Avionics Passive Cooling With Microencapsulated Phase Change Materials
1998 ◽
Vol 120
(3)
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pp. 238-242
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Keyword(s):
Analysis for an avionics application typical of remotely located, intermittently operated avionics on aircraft and missiles show that a large weight reduction (about 9:1) can be obtained by using recently developed microencapsulated phase change materials technology instead of a solid aluminum plate for a passive heat sink. Tests with a configuration based on the typical avionics application used for analysis show good agreement with analysis. Use of microencapsulated rather than bulk phase change materials avoids a number of design problems previously encountered with application of such materials.
2021 ◽
Vol 126
◽
pp. 105407
2018 ◽
Vol 13
(4)
◽
pp. 301-310
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2015 ◽
Vol 26
(6)
◽
pp. 613-619
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2019 ◽
Vol 192
◽
pp. 72-80
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2017 ◽
Vol 115
◽
pp. 737-742
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