NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Effects of anisotropic conduction and heat pipe interaction on minimum mass space radiatorsEquations are formulated for the two dimensional, anisotropic conduction of heat in space radiator fins. The transverse temperature field was obtained by the integral method, and the axial field by numerical integration. A shape factor, defined for the axial boundary condition, simplifies the analysis and renders the results applicable to general heat pipe/conduction fin interface designs. The thermal results are summarized in terms of the fin efficiency, a radiation/axial conductance number, and a transverse conductance surface Biot number. These relations, together with those for mass distribution between fins and heat pipes, were used in predicting the minimum radiator mass for fixed thermal properties and fin efficiency. This mass is found to decrease monotonically with increasing fin conductivity. Sensitivities of the minimum mass designs to the problem parameters are determined.
Document ID
19920001920
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Baker, Karl W.
(NASA Lewis Research Center Cleveland, OH, United States)
Lund, Kurt O.
(California Univ. San Diego., United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1991
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
NAS 1.15:105297
E-6636
NASA-TM-105297
Report Number: NAS 1.15:105297
Report Number: E-6636
Report Number: NASA-TM-105297
Meeting Information
Meeting: International Solar Energy Conference
Location: Maui, HI
Country: United States
Start Date: April 4, 1992
End Date: April 8, 1992
Sponsors: ASME
Accession Number
92N11138
Funding Number(s)
PROJECT: RTOP 590-13-21
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available