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The Atlas-Centaur was a United States 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 (CCAFS) in Florida. [1] [2]
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.
American orbital launch vehicle. Version with basic Centaur upper stage. AKA: LV-3C. Payload: 1,700 kg (3,700 lb). Thrust: 173,843.00 kN (39,081,461 lbf). Gross mass: 136,124 kg (300,102 lb). Height: 33.00 m (108.00 ft).
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SM-65D Atlas. Atlas LV-3C. 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]
SLV-3B was a one-off Atlas used to launch the first OAO satellite, which consisted of the SLV-3C Atlas with the Agena and payload enclosed in a full-width fairing. The configuration was launched once, on August 4, 1966, from Cape Canaveral Launch Complex 12 to deliver the OAO satellite to orbit.
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Mar 1, 2013 · Atlas-Centaur’s initial interplanetary missions included the Mariner 6 and 7 (1969) flybys of Mars; Mariner 9 (1971) to Mars, which was the first spacecraft to orbit another planet; and Pioneer 10 (1972), which was the first spacecraft to visit Jupiter and the first to exit the solar system.
