HYBRID ROCKET PROPULSION SYSTEMS BY: MCDOG SNIZZY ALLEN A.K.A SHAWN.

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Presentation transcript:

HYBRID ROCKET PROPULSION SYSTEMS BY: MCDOG SNIZZY ALLEN A.K.A SHAWN

 A hybrid rocket is a rocket with a rocket motor which uses propellants in two different states of matter - one solid and the other either gas or liquid. The Hybrid rocket concept can be traced back at least 75 years.

 In its simplest form a hybrid rocket consists of a pressure vessel (tank) containing the liquid propellant, the combustion chamber containing the solid propellant, and a valve isolating the two. When thrust is desired, a suitable ignition source is introduced in the combustion chamber and the valve is opened. The liquid propellant (or gas) flows into the combustion chamber where it is vaporized and then reacted with the solid propellant. Combustion occurs in a boundary layer diffusion flame adjacent to the surface of the solid propellant.

