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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 .
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] .
- December 17, 1957; 65 years ago
- 1957–2010s (decade)
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. Launches were conducted from Launch Complex 36 at the Cape Canaveral Air Force Station (CCAFS) in Florida.
- 8 May 1962
- Expendable launch system
- 197
Atlas V [a] is an expendable launch system and the fifth major version in the Atlas launch vehicle family. It was originally designed by Lockheed Martin, now being operated by United Launch Alliance (ULA), a joint venture between Lockheed Martin and Boeing. It is used for DoD, NASA, and Commercial payloads.
Flight No.Date And Time (utc)TypeSerial No.10017 May 202422:16N22AV-085996 October 2023 18:06501AV-1049810 September 2023 12:47551AV-1029710 November 2022 09:49401AV-098- US$110–153 million in 2016
- 97, 401: 41, 411: 6, 421: 9, 431: 3, 501: 7, 511: 1, 521: 2, 531: 5, 541: 9, 551: 12, N22: 2
- 2 (3 with Star 48 upper stage)
- 21 August 2002, Hot Bird 6
The Atlas LV-3B, Atlas D Mercury Launch Vehicle or Mercury-Atlas Launch Vehicle, was a human-rated expendable launch system used as part of the United States Project Mercury to send astronauts into low Earth orbit.
SLV-3C was the standard Atlas-Centaur booster, without the tapered forward section to accommodate the smaller Agena stage. The Atlas Centaur effort started in 1958 at the Advanced Research Projects Agency.
