Design of a Liquid Metal Heat Pipe Space Experiment

941156

4/1/1994

Authors
Abstract
Content
Although high temperature, liquid metal heat pipe radiators have become a standard component design for many high power space systems, no experimental data on the operation of these kinds of heat pipes in a micro-gravity environment exists. Issues such as which wick structures or fluids work best in these conditions are unknown. In addition, the freeze/thaw behavior of liquid metals in zero-g is not well understood. The purpose of the Liquid Metal Thermal Experiment, known as LMTE, is to fill this gap in our knowledge of liquid metal heat pipes by flying three potassium heat pipes on board the Space Shuttle in 1995.
Meta TagsDetails
DOI
https://doi.org/10.4271/941156
Pages
10
Citation
Critchley, E., and Corrigan, M., "Design of a Liquid Metal Heat Pipe Space Experiment," SAE Technical Paper 941156, 1994, https://doi.org/10.4271/941156.
Additional Details
Publisher
Published
4/1/1994
Product Code
941156
Content Type
Technical Paper
Language
English