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Accession Number:
AD0270114
Title:
RESEARCH ON SOLID PROPELLANT IGNITABILITY AND IGNITER CHARACTERISTICS
Descriptive Note:
Corporate Author:
PRINCETON UNIV N J
Report Date:
1961-12-18
Pagination or Media Count:
1.0
Abstract:
The ignition was studied of small internal burning solid propellant grains in a rocket motor, utilizing hot combustion products from an upstream gas rocket to test the applicability of the concept that ignition is a runaway gas phase reaction. Author
Distribution Statement:
APPROVED FOR PUBLIC RELEASE