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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 ...
- December 17, 1957; 65 years ago
- 1957–2010s (decade)
Jan 7, 2024 · Atlas Rocket. Atlas launchers are a family of non-reusable launch vehicles. The first rocket used during the Mercury projects was the Atlas LV-38, originally ideated as an intercontinental ballistic missile (ICBM) equipped with a nuclear warhead, after it was converted for use in space manned mission due to his high payload capacity and ...
Apr 6, 2020 · Used in: Space Shuttle booster stages. Liquid Propellants: These are the most commonly used propellants today. The common subtypes are: – a. Liquid oxygen (LOX) and highly refined kerosene (RP-1). Used for the first stages of the Saturn V, Atlas V, and Falcon 9. The equation for the corresponding chemical reaction will be as follows –
The Agena, used first as an upper stage on Thor-Agena rockets was adapted for use on Atlas rockets. Several Agena models were used as the program progressed, including the Agena-A, Agena-B, and Agena-D stages. Many space probes were launched on Atlas-Agena rockets.
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 ...
The combined Atlas- Agena rocket, featuring an Atlas booster coupled with an Agena upper stage, was used for launching lunar and planetary probes as well as Earth-orbiting satellites, such as Seasat, where the Agena stage was also the spacecraft.
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.
