Accession Number : ADD000121

Title :   Hybrid Generator.

Descriptive Note : Patent,

Corporate Author : DEPARTMENT OF THE NAVY WASHINGTON D C

Personal Author(s) : Muzzy,Raymond J

Report Date : 01 Jan 1974

Pagination or Media Count : 4

Abstract : The patent relates to an improved hybrid injector to gasify and aerate a liquid oxidizer. A solid propellant gas generator is enclosed in an annular manifold surrounding the passageway leading from a source of liquid oxidizer to the main combustion chamber. Openings through the manifold communicate the gas generator with the liquid oxidizer passageway to thereby gasify and aerate the liquid oxidizer passing into the main combustion chamber.

Descriptors :   *Hybrid rocket engines, *Injectors, *Patents, Hybrid rocket propellants, Liquid rocket oxidizers, Solid rocket fuels, Gas generating systems, Combustion chambers

Subject Categories : Rocket Engines
      Rocket Propellants

Distribution Statement : APPROVED FOR PUBLIC RELEASE