Thermal
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Michael Pauken
(818)354-4242
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Shonte Wright
(818)354-8502
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Implementation and Validation of a PC based ESATAN Model for the Ulysses Spacecraft
Colin Goulding, Jet Propulsion Laboratory
Co-authors: S. Bishop, F. Castro, D. Presti, A. Woodcock
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Abstract |
Paper
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Study of Transient Behavior of Micro Loop Heat Pipe Evaporator and Modifications to the Existing Global Model
Priyanka Ponugoti, University of Cincinnati
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Abstract | Paper
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Improvements to the Aeroheating and Thermal Analysis Code (ATAC)
Alvin Murray, ITT Aerotherm
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Abstract | Paper
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Mars Exploration Rover Entry, Descent, & Landing: A Thermal Perspective
Glenn Tsuyuki, Jet Propulsion Laboratory
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Abstract | Paper
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Thermal Analysis Methods for Aerobraking Heating
Ruth Amundsen, NASA LaRC
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Abstract | Paper
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Thermal Analysis of a Hypersonic Projectile using Semi-Empirical and FEA
Arthur Mabbett, NSWC Dahlgren
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Abstract |
Paper (Please Note: Information herein can not be reproduced without the author’s consent)
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Techniques for Preparing Pro/Engineer Models for Convective Heat Transfer Analysis with CFdesign
Caleb Fisher, NASA Glenn Research Center
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Abstract | Paper
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Lunar Reconnaissance Orbiter Thermal Design Drivers and Current Thermal Design Concept
A. J. Mastropietro, NASA GSFC
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Abstract | Paper
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