ACKNOWLEDGMENTS This research was sponsored by the United States Air Force under contract F33615- 87-C-2738 administered by the Aero Propulsion Laboratory. Ms J. E. Johnson (AFWAL/POOS) was the Program Monitor. Technical help provided by Mr J. Tennant and Mr M. Ryan (UES), and Mr D. Reinmuller (APL) is appreciated. REFERENCES [1] Ranken, W.A. (1981) Heat pipe development for the SPAR space power system, Advances in Heat Pipe Technology, Proceedings of the 4th International Heat Pipe Conference, September, London, pp. 561-574, Ed. D. A. Reay, Pergamon Press, 1982. [2] McNamara, E.J., Dottore, F.A. et al. (1987) Analytical studies performed supporting SP-1OO heat rejection subsystem, 22nd Intersociety Energy Conversion Engineering Conference, 10-14 August, Vol. I, pp. 424-429. [3] Merrigan, M.A. (1985) Heat pipe technology issues, Space Nuclear Power Systems 1984, Vol. 2, Orbit Book Co., Malabar, Florida, Ed. M. S. El Genk & M. D. Hoover, pp. 419-426. [4] Ponnappan, R. (1988) Studies on the Startup Transients and Performance of a Gat pipes, High Temperature (USA), Vol. 21, No. 6, November- December, pp. 929-936.
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