Thermal performance and operational characteristics of Loop Heatc pipe (NRL LHP)

SAE Technical Papers

Volumn , Issue , 1998, Pages

  Cheung, Kwok Hung ^a   Hoang, Triem T ^b   Ku, Jentung ^c   Kaya, Tarik ^c  

^a NAVAL RESEARCH LABORATORY   (United States)

^b TTH Research Inc   (United States)

^c NASA GODDARD SPACE FLIGHT CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

NASA; RESEARCH LABORATORIES; SPACE FLIGHT; TESTING;

LOW POWER TEST; LOW-POWER OPERATION; NASA GODDARD SPACE FLIGHT CENTER; NAVAL RESEARCH LABORATORY; OPERATIONAL CHARACTERISTICS; POWER CYCLING TESTS; ROBUST OPERATION; THERMAL PERFORMANCE;

SOFTWARE TESTING;

EID: 85072481931     PISSN: 01487191     EISSN: 26883627     Source Type: Journal    
DOI: 10.4271/981813     Document Type: Conference Paper

References (5)

1. Maidanik, Y.F., Vershinin S.V., Kholodov V.F., and Dolgirev Y.F., US Patent Number 4,515,209, May 7, 1985.
2. Kiseev, V.M., Belonogov, A.G., and Pogorelov N.P., "Development of Two-Phase Loops with Capillary Pumps," SAE 972482, July 14-17, 1997.
3. Maidanik, Y. F., Ferchtater Y.G., and Goncharov K.A., "Capillary Pump Loop for the Systems of Thermal Regulation of Spacecraft," ESA SP-324, 1991.
4. th ICES, Germany, 1994.
5. Phillips, A.L., Fale J.E., Gernert N.J., Sarraf D.B., and Bienert W.J., "Loop Heat Pipe Qualification for High Vibration and High-G Environments" AIAA-98-0885, 1998.