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Heat transfer from an internal combustion (Otto-cycle) engine on the surface of MarsThe cooling requirements for an average car sized engine (spark-ignition, V-6, four-stroke, naturally aspirated, about 200 kg, about 100 kW) were looked at for Mars. Several modes of cooling were considered, including forced convection, exhaust, radiation and closed loop systems. The primary goal was to determine the effect of the thinner Martian atmosphere on the cooling system. The results show that there was only a 6-percent difference in the cooling requirements. This difference was due mostly to the thinner atmosphere during forced convection and the heat capacity of the exhaust. A method using a single pass counter-flow heat exchanger is suggested to offset this difference in cooling requirements.
Document ID
19920056955
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Gwynne, Owen
(SETI Institute; NASA, Ames Research Center Moffett Field, CA, United States)
Date Acquired
August 15, 2013
Publication Date
May 1, 1992
Publication Information
Publication: British Interplanetary Society, Journal
Volume: 45
Issue: 5, Ma
ISSN: 0007-094X
Subject Category
Fluid Mechanics And Heat Transfer
Accession Number
92A39579
Distribution Limits
Public
Copyright
Other

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