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