Ultrasonic Wave Propagation Model for Nondestructive Evaluation of Solid Rocker Motor Propellant
Abstract
The detection of voids in SRM propellant is critical to the safety of Launch Vehicles. Currently this is done with the use of x-rays as an NDE technique. It is hoped to supplant this technique with the use of ultrasonic NDE methods for reasons of reduced cost, increased mobility of the NDE set-up, automated accept/reject criteria, to name a few. To be feasible the ultrasonic NDE methods must be to differentiate between a through-transmission signal from an SRM propellant segment with a void, and a signal from a segment without a void. The ability of ultrasonic NDE to penetrate one meter of propellant has already been demonstrated with sufficient signal-to-noise ratio. The crux of the ultrasonic NDE method will be in using the information present in the received signal to detect, locate, and size voids.
Document Details
- Document Type
- Technical Report
- Publication Date
- Jan 01, 1993
- Accession Number
- ADA267653
Entities
People
- Rosario Nici
Organizations
- Air Force Institute of Technology