Cryogenic heat pipes in spacecraft applications-Reference-Cited by-同舟云学术

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Cryogenic heat pipes in spacecraft applications

Published:1986-06-02 Issue: Volume: Page:
ISSN:
Container-title:4th Thermophysics and Heat Transfer Conference
language:
Short-container-title:

Author:

PETERSON G.¹,COMPAGNA G.²

Affiliation:

1. Texas A & M University, College Station

2. Eastman Kodak Co., Rochester, NY

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1986-1254

Reference25 articles.

1. AFFDL-TR-66-225, June 1956. Id 3. Hopkins, 9. 3. and Rr;oks,i"P. "Orhital Perfsraance of a 3ire-Yar:i?tirxe

2. Cryogenic Engineerinq," vol. 75, pp.1387-1097. i'iR2, 4. Sherman, 4. "%istoiy, Statui, a.;d Future Apolications of 5imCehcrne :r3oqeniC . Systeins," -ante; in C:y_osse

3. Enqineering, Vol. 27, Plenun ?res:> N. Y . , 1982,p. inn 7-i0?9.

Cited by 2 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. PERFORMANCE CHARACTERISTICS OF CRYOGENIC TWO-PHASE THERMOSYPHON;Proceeding of Heat Pipe Technology: Volume 1. Fundamentals and Experimental Studies;2023

2. Development of high performance sintered powder metal wick cryogenicheat pipes;23rd Thermophysics, Plasmadynamics and Lasers Conference;1988-06-27

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