Accession Number:

AD0851517

Title:

Effects of Engine Thrust Transients on XSM-65D Missiles,

Descriptive Note:

Corporate Author:

GENERAL DYNAMICS/ASTRONAUTICS SAN DIEGO CA

Personal Author(s):

Report Date:

1960-11-03

Pagination or Media Count:

151.0

Abstract:

Missile 36D was tested at the Sycamore Canyon Captive Test Site, from 28 October 1959 through 9 February 1960. The purpose of the test program was to study missile tank skin strain characteristics during the thrust build-up transient for both wet and dry engine start configurations. Author

Subject Categories:

  • Surface-Launched Guided Missiles
  • Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE