Download e-book for iPad: Thermal Design Principles of Spacecraft and Entry Bodies by Jerry Bevans

By Jerry Bevans

ISBN-10: 0123957354

ISBN-13: 9780123957351

ISBN-10: 0323142117

ISBN-13: 9780323142113

Growth in Astronautics and Aeronautics, quantity 21: Thermal layout ideas of Spacecraft and access our bodies is a suite of technical papers drawn often from the yankee Institute of Aeronautics and Astronautics 3rd Thermophysics professional convention, held in la, California on June 24-26, 1968
This quantity is split into 3 components. the 1st half covers a few facets of thermal procedures and layout, together with thermal research, convection, radiation, ablation, and house rocket results. the second one half surveys the distant measurements of the thermophysical and thermal radiation homes and joint conductance, that are severe standards for house thermal layout. The 3rd half specializes in the gap environmental results on thermal coatings. This half bargains first with the speculation of radiative degradation, via a presentation of the laboratory measurements. This half additionally appears into the result of a number of flight experiments.
This booklet might be of significant worth to thermophysicists, area engineers, and architects who're operating within the house technological know-how fields.

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Extra info for Thermal Design Principles of Spacecraft and Entry Bodies

Example text

Their assistance is gratefully acknowledged. *Staff Engineer. tAssistant Manager, Heat Transfer and Thermodynamics Department. 31 T. ISHIMOTO AND J. A. MOSES Grafacon Display Unit The Grafacon input system consists of a "Rand Tablet" writing surface, stylus, display CRT, and control electronics. The "Rand Tablet" is approximately 10 in. square with the x and y sides containing a printed circuit providing 1024 position lines. Resolution is 100 lines/in. The stylus contains a pickup probe, amplifier, and microswitch which is actuated by pressing the stylus tip to the tablet.

Three sets of computations and measurements were made as follows: l) white surface directly irradiated, black and aluminum surfaces dark; 2) black surface irradiated, aluminum and white surfaces dark; and 3) aluminum surface irradiated, white and black surfaces dark. Analytical and Experimental Results Measurements were made both in mid-June and early December 1967 to investigate repeatability with l) extreme seasonal variations of solar irradiation and 2) the use of different operating personnel.

W. Baughn* and G. A. Monroe Itek Corporation, Palo Alto Directorate, Palo Alto, California Abstract An instrument has been developed for the measurement of the thermal radiation geometric configuration factor. This instrument uses an inverse Cassegrain arrangement of mirrors to obtain an image similar to that which occurs with Nusselt's geometric interpretation of the configuration factor. This image is transmitted through a coherent fiber optics bundle to a camera for recording. The primary advantages of this design are the capability to make measurements in an enclosure with limited access, and simplicity in use.

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Thermal Design Principles of Spacecraft and Entry Bodies by Jerry Bevans


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