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NASA NTRS · 20150001430

Temperature Control with Two Parallel Small Loop Heat Pipes for GLM Program

Abstract

The concept of temperature control of an electronic component using a single Loop Heat Pipe (LHP) is well established for Aerospace applications. Using two LHPs is often desirable for redundancy/reliability reasons or for increasing the overall heat source-sink thermal conductance. This effort elaborates on temperature controlling operation of a thermal system that includes two small ammonia LHPs thermally coupled together at the evaporator end as well as at the condenser end and operating "in parallel". A transient model of the LHP system was developed on the Thermal Desktop (TradeMark) platform to understand some fundamental details of such parallel operation of the two LHPs. Extensive thermal-vacuum testing was conducted with two thermally coupled LHPs operating simultaneously as well as with only one LHP operating at a time. This paper outlines the temperature control procedures for two LHPs operating simultaneously with widely varying sink temperatures. The test data obtained during the thermal-vacuum testing, with both LHPs running simultaneously in comparison with only one LHP operating at a time, are presented with detailed explanations.

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BibTeXRIS

Khrustalev, Dmitry, Stouffer, Chuck, Ku, Jentung, Hamilton, Jon, Anderson, Mark. 2014-01-01. Temperature Control with Two Parallel Small Loop Heat Pipes for GLM Program. https://ntrs.nasa.gov/citations/20150001430

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