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NASA NTRS · 19940015021

Materials characterization of propellants using ultrasonics

Abstract

Propellant characteristics for solid rocket motors were not completely determined for its use as a processing variable in today's production facilities. A major effort to determine propellant characteristics obtainable through ultrasonic measurement techniques was performed in this task. The information obtained was then used to determine the uniformity of manufacturing methods and/or the ability to determine non-uniformity in processes.

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BibTeXRIS

Workman, Gary L., Jones, David. 1993-10-31. Materials characterization of propellants using ultrasonics. https://ntrs.nasa.gov/citations/19940015021

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