Titan (IIIE) Centaur Launch Vehicle
Contractors: Martin Marietta, NASA
Year of Manufacture: 1974
Length: 160.0 ft Maximum Diameter: 10.0 ft Total weight: 1,411,200 lb
Stages:
Supplementary Engines: Solid fuel, 2,498,000 Pounds thrust.
Stage 1: Nitrogen Tetroxide/Aerozine 50 fuel, 530,000 Pounds thrust.
Stage 2: Nitrogen Tetroxide/Aerozine 50 fuel. 101,000 Pounds thrust.
Stage 3: Liquid Oxygen/ Liquid Hydrogen fuel, 30,000 Pounds thrust.
All data extracted from the Encyclopedia of U.S. Spacecraft by Bill Yenne, published by Bison Books LTD