Validation Design for a Multi-Evaporator Miniature Loop Heat Pipe for Spacecraft Applications
Author:
Affiliation:
1. NASA Goddard Space Flight Center, Greenbelt, Maryland 20771
2. TTH Research, Inc., Clifton, Virginia 20124
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.51349
Reference35 articles.
1. Operating Characteristics of Loop Heat Pipes
2. Geoscience Laser Altimeter System (Glas) Loop Heat Pipes - An Eventful First Year On-Orbit
3. Thermal Vacuum/Balance Test Results of Swift BAT with Loop Heat Pipe Thermal System
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