Rocket Propellant

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High Quality Content by WIKIPEDIA articles! Rocket propellant is mass that is stored in some form of propellant tank, prior to being used as the propulsive mass that is ejected from a rocket engine in the form of a fluid jet to produce thrust. A fuel propellant is often burned with an oxidizer propellant to produce large volumes of very hot gas. These gases expand and push on a nozzle, which accelerates them until they rush out of the back of the rocket at extremely high speed, making thrust. Sometimes the propellant is not burned, but can be externally heated for more performance. For smaller attitude control thrusters, a compressed gas escapes the spacecraft through a propelling nozzle. Chemical rocket propellants are most commonly used, which undergo exothermic chemical reactions which produce hot gas which is used by a rocket for propulsive purposes.

Weitere Informationen

  • Allgemeine Informationen
    • GTIN 09786130559328
    • Herausgeber Betascript Publishing
    • Anzahl Seiten 152
    • Genre Baum- und Umwelttechnik
    • Editor Lambert M. Surhone, Miriam T. Timpledon, Susan F. Marseken
    • EAN 9786130559328
    • Format Fachbuch
    • Titel Rocket Propellant

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