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Atlas-Centaur AC-27 at Launch Complex 36A in February 1972 prior to launching Pioneer 10. Initially, a modified Atlas D designated LV-3C was used as the first stage. This was quickly replaced by SLV-3C, and later the SLV-3D, both derived from the standard Atlas SLV-3 rocket.
- 8 May 1962
- Expendable launch system
- 197
Variants. SM-65 Atlas. 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]
Model NameFirst LaunchLast LaunchTotal Launches195919603Atlas LV-3A19601968491959196391964196851- December 17, 1957; 65 years ago
- 1957–2010s (decade)
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The Atlas LV-3B was a human-rated expendable launch system used as part of the United States Project Mercury to send astronauts into low Earth orbit. Manufactured by American aircraft manufacturing company Convair, it was derived from the SM-65D Atlas missile, and was a member of the Atlas family of rockets. [2]
- 29 July 1960
- 9
- 1½
Atlas LV. Atlas LV-3C s/n AC-3 / Centaur D s/n 135D - 1964-06-30. 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).
First Launch: 1962-05-08. Last Launch: 1965-03-02. Number: 5 . Payload: 1,700 kg (3,700 lb). Thrust: 1,704.82 kN (383,259 lbf). Gross mass: 136,124 kg (300,102 lb). Height: 33.00 m (108.00 ft). Diameter: 3.05 m (10.00 ft). LEO Payload: 3,630 kg (8,000 lb) to a 185 km orbit. Payload: 2,255 kg (4,971 lb) to a GTO.
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.
Aug 8, 2016 · Last Launch: 1972-08-21. Number: 17 . Payload: 1,800 kg (3,900 lb). Thrust: 1,939.29 kN (435,970 lbf). Gross mass: 148,404 kg (327,174 lb). Height: 38.00 m (124.00 ft). Diameter: 3.05 m (10.00 ft). Apogee: 400,000 km (240,000 mi). LEO Payload: 1,800 kg (3,900 lb). Payload: 1,800 kg (3,900 lb) to a GTO. LEO Payload: 1,900 kg (4,100 lb).
