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NASA NTRS · 19830045909

Long titanium heat pipes for high-temperature space radiators

Abstract

Titanium heat pipes are being developed to provide light weight, reliable heat rejection devices as an alternate radiator design for the Space Reactor Power System (SP-100). The radiator design includes 360 heat pipes, each of which is 5.2 m long and dissipates 3 kW of power at 775 K. The radiator heat pipes use potassium as the working fluid, have two screen arteries for fluid return, a roughened surface distributive wicking system, and a D-shaped cross-section container configuration. A prototype titanium heat pipe, 5.5-m long, has been fabricated and tested in space-simulating conditions. Results from startup and isothermal operation tests are presented. These results are also compared to theoretical performance predictions that were used to design the heat pipe initially.

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BibTeXRIS

Girrens, S. P., Ernst, D. M.. 1982-01-01. Long titanium heat pipes for high-temperature space radiators. https://ntrs.nasa.gov/citations/19830045909

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