Accession Number:

AD0419582

Title:

COMBUSTION INSTABILITY RESEARCH ON SOLID AND LIQUID PROPELLANT ROCKET MOTORS AT SHEFFIELD UNIVERSITY,

Descriptive Note:

Corporate Author:

SHEFFIELD UNIV (ENGLAND)

Personal Author(s):

Report Date:

1963-06-01

Pagination or Media Count:

24.0

Abstract:

Rocket motor combustion instability has been under investigation. The first phase of this work concerned the high frequency tangential mode of oscillation, in a premixed gaseous fuelled rocket motor. In particular the first tangential travelling mode was studied because this is considered the most destructive mode of instability. The research was extended to cast double base propellants. Author

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Distribution Statement:

APPROVED FOR PUBLIC RELEASE