Accession Number : AD0631358

Title :   THERMAL AND STRUCTURAL ANALYSIS OF SPACE RADIATOR SYSTEMS.

Descriptive Note : Technical note,

Corporate Author : ROME UNIV (ITALY) SCUOLA DI INGEGNERIA AERONAUTICA

Personal Author(s) : Broglio,Luigi

Report Date : AUG 1961

Pagination or Media Count : 30

Abstract : The paper is divided into four parts. In Part I the problem is studied referring to an element of radiator consisting of a hollow infinite cylinder, heated from inside, with axial symmetry, and cooled from outside, still with axial symmetry, through spontaneous radiation. In Part II the influence of the variation of thermal conductivity and of specific heat with temperature is taken into account. In Part III the particular case of steady flow is considered. In Part IV thermal stresses are studied, for the case of the cylinder of small thickness. Some numerical examples complete the work. (Author)

Descriptors :   (*RADIATORS(HEATING AND COOLING), SPACECRAFT COMPONENTS), CYLINDRICAL BODIES, SHELLS(STRUCTURAL FORMS), HEAT TRANSFER, THERMAL CONDUCTIVITY, SPECIFIC HEAT, THERMAL STRESSES, FLUID FLOW, STRUCTURAL PROPERTIES

Subject Categories : Air Condition, Heating, Lighting & Ventilating
      Thermodynamics
      Unmanned Spacecraft

Distribution Statement : APPROVED FOR PUBLIC RELEASE