Accession Number : ADD002282
Title : Rocket Motor Apparatus.
Descriptive Note : Patent,
Corporate Author : DEPARTMENT OF THE NAVY WASHINGTON D C
Personal Author(s) : Panella,Edward A
Report Date : 18 Nov 1975
Pagination or Media Count : 5
Abstract : The patent relates to a method whereby a plurality of perforated tubes are placed longitudinally between the insulator layer and silicone rubber layer of a stress relieving rocket motor liner to insure proper pressure distribution within the motor during burn.
Descriptors : *Solid propellant rocket engines, *Rocket propellant grains, *Pressure distribution, *Patents, Combustion, Stress relieving, Combustion chamber liners
Subject Categories : Solid Propellant Rocket Engines
Solid Rocket Propellants
Distribution Statement : APPROVED FOR PUBLIC RELEASE