Accession Number : AD0843804

Title :   Centaur Nose Fairing Honeycomb Specimen Test,

Corporate Author : GENERAL DYNAMICS/ASTRONAUTICS SAN DIEGO CA

Personal Author(s) : Panella, Vincent P.

Report Date : 13 NOV 1961

Pagination or Media Count : 34

Abstract : The purpose of the study was to determine Young's modulus of the facing material, and the core shear modulus in bending of the sandwich structure as a function of core orientation and loading systems. (Author)

Descriptors :   *SANDWICH CONSTRUCTION), (*LAUNCH VEHICLES, NOSE CONES), (*FAIRINGS, STRUCTURAL PROPERTIES, HONEYCOMB CORES, GLASS TEXTILES, SHEAR STRESSES, BENDING, DEFLECTION, LOADS(FORCES), CURVE FITTING, FAILURE(MECHANICS), THICKNESS, TABLES(DATA), PERFORMANCE(ENGINEERING).

Subject Categories : Structural Engineering and Building Technology
      Mechanics
      Ground Support Sys & Facil For Space Vehicles

Distribution Statement : APPROVED FOR PUBLIC RELEASE