• 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