Accession Number : ADD010603
Title : Integrated Solid Propellant Gas Generator and Fluid Heat Exchanger.
Descriptive Note : Patent,
Corporate Author : DEPARTMENT OF THE AIR FORCE WASHINGTON DC
Personal Author(s) : Jenkins,Donald S
Report Date : 27 Sep 1983
Pagination or Media Count : 5
Abstract : This invention relates to a gas generator which is structurally and functionally integrated with a fluid heat exchanger. A liquid which is to be heated, vaporized, and used as pressurized gas is introduced into the integrated apparatus where the liquid absorbs heat from the adjacent, but separated, hot gas flow from the gas generator. Unlike the prior art, this integrated gas generator/fluid heat exchanger is useable to pressurize an oxidizer tank of a liquid engine missile.
Descriptors : *Patents, *Gas generating systems, *Heat exchangers, *Propellant tanks, Pressurization, Liquid rocket oxidizers, Heating, Vaporization, Hot gases, Liquid propellant rocket engines, Solid propellants, Integrated systems
Subject Categories : Hydraulic and Pneumatic Equipment
Liquid Propellant Rocket Engines
Distribution Statement : APPROVED FOR PUBLIC RELEASE