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  1. Solid-propellant rocket - Wikipedia

    • A solid-propellant rocket or solid rocket is a rocket with a rocket engine that uses solid propellants (fuel/oxidizer). The earliest rockets were solid-fuel rockets powered by gunpowder; The inception of gunpowder rockets in warfare can be credited to the ancient Chinese, and in the 13th century, the Mongols played a pivotal role in facilitating their westward adoption… See more

    Basic concepts

    A simple solid rocket motor consists of a casing, nozzle, grain (propellant charge), and igniter.
    The solid grain mass burns in a predictable fashion to produce exhaust gases, the flow of which is … See more

    History

    The medieval Song dynasty Chinese invented a very primitive form of solid-propellant rocket. Illustrations and descriptions in the 14th century Chinese military treatise Huolongjing by the Ming dynasty mil… See more

     
  1. In a solid rocket, the fuel and oxidizer are mixed together into a solid propellant which is packed into a solid cylinder. A hole through the cylinder serves as a combustion chamber. When the mixture is ignited, combustion takes place on the surface of the propellant. A flame front is generated which burns into the mixture.
    www.grc.nasa.gov/WWW/k-12/airplane/srockth.html
    www.grc.nasa.gov/WWW/k-12/airplane/srockth.html
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    Solid Rocket Propulsion. How Solid Rocket Motors Work. Conceptually, solid rocket motors (or SRMs) are simple devices with very few moving parts. An electrical signal is sent to the igniter which creates hot gases which ignite the …

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  5. "Solid Rocket Propulsion" - Purdue University

    Solid Rocket Motors. Conceptually, solid rocket motors (or SRMs) are simple devices with very few moving parts. An electrical signal is sent to the igniter which creates hot gases which ignite the main propellant grain (see image below).

  6. Solid Rocket Engine | Glenn Research Center | NASA

  7. Rocket Propulsion | Aeronautics and Astronautics - MIT …

    This class focuses on chemical rocket propulsion systems for launch, orbital, and interplanetary flight. It studies the modeling of solid, liquid-bipropellant, and hybrid rocket engines.