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TECHNICAL PAPERS: Conduction

Optimum Design of Spacecraft Radiators With Longitudinal Rectangular and Triangular Fins

[+] Author and Article Information
Rizos N. Krikkis

Institute of Chemical Engineering and High Temperature Chemical Processes, P.O. Box 1414, Stadiou St., Platani, 26 500 Patras, Greece

Panagiotis Razelos

College of Staten Island, CUNY, NY

J. Heat Transfer 124(5), 805-811 (Sep 11, 2002) (7 pages) doi:10.1115/1.1497359 History: Received December 20, 2001; Revised May 23, 2002; Online September 11, 2002
Copyright © 2002 by ASME
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References

Figures

Grahic Jump Location
Optimum parameter εuopt2 as a function of the opening angle for various emissivities and rectangular profile
Grahic Jump Location
ε−1/2Dopt versus the opening angle for various emissivities and rectangular profile
Grahic Jump Location
Optimum parameter εuopt2 as a function of the opening angle for various emissivities and triangular profile
Grahic Jump Location
ε−1/2Dopt versus the opening angle for various emissivities and triangular profile
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(a) Schematic tubular space radiator; and (b) longitudinal fin geometry

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