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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 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 ...
Propellant. RP-1 / LOX. [ edit on Wikidata] The SM-65F Atlas, or Atlas-F, was the final operational variant of the Atlas missile, only differing from the Atlas E in the launch facility and guidance package used. It first flew on 8 August 1961, [1] and was deployed as an operational ICBM between 1961 and 1966.
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.
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.
SM-65A Atlas. The Convair SM-65A Atlas, or Atlas A, was the first full-scale prototype of the Atlas missile, which first flew on 11 June 1957. Unlike later versions of the Atlas missile, the Atlas A did not feature the stage and a half design. Instead, the booster engines were fixed in place, and the sustainer engine was omitted.
The vernier engines, a trademark of Atlas vehicles, were designed to control the roll of the missile and trim its final flight velocity. The booster and vernier engines were all fed by liquid oxygen/RP-1 (kerosene) liquid propellant, and all engines were ignited at liftoff.
May 7, 2024 · The Atlas-Centaur rocket combined an Atlas first stage, which burned kerosene fuel, with a Centaur second stage, fueled with liquid hydrogen; it was the first rocket to use liquid hydrogen as fuel. Further versions of the Atlas included the SLV-3, a standardized launch vehicle designed for both military and civilian use that operated in various ...
