Analytical determination of the effective emittance of an insulated louver system-Reference-Cited by-同舟云学术

Analytical determination of the effective emittance of an insulated louver system

Published:1965-07-26 Issue: Volume: Page:
ISSN:
Container-title:2nd Annual Meeting
language:
Short-container-title:

Author:

OLLENDORF S.¹

Affiliation:

1. NASA, GODDARD SPACE FLIGHT CENTER, GREENBELT, MD.

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1965-425

Reference7 articles.

1. P - denotes specular system P r i n t i n g 1959, pp. 202, 203.

2. E . M. sparrow, N . G . E c k e r t , V . K. Jonsson, "An Enclosure Theory f o r 3. D . C . Hamilton, W . R . Morgan, "Radiant-Interchange Configuration

3. F a c t o r s " NASA TN 2836, 1952. 4 . John E. Vehrencamp , "Orbiting Geophysical Observatory Temperature

4. C o n t r o l System Design", paper p r e s e n t e d ASME-AICRE Reat T r a n s f e r Conf e r e n c e , August 1963, Boston, Massachusetts. 5 . J . A . Plamondon, "Analysis of Movable Louvers f o r Temperature C o n t r o l " ,

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1. Passive thermal control systems in spacecrafts;Journal of the Brazilian Society of Mechanical Sciences and Engineering;2023-02-18

2. Analytical and experimental studies of an all specular thermal control louver system in a solar vacuum environment;7th Thermophysics Conference;1972-04-10

3. Thermal tests of an improved louver system for spacecraft thermal control;4th Thermophysics Conference;1969-06-16

4. SHUTTER SYSTEM DESIGN FOR THE NIMBUS SPACECRAFT;Thermophysics of Spacecraft and Planetary Bodies;1967