STRUCTURAL VERIFICATION TESTS OF THE AEROJET UTILITY VAN
Abstract
Structural tests to verify the acceptability of the utility van as a transport vehicle for second-stage Minuteman operational motors were successfully completed. During the tests, the van and tie-downs were subjected to limit loads to determine stress levels at critical load points and to measure vehicle deflection and recovery from the downward and side loads imposed.
Document Details
- Document Type
- Technical Report
- Publication Date
- Dec 01, 1962
- Accession Number
- AD0296871
Entities
People
- W. D. Hulse
Organizations
- Aerojet Rocketdyne Holdings