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RP-1 kerosene fuel
- Atlas was a liquid propellant rocket burning RP-1 kerosene fuel with liquid oxygen in three engines configured in an unusual "stage-and-a-half" or "parallel staging" design: two outboard booster engines were jettisoned along with supporting structures during ascent, while the center sustainer engine, propellant tanks and other structural elements remained connected through propellant depletion and engine shutdown.
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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 ...
Jan 1, 2021 · The two booster engines shared a turbopump and gas generator. The verniers received propellants from the sustainer. This configuration was used on Atlas B and C test missiles. MA-2, produced from 1958 through 1962, consisted of two XLR89-5 booster engines, an LR105-5 sustainer, and two LR101 vernier engines. The two booster engines each had its ...
Oct 9, 2023 · In 1997 Lockheed Martin established an agreement with NPO Energomash, the leading Russian developer of liquid propellant rocket engines, to purchase engines for Atlas launch vehicles. The Russian American collaboration required to make these flights successful has surmounted significant challenges and withstood the test of time.
May 25, 2020 · Convair engineers developed a “balloon” which was its fuel tank, always kept under pressure with either propellant or nitrogen gas to provide the needed rigidity. At launch three engines would fire using RP-1 and LOX as fuel.
When designing the Atlas, he eliminated the rocket's exterior structure and depended instead on pressurized thin (0.020") welded stainless steel propellant tanks with very little additional structure to bear the huge loads associated with hypersonic flight ( video ).
ATLAS STAGE Size: 3.05-m Dia x 24.90-m Length Propellant: 156,400-kg Liquid Oxygen & RP-1 Propulsion: Rocketdyne MA-5A booster and sustainer engines SOLID ROCKET BOOSTERS Four Thiokol Castor IVA ...
The SM-65C Atlas, or Atlas C was a prototype of the Atlas missile. First flown on 24 December 1958, the Atlas C was the final development version of the Atlas rocket, prior to the operational Atlas D. [1] It was originally planned to be used as the first stage of the Atlas-Able rocket, but following an explosion during a static test on 24 ...
