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Last flight. 31 August 2004. [ edit on Wikidata] The Atlas-Centaur was a United States expendable launch vehicle derived from the SM-65 Atlas D missile. The vehicle featured a Centaur upper stage, the first such stage to use high-performance liquid hydrogen as fuel.
Dec 7, 1991 · Classification: Space Launch Vehicle. Length: 149 feet, 7 inches (with medium fairing) Length: 155 feet, 10 inches (with large fairing) Diameter: 10 feet. Date of First Cape Canaveral Launch: December 7, 1991. Date of Final Cape Canaveral Launch: July 25, 1996. Number of Cape Canaveral Launches: 9. The Atlas II-Centaur was developed in 1989 ...
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May 24, 2000 · Atlas IIIA-Centaur Launch, Photo Courtesy Lockheed-Martin. Classification: Space Launch Vehicle. Length: 170 feet, 2 inches. Diameter: 10 feet. Date of First Cape Canaveral Launch: May 24, 2000. Date of Final Cape Canaveral Launch: March 13, 2004. Number of Cape Canaveral Launches: 2. In November, 1995 Lockheed-Martin approved plans for a new ...
Atlas IIIA. Atlas V. Atlas is a family of US missiles and space launch vehicles that originated with the SM-65 Atlas. The Atlas intercontinental ballistic missile (ICBM) program was initiated in the late 1950s under the Convair Division of General Dynamics. [2] Atlas was a liquid propellant rocket burning RP-1 kerosene fuel with liquid oxygen ...
Model NameFirst LaunchLast LaunchTotal Launches195919603Atlas LV-3A19601968491959196391964196851Jul 25, 1990 · By Cliff Lethbridge. Atlas-Centaur 1966 Launch, Photo Courtesy NASA. Classification: Space Launch Vehicle. Length: 131 feet. Diameter: 10 feet. Date of First Cape Canaveral Launch: April 7, 1966. Date of Final Cape Canaveral Launch: July 25, 1990. Number of Cape Canaveral Launches: 63. Introduced in 1966, this improved version of the 1962 Atlas ...
The Atlas-Centaur was a US expendable launch vehicle derived from the SM-65 Atlas D missile. Launches were conducted from Launch Complex 36 at the Cape Canaveral Air Force Station in Florida. Specifications
The first attempt to launch an Atlas/Centaur from the Atlantic Missile Range was unsuccessful when the Centaur stage blew up at T+55 seconds due to a second stage structural failure. Despite this failure, the launch marked the first U.S. use of a space vehicle fueled by a liquid hydrogen engine. First Centaur flight (unsuccessful).
