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Accession Number:
ADD002285
Title:
Propellant Pressure Burning Rate Slope Modification.
Descriptive Note:
Patent,
Corporate Author:
DEPARTMENT OF THE NAVY WASHINGTON D C
Report Date:
1975-11-18
Pagination or Media Count:
2.0
Abstract:
The burning rate-pressure slopes of smokeless solid propellant compositions containing butyl rubber, polytetrafluoroethylene and ammonium perchlorate, are altered by adding triphenylphosphine. Also, the burning rate of regular propellants which are not smokeless e.g., which additionally contain aluminum, are altered.
Distribution Statement:
APPROVED FOR PUBLIC RELEASE
