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

Subject Categories:

Distribution Statement:

APPROVED FOR PUBLIC RELEASE