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

Personal Author(s):

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

Subject Categories:

  • Metallurgy and Metallography
  • Surface-Launched Guided Missiles

Distribution Statement:

APPROVED FOR PUBLIC RELEASE