The Effect of Accelaration on the Burning Rate Double Base Rocket Propellants.
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Authors
Bulman, Melvin John
Subjects
Advisors
Netzer, David W.
Date of Issue
1969-06
Date
Publisher
Monterey, California. Naval Postgraduate School
Language
en_US
Abstract
Double base rocket propellants with and without aluminum were
burned in a centrifuge at two pressures and nine accelerations. ,The
burning rates were measured to isolate the effect of the aluminum.
The burning rate of the non-aluminized propellant was found to
vary with acceleration and a model was advanced. The addition of
aluminum causes an increase in burning rate at higher accelerations
and a possible mechanism is discussed.
Type
Thesis
Description
Series/Report No
Department
Aeronautical Engineering
Organization
Naval Postgraduate School