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Accession Number:
ADD002282
Title:
Rocket Motor Apparatus.
Descriptive Note:
Patent,
Corporate Author:
DEPARTMENT OF THE NAVY WASHINGTON D C
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.
Distribution Statement:
APPROVED FOR PUBLIC RELEASE