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Accession Number:
ADD002266
Title:
Method and Apparatus for Reducing Smoke at Launch of High Performance Rockets.
Descriptive Note:
Patent Application,
Corporate Author:
DEPARTMENT OF THE NAVY WASHINGTON D C
Report Date:
1975-08-14
Pagination or Media Count:
13.0
Abstract:
The patent application relates to a method whereby the exhaust signature of high performance rockets is reduced by including in a solid propellant rocket motor a substantially smokeless, double-base propellant and a smoky, high-energy, composite propellant, both simultaneously ignited during missile launch.
Distribution Statement:
APPROVED FOR PUBLIC RELEASE