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Accession Number:
AD0829819
Title:
STRUCTURAL TEST REQUIREMENTS FATIGUE AND CYCLE TESTING OF THE XSM-65D MISSILE,
Descriptive Note:
Corporate Author:
GENERAL DYNAMICS/ASTRONAUTICS SAN DIEGO CA
Report Date:
1958-09-05
Pagination or Media Count:
25.0
Abstract:
The purpose of this test is to investigate the structural fatigue life of the XSM-65D missile and determine statistical fatigue properties of the typical splice joints used in the missile design. Author
Distribution Statement:
APPROVED FOR PUBLIC RELEASE