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NASA NTRS ยท 19730023873

Thermal flux transfer system

Abstract

A thermal flux transfer system for use in maintaining the thrust chamber of an operative reaction motor at given temperatures is described. The system is characterized by an hermetically sealed chamber surrounding a thrust chamber to be cooled, with a plurality of parallel, longitudinally spaced, disk-shaped wick members formed of a metallic mesh and employed in delivering a working fluid, in its liquid state, radially toward the thrust chamber and delivering the working fluid, in its vapor state, away from the nozzle for effecting a cooling of the nozzle, in accordance with known principles of an operating heat pipe.

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BibTeXRIS

Freggens, R. A.. 1973-09-18. Thermal flux transfer system. https://ntrs.nasa.gov/citations/19730023873

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