This paper describes recent technology developments in thermal energy storage devices for use on spacecraft for thermal control of electronic components requiring thermal stability. A thermal energy storage module has been designed, built and tested using lithium nitrate as the melt material and carbon foam as the conductive filler. For this unit the observed melt temperature was around 30 °C. The supercooling property of lithium nitrate was reduced by adding zinc nitrate as a catalyst. The hydrophobic nature of the carbon foam was overcome by adding a surfactant to the lithium nitrate. The resulting energy storage capacity of the prototype module during the melt was 40 W‐hr/kg. There was very good thermal conductivity through the module resulting in very low temperature gradients even at high power levels.
Thermal Energy Storage Technology Developments
SPACE TECHNOLOGY AND APPLICATIONS INTERNATIONAL FORUM-STAIF 2007: 11th Conf Thermophys.Applic.in Micrograv.; 24th Symp Space Nucl.Pwr.Propulsion; 5th Conf Hum/Robotic Techn & Vision Space Explor.; 5th Symp Space Coloniz.; 4th Symp New Frontrs & Future Con ; 2007 ; Albuquerque, New Mexico (USA)
AIP Conference Proceedings ; 880 , 1 ; 412-420
30.01.2007
9 pages
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
JPL Thermal Technology Portfolio: Current Developments
NTRS | 2019
|Survey of Technology Developments in Flywheel Attitude Control and Energy Storage Systems
Online Contents | 2009
|ERRATUM - Survey of Technology Developments in Flywheel Attitude Control and Energy Storage Systems
Online Contents | 2010
|Thermal Control Technology Developments for a Venus Lander
American Institute of Physics | 2010
|