Accession Number:
ADD002282
Title:
Rocket Motor Apparatus.
Descriptive Note:
Patent,
Corporate Author:
DEPARTMENT OF THE NAVY WASHINGTON D C
Personal Author(s):
Report Date:
1975-11-18
Pagination or Media Count:
5.0
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:
Subject Categories:
- Solid Propellant Rocket Engines
- Solid Rocket Propellants