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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 ...
The first flight-ready Atlas, designated Atlas #4A, was received at Cape Canaveral in December, 1956. The foundation was thus laid for a plethora of Atlas missile and rocket launches which followed. Originating as the X-11, Atlas A was the name given to the first series of Atlas missiles delivered to Cape Canaveral for flight testing.
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Jan 1, 2021 · In its direction of the Navaho program, Wright Field insisted that it be fueled by JP-4, which was intended to give it more power per pound. Rocketdyne objected, because JP-4 production and purity standards were too loose to permit its use as a rocket fuel. Finally, a highly-refined version of JP-4 known as RP-1 (Rocket Propellant 1) was developed.
Apr 6, 2020 · 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 –. 2C12H26 + 37O2 → 24CO2 + 26H2O.
Booster for GX rocket. The Atlas V Common Core Booster was to have been used as the first stage of the joint US-Japanese GX rocket, which was scheduled to make its first flight in 2012. GX launches would have been from the Atlas V launch complex at Vandenberg Air Force Base, SLC-3E. However, the Japanese government decided to cancel the GX ...
Rocketdyne objected, because JP-4 production and purity standards were too loose to permit its use as a rocket fuel. Finally, a highly-refined version of JP-4 known as RP-1 (Rocket Propellant 1) was developed. LOX was retained as the oxidizer. This combination became the basis for a number of rocket engines.
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.
