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Birur, Gajanana C.
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Design Description and Initial Characterization Testing of an Active Heat Rejection Radiator with Digital Turn-Down Capability

SAE International Journal of Aerospace

  • Journal Article
  • 2009-01-2419
Published 2009-07-12 by SAE International in United States
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Mechanically Pumped Fluid Loop Technologies for Thermal Control of Future Mars Rovers

Published 2006-07-17 by SAE International in United States
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Evaluation of Coatings and Materials for Future Radiators

Published 2006-07-17 by SAE International in United States
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High Temperature Mechanically Pumped Fluid Loop for Space Applications –Working Fluid Selection

Published 2004-07-19 by SAE International in United States
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Active Control of the Operating Temperature in a Loop Heat Pipe with Two Evaporators and Two Condensers

Published 2001-07-09 by SAE International in United States
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An Experimental Study of the Operating Temperature in a Loop Heat Pipe with Two Evaporators and Two Condensers

Published 2001-07-09 by SAE International in United States
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Testing of a Loop Heat Pipe with Two Evaporators and Two Condensers

Published 2001-07-09 by SAE International in United States
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Thermal Performance of a Miniature Variable Conductance Loop Heat Pipe

Published 2000-07-10 by SAE International in United States
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Thermal Control of Mars Lander and Rover Batteries and Electronics Using Loop Heat Pipe and Phase Change Material Thermal Storage Technologies

Published 2000-07-10 by SAE International in United States
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Mars Pathfinder Active Heat Rejection System: Successful Flight Demonstration of a Mechanically Pumped Cooling Loop

Published 1998-07-13 by SAE International in United States
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