DocumentCode
2229108
Title
Partially air coupled through transmission ultrasonic inspection of large solid rocket motors
Author
Gammell, Paul M.
Author_Institution
Mater. Evaluation Branch, Naval Surface Warfare Center, Silver Spring, MD
fYear
1993
fDate
31 Oct-3 Nov 1993
Firstpage
659
Abstract
Through transmission ultrasonic inspection techniques have many advantages as a survey technique. When solid rocket motors are inspected it is highly desirable not to contact the propellant with the transducer for reasons involving safety, damage to the product, and speed of inspection. The development of air coupled ultrasonic inspection techniques for large solid rocket motors is discussed. The appropriate frequency range appears to be around 50 kHz. Transducers that performed satisfactorily at these frequencies and suggested improvements are discussed
Keywords
aerospace propulsion; aerospace testing; flaw detection; inspection; rockets; ultrasonic materials testing; 50 kHz; cracks; disbonds; excessive porosity; large solid rocket motors; partially air coupled through transmission ultrasonic inspection; voids; Acoustic transducers; Couplings; Frequency; Impedance; Inspection; Propulsion; Reluctance motors; Rockets; Solids; Ultrasonic transducers;
fLanguage
English
Publisher
ieee
Conference_Titel
Ultrasonics Symposium, 1993. Proceedings., IEEE 1993
Conference_Location
Baltimore, MD
Print_ISBN
0-7803-2012-3
Type
conf
DOI
10.1109/ULTSYM.1993.339494
Filename
339494
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