Monochromatic high-speed photography of solid rocket propellant combustion

Authors
Edington, Ronald James
Advisors
Netzer, David W.
Second Readers
Subjects
monochromatic high-speed photography
solid rocket propellant combustion
Date of Issue
1983-03
Date
March 1983
Publisher
Monterey, California. Naval Postgraduate School
Language
en_US
Abstract
Eight composite solid propellant formulations containing varying diameter and weight percentages of metallic particles were burned in strand form in two different nitrogen purged combustion bombs at a pressure of 500 psi. High-speed cinematography was used with an argon laser as the primary monochromatic light source. Two illumination approaches were tried, backlighting and frontlighting. Careful examination of the backlighting films revealed that the flame envelopes surrounding the particles could be eliminated and that the true particle size could be obtained. However, Schlieren effects obscured much of the information which was available on the film. The frontlighting technique eliminated the Schlieren effects and allowed good particle behavioral data to be obtained, but the reflected monochromatic light was not sufficient to allow true particle diameters to be taken.
Type
Thesis
Description
Series/Report No
Department
Aeronautics
Organization
Naval Postgraduate School (U.S.)
Identifiers
NPS Report Number
Sponsors
F04611-83-x-0010
Funding
F04611-83-x-0010
Format
Citation
Distribution Statement
Approved for public release; distribution is unlimited.
Rights
This publication is a work of the U.S. Government as defined in Title 17, United States Code, Section 101. Copyright protection is not available for this work in the United States.
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