Theoretical performance analysis of electrochromic radiators for space suit thermal control

Variable emissivity electrochromics have been proposed as an enabling technology for integrating a radiator capability into a space suit in order to augment or replace the traditional means of heat rejection achieved via water sublimation. Thermal analysis was performed to establish design trade spaces and to provide operational guidelines and performance specifications for electrochromic technology development. Based on using the available surface area of an entire space suit as a radiator and the projected infrared emissivity modulation capability of state-of-the-art electrochromic material, the proposed application for space suit heat rejection suggests the potential exists to reduce or eliminate reliance on water consumption for thermal control within a defined range of metabolic and environmental boundary conditions.

[1]  Claes G. Granqvist,et al.  Handbook of inorganic electrochromic materials , 1995 .

[2]  Ryan A. Stephan,et al.  Performance Testing of an Advanced Lightweight Freezable Radiator , 2006 .

[3]  Bruce Conger,et al.  Lunar Portable Life Support System Heat Rejection Study , 2009 .

[4]  James E. Anderson,et al.  Results of shuttle EMU thermal vacuum tests incorporating an infrared imaging camera data acquisition system , 1991 .

[5]  F. G. Benedict,et al.  The Temperature of the Human Skin. , 1919, Proceedings of the National Academy of Sciences of the United States of America.

[6]  Gajanana C. Birur,et al.  Large, Switchable Electrochromism in the Visible Through Far‐Infrared in Conducting Polymer Devices , 2002 .

[7]  R. Mortimer,et al.  New Electrochromic Materials , 2002, Science progress.

[8]  Harry Jones The Dynamic Impact of EVA on Lunar Outpost Life Support , 2008 .

[9]  David M. Klaus,et al.  Conceptual Analysis of Electrochromic Radiators for Space Suits , 2009 .

[10]  James Nabity,et al.  A Freezable Heat Exchanger for Space Suit Radiator Systems , 2008 .

[11]  A GUIBERT,et al.  Radiation area of the human body. , 1952, Journal of applied physiology.

[12]  A. Hernández-Cabrera,et al.  Coherent response of a biased double-well superlattice subjected to an ultrashort interband excitation , 2002 .

[13]  Jean-Marie Tarascon,et al.  Flexible electrochromic reflectance device based on tungsten oxide for infrared emissivity control , 2002 .

[14]  Anthony J. Hanford,et al.  Testing of Commercial Hollow Fiber Membranes for Space Suit Water Membrane Evaporator , 2009 .

[15]  Howard P. Groger,et al.  All‐Solid‐State Electrochromic Variable Emittance Coatings for Thermal Management in Space , 2003 .

[16]  Frank Kreith Radiation heat transfer for spacecraft and solar power plant design , 1962 .

[17]  Stephen A. Bayes,et al.  Regenerable non-venting thermal control subsystem for extravehicular activity , 1983 .

[18]  H. Demiryont,et al.  Electrochromic emissivity modulator for spacecraft thermal management , 2009 .