Accession Number : ADD001913
Title : Acoustic Emission System for Solid Propellant Burn Rate Measurements.
Descriptive Note : Patent,
Corporate Author : DEPARTMENT OF THE AIR FORCE WASHINGTON D C
Personal Author(s) : Geisler,Robert L ; Koury,James L ; Johnston,Arch D
Report Date : 19 Aug 1975
Pagination or Media Count : 4
Abstract : The patent relates generally to the measurement of burn rate times in solid propellants and more particularly to the measurement of acoustic signals created by thermal fracture or deflagration of a solid oxidizer in the propellant.
Descriptors : *Solid propellants, *Burning rate, *Measuring instruments, *Patents, *Acoustic emissions, Deflagration, Solid rocket oxidizers, Piezoelectric transducers
Subject Categories : Test Facilities, Equipment and Methods
Combustion and Ignition
Solid Rocket Propellants
Distribution Statement : APPROVED FOR PUBLIC RELEASE