THERMAL RADIATIVE HEAT TRANSFER TO SPACE FROM A BODY ENCLOSED BY A SEMITRANSPARENT BODY | Zendy

R.J. Hefner | Zendy

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THERMAL RADIATIVE HEAT TRANSFER TO SPACE FROM A BODY ENCLOSED BY A SEMITRANSPARENT BODY

Author(s) -

R.J. Hefner

Publication year - 1960

Publication title -

osti oai (u.s. department of energy office of scientific and technical information)

Language(s) - English

Resource type - Reports

DOI - 10.2172/4152631

Subject(s) - radiator (engine cooling) , thermal radiation , dissipation , thermal , energy transfer , heat transfer , radiative transfer , penetration (warfare) , space (punctuation) , mechanics , physics , radiant energy , materials science , radiation , optics , engineering , thermodynamics , computer science , atomic physics , operating system , operations research

Bumpers were proposed for protecting space radiator systems from penetration by meteoroids. The development of equations to determine the thermal energy dissipation to space by a hot body completely enclosed by a second body is presented. The particular case of heat dissipation from space radiators enclosed within the bumpers is considered, and the criteria for selection of bumper materials for a minimum weight radiator system are discussed. (auth

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