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NASA NTRS · 19900014225

Ceramic heat pipe wick

Abstract

A wick for use in a capillary loop pump heat pipe is disclosed. The wick material is an essentially uniformly porous, permeable, open-cell, silicon dioxide/aluminum oxide inorganic ceramic foam having a silica fiber ratio, by weight, of about 78 to 22, respectively, a density of 6 lbs/cu ft, and an average pore size of less than 5 microns. A representative material having these characteristics is Lockheed Missile and Space Company, Inc.'s HTP 6-22. This material is fully compatible with the freons and anhydrous ammonia and allows for the use of these very efficient working fluids, and others, in capillary loops.

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BibTeXRIS

Seidenberg, Benjamin, Swanson, Theodore. 1989-11-28. Ceramic heat pipe wick. https://ntrs.nasa.gov/citations/19900014225

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