Search results
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.
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 .
The modified Atlas LV-3B was used for the orbital element of Project Mercury, launching four crewed Mercury spacecraft into low Earth orbit. Atlas D launches were conducted from Cape Canaveral Air Force Station, at Launch Complexes 11, 12, 13 and 14, and Vandenberg AFB Launch Complex 576 .
The Atlas SLV-3, or SLV-3 Atlas was an American expendable launch system derived from the SM-65 Atlas / SM-65D Atlas missile. It was a member of the Atlas family of rockets. The Atlas SLV-3 was a stage and a half rocket, built as a standardized replacement for earlier Atlas launch systems, which had been derived from the various Atlas missiles. [1]
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).
Language links are at the top of the page across from the title.
Oct 25, 2022 · Atlas Centaur LV-3C Development History. Staff Tribble 21 Min Read. Last Updated: October 25, 2022. New Launchers – Angara. Atlas Centaur, the world’s first space launch vehicle with a liquid hydrogen-fueled stage, suffered through a troubled development phase that lasted from 1958 to 1966.
