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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 ...
- December 17, 1957; 65 years ago
- 1957–2010s (decade)
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.
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 ...
Aug 21, 2002 · The first stage can produce a liftoff thrust of 933,406 pounds. The first stage can be augmented by up to five Aerojet strap-on solid rocket boosters. 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.
Aug 3, 2016 · The 1954 design for the Atlas as contracted for by the Air Force used three main engines to power a 110 metric ton rocket able to send a 1400 kg nuclear warhead over a 10,200 km range. CEP was 3700 m.
4 days ago · The Thor missile force was withdrawn in 1963. Propelled by liquid oxygen and kerosene, the basic rocket was 65 feet (19.8 m) in length, with a body diameter of 8 feet (2.4 m), weight at firing of 110,000 pounds (49,900 kg), and speed at burnout of 7,670 to 11,505 miles (12,300 to 18,500 km) per hour.
Atlas Rockets Atlas Rockets Overview 50 years of Rocketry. Atlas was the name given to Americas first operational ICBM. Although its career as a nuclear armed missile was short-lived, the Atlas has evolved into one of the worlds premier satellite launchers. Over the last 50 years, more than 600 Atlas rockets have flown. Stage and a Half ...
