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NASA NTRS · 19770054428

Re-entrant groove heat pipe

Abstract

This paper describes theoretical and experimentally verified heat pipe characteristics of an axially grooved aluminum extrusion with a re-entrant groove profile. The extrusion is 13 mm diameter with 20 axial grooves, each groove consisting of a nominal .8 mm diameter channel with a .2 mm wide passageway connecting the channel to the hollow core. A computer program was written to compute the zero gravity heat transport capability of the extrusion. A heat pipe was fabricated and its performance characteristics measured. The characteristics of the pipe with ammonia at 20 C are: zero gravity pumping limit 143 w-meters; static wicking height 21.5 mm; evaporator and condenser coefficients 7300 and 20,500 watt/sq m C, respectively.

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BibTeXRIS

Harwell, W., Kaufman, W. B., Tower, L. K.. 1977-06-01. Re-entrant groove heat pipe. https://ntrs.nasa.gov/citations/19770054428

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