Solid Propellant Structural Test Vehicle. Techniques for Measuring Stress, Strain and Temperature in Solid Propellant Motors
Abstract
The report summarizes experience gained on propellant grain instrumentation during 3 years of effort on the AFRPL-sponsored Structural Test Vehicle (STV) Program. The report discusses the types of stress-, strain-, and temperature-measuring transducers available for use in solid propellant grains, methods of calibrating the transducers, installation techniques, and special handling problems. The report is designed for use as a practical 'how to do' guide in the study of propellant grain structural integrity.
Document Details
- Document Type
- Technical Report
- Publication Date
- Nov 01, 1971
- Accession Number
- AD0890778
Entities
People
- Harold Leeming
Organizations
- Lockheed Propulsion Company