Demonstrative in-orbit operations of a pressure-regulated two-phase fluid loop model
Author:
Affiliation:
1. NASDA, Office of Satellite Systems, Tokyo, Japan
2. Toshiba Corp., Komukai Works, Kawasaki, Japan
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1998-2451
Reference14 articles.
1. Thermally driven flow experiments aboard Space Shuttle
2. Development Tests of a Vapor/Liquid Separated Two-Phase Fluid Loop
3. A high power spacecraft thermal management system
4. The Hybrid Capillary Pumped Loop
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3. Conceptual Study on Heat Transfer System for Space Solar Power System;41st Aerospace Sciences Meeting and Exhibit;2003-01-06
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