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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)
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Nov 17, 2022 · Initially designed as an intercontinental ballistic missile (ICBM) capable of deploying a nuclear weapon, the Atlas rocket had a powerful enough engine to la...
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 –
Jan 1, 2021 · Two LR101 vernier engines provided pitch and roll control for the Atlas and Mercury-Atlas. The were fed propellant from the sustainer engine turbopump; each produced about 1,000 lbT for as long as the sustainer engine operated. The gimbaled thrust chamber was was attached to the missile via a welded tubular engine mount. Each assembly weighed ...
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 ).