Accession Number:

AD0829815

Title:

NATURAL BENDING MODES OF THE XSM-65C MISSILES AT VARIOUS INSTANTS OF FLIGHT,

Descriptive Note:

Corporate Author:

GENERAL DYNAMICS/ASTRONAUTICS SAN DIEGO CA

Personal Author(s):

Report Date:

1958-07-01

Pagination or Media Count:

70.0

Abstract:

The note furnishes the free-free bending vibration modes for the XSM-65C missiles. The data presented is required for stability and loads investigations in which the effects of missile elasticity and vibration are important considerations. The bending modes for the XSM-65C missile tabulated in this report reflect a revised propellant sloshing analysis and a 33 mass station solution. An addendum is also included in which the bending vibration modes are presented for the fully tanked XSM-65C missile cantilevered at Station 1200. Author

Subject Categories:

  • Surface-Launched Guided Missiles
  • Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE