Accession Number : AD0833175

Title :   INVESTIGATION OF SPRING RATE CHARACTERISTICS ON STUB TANK AND SUSTAINER THRUST CONE OF TSTS NO. 3,

Corporate Author : GENERAL DYNAMICS/ASTRONAUTICS SAN DIEGO CA

Personal Author(s) : Haynes, D. R.

Report Date : 30 SEP 1959

Pagination or Media Count : 12

Abstract : The objective of this test was to determine the deflection magnitude of the fuel tank and sustainer thrust cone, at various locations, for each of several loading conditions. (Author)

Descriptors :   *PROPELLANT TANKS), (*SUSTAINER ENGINES, TEST METHODS, STRUCTURAL PROPERTIES, DEFLECTION, THRUST, LOADS(FORCES), FAILURE, SURFACE TO SURFACE MISSILES, AERODYNAMIC LOADING.

Subject Categories : Mechanics
      Liquid Propellant Rocket Engines

Distribution Statement : APPROVED FOR PUBLIC RELEASE