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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 ...
- December 17, 1957; 65 years ago
- 1957–2010s (decade)
Booster for GX rocket. The Atlas V Common Core Booster was to have been used as the first stage of the joint US-Japanese GX rocket, which was scheduled to make its first flight in 2012. GX launches would have been from the Atlas V launch complex at Vandenberg Air Force Base, SLC-3E. However, the Japanese government decided to cancel the GX ...
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
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Jan 1, 2021 · Atlas E (SM-65E) was an improved version of the Atlas D. Its MA-3 booster engines each had a turbopump rather than the single turbopump for both booster engines that Atlas D had used. Atlas E also had a new inertial guidance system that did not require the radio link of Atlas D. It first flew on 11 Oct 1960. A total of 28 were deployed at 4 ...
May 25, 2020 · The Atlas was essentially a highly evolved version of the German V-2 missile, which Germany had used against the Allies during the waning years of World War II. Like the V-2, the Atlas was powered by rocket engines that burned a mixture of liquid fuel and oxidizer. But while the V-2 had an effective range of only a few hundred miles, the Atlas ...
The 1-1/2 Stage USSRC NASA Atlas. The boat tail and outboard booster engines are jettisoned after the initial boost phase, leaving the sustainer and verniers to run for the remainder of the boost. Rocketdyne introduced five key innovations when developing the Navaho Phase II and III propulsion systems, which led to Atlas/Jupiter/Thor propulsion.
Aug 21, 2002 · Each booster can produce a thrust of 285,500 pounds. The Atlas V second stage is comprised of either a one-engine or two-engine RL-10A Centaur upper stage. The Centaur burns a combination of liquid hydrogen and liquid oxygen. The one-engine Centaur can produce a thrust of 22,290 pounds. The two-engine Centaur can produce a thrust of 41,592 pounds.
The first flight-ready Atlas, designated Atlas #4A, was received at Cape Canaveral in December, 1956. The foundation was thus laid for a plethora of Atlas missile and rocket launches which followed. Originating as the X-11, Atlas A was the name given to the first series of Atlas missiles delivered to Cape Canaveral for flight testing.
