Hostname: page-component-cd9895bd7-mkpzs Total loading time: 0 Render date: 2024-12-22T15:17:15.947Z Has data issue: false hasContentIssue false

The heat pipe: its development, and its aerospace applications

Published online by Cambridge University Press:  04 July 2016

D. A. Reay*
Affiliation:
International Research and Development Co Ltd, Newcastle upon Tyne

Extract

The transport of thermal energy from one location to another, for example from a heat source to a remote heat sink, has been a major topic of study over the past decade.

Most of the work has been directed at improving the efficiency of heat transport, while retaining the simplicity and reliability of what is, in general, considered as a secondary part of any system.

One device which has fulfilled most of the requirements of such a heat transport system is the heat pipe. The heat pipe was first proposed by Gaugler of the General Motors Corporation (US) in 1942, and was the subject of a patent published in 1944. Because the heat transfer problems of that time could be solved by more conventional methods, Gaugler's ideas remained unexploited for approximately 20 years. It was not until the early 1960s that Grover, without knowledge of Gaugler's proposals, in effect re-invented the heat pipe while working at Los Alamos Scientific Laboratory. Grover and his colleagues were working on spacecraft power generation systems at the time.

Type
Technical notes
Copyright
Copyright © Royal Aeronautical Society 1974 

Access options

Get access to the full version of this content by using one of the access options below. (Log in options will check for institutional or personal access. Content may require purchase if you do not have access.)

References

(a) US Patent 2,350,348. Published June 1944.Google Scholar
(b) Winter, E. R. F. and Barsch, W. O. The Heat Pipe. Advances in Heat Transfer, Vol 7. Academic Press, 1971.Google Scholar
1. Gerrels, E. E. and Larson, J. W. Brayton Cycle Vapour Chamber (Heat Pipe) Radiator Study. NASA CR-1677, Contract NAS3-10615, General Electric Company, February 1971.Google Scholar
2. Asselman, G. A. A. and Green, D. B. The heat pipe, an applied technology. Philips Technical Review, 1972.Google Scholar
3. Leefer, B. I. Nuclear thermionic energy converter. Proceedings 20th Annual Power Sources Conf, pp 172175, May 1966.Google Scholar
4. Wyatt, T. Controllable heat pipe experiment. Johns Hopkins University. Applied Physics Lab. SDO-1134, March 1965.Google Scholar
5. Marcus, B. D. and Fleischman, G. L. Steady state and transient performance of hot reservoir gas controlled heat pipes. ASME Paper 70HT/SpT-ll, New York, 1970.Google Scholar
6. Turner, R. C. The constant temperature heat pipe—a unique device for the thermal control of spacecraft components. AIAA 4th Thermophys Con, Paper 69-632, June 1969.Google Scholar
7. Bienert, W. Heat pipes for temperature control. AIChE 4th Intersoc Energy Conf, Washington DC, September 1969.Google Scholar
8. Roukis, J., Rogovin, J. and Swerdling, B. Heat pipe applications to space vehicles. Grumman Aerospace. AIAA Paper 71-410, 1971.Google Scholar
9. Bienert, W. and Brennan, P. J. Transient performance of electrical feedback—controlled variable conductance heat pipes, ASME Paper 71-Av-27, New York, 1971.Google Scholar
10. Bienert, W., Brennan, P. J. and Kirkpatrick, J. P. Feedback-controlled variable conductance heat pipes. AIAA Paper 71-421, 1971.Google Scholar
11. Bienert, W., et al. Study to evaluate the feasibility of a feedback-controlled variable conductance heat pipe. Contract NAS2-5722, Tech Summary Report, DTM-70-4, Dynatherm, September 1970.Google Scholar
12. Katzoff, S. Heat pipes and vapour chambers for the thermal control of spacecraft. AIAA Paper 67-310, April 1967.Google Scholar
13. Kirkpatrick, J. P. and Marcus, B. D. A variable conductance heat pipe experiment. AIAA Paper 71-411, 1971.Google Scholar
14. Anand, D. K. and Hester, R. B. Heat pipe applications for spacecraft thermal control. Johns Hopkins Univ Tech Memo TG-922, August 1967.Google Scholar
15. Schlosinger, A. P. Heat pipes for space suit temperature control. Aviation and Space Conference, Los Angeles, June 1968.Google Scholar
16. Savage, C. J. Heat pipes and vapour chambers for satellite thermal balance. RAE Tech Report 69125, June 1969.Google Scholar
17. Thurman, J. L. and Mei, S. Application of heat pipes to spacecraft thermal control problems. Tech Note AST- 275, Brown Engineering (Teledyne), July 1968.Google Scholar
18. Conway, E. C. and Kelley, M. J. A continuous heat pipe for spacecraft thermal control. GEC Space Systems, Pennsylvania (undated).Google Scholar
19. Harkness, R. E. Performance of the GEOS II. Advanced Prop Lab Tech Digest, pp 14-19, May-June 1969.Google Scholar
20. Basiulis, A. Undirectional heat pipes to control TWT temperature in synchronous orbit. NASA Contract NAS- 3-9719, Hughes Aircraft Co, California, 1969.Google Scholar
21. Edelstein, F. and Hemback, R. J. Design, fabrication and testing of a variable conductance heat pipe for equipment thermal control. Grumman Aerospace. AIAA Paper 71-422, 1971.Google Scholar
22. Eby, R. J., Kelly, W. J. and Karam, R. D. Thermal control of ATS F & G ASME Paper 71-Av-28, New York, 1971.Google Scholar
23. Scollon, T. R. Heat pipe energy distribution systems for spacecraft thermal control. GEC Space Systems Group AIAA Paper 71-412, 1971.Google Scholar
24. Groll, M. and Zimmerman, P. Heat pipe for temperature control of a meteorological satellite. IKE, University of Stuttgart ESRO Report CR-59, September 1972.Google Scholar
25. Reay, D. A. and Summerbell, D. The development of heat pipes for satellites. Paper 9-2, 1st Intnl Heat Pipe Conference, Stuttgart, Germany, October 1973.Google Scholar