Military equipment introduced in the 1960s