Publication Date:
2019-07-13
Description:
Heat pipes are among the most promising technologies for space radiator systems. The paper reports further evaluation of potential heat pipe fluids in the intermediate temperature range of 400 to 700 K in continuation of two recent reports. More thermo-physical property data are examined. Organic, inorganic, and elemental substances are considered. The evaluation of surface tension and other fluid properties are examined. Halides are evaluated as potential heat pipe fluids. Reliable data are not available for all fluids and further database development is necessary. Many of the fluids considered are promising candidates as heat pipe fluids. Water is promising as a heat pipe fluid up to 500 to 550 K. Life test data for thermo-chemical compatibility are almost non-existent.
Keywords:
Spacecraft Propulsion and Power
Type:
NASA/CR-2005-213582
,
E-15049
,
Space Technology and Applications International Forum; Feb 13, 2005 - Feb 17, 2005; Albuquerque, NM; United States
Format:
application/pdf
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