The enhanced capillary pumped loop flight experiment, a prototype ofthe EOS platform thermal control system-Reference-Cited by-同舟云学术

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The enhanced capillary pumped loop flight experiment, a prototype ofthe EOS platform thermal control system

Published:1991-06-24 Issue: Volume: Page:
ISSN:
Container-title:26th Thermophysics Conference
language:
Short-container-title:

Author:

BUTLER D.¹,HOANG T.²

Affiliation:

1. NASA, Goddard Space Flight Center, Greenbelt, MD

2. NASA, Goddard Space Flight Center; NSI Technology Services Corp., Greenbelt, MD

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1991-1377

Reference10 articles.

1. CAPL Critical Design Review, RCA Astro-Electronics,1986.

2. Fredley,JE.andC.Braun,"ALowPressureDrop HeatExchanger withIntegralHeatPipe,"F'roceedingsof the 1988ASMENationalHeatTransferConference,Vol. 1,pp. 361-377.

3. HandbookofFluidDynamics,V.L. Sweeter,Editor, McGraw-HillBook Company,Inc., 1961.

Cited by 4 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Mathematical model of a loop heat pipe with cylindrical evaporator and integrated reservoir;Applied Thermal Engineering;2008-06

2. Solar Absorber Plates: Design and Application to Microgravity Capillary-Pumped-Loop Experiments;Journal of Spacecraft and Rockets;2000-01

3. Gravity dependent condensation pressure drop and heat transfer in ammonia two-phase heat transport systems;28th National Heat Transfer Conference;1992-08-09

4. A prototype heat pipe heat exchanger for the capillary pumped loop flight experiment;27th Thermophysics Conference;1992-07-06

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