Title :
Experimental investigation of a neon cryogenic capillary pumped loop
Author :
Bugby, David C. ; Kroliczek, Edward J. ; Cullimore, Brent A. ; Baumann, Jane E.
Author_Institution :
Swales Aerosp., Beltsville, MD, USA
fDate :
27 Jul-1 Aug 1997
Abstract :
This paper describes the first known demonstration of a cryogenic capillary pumped loop (CCPL) using neon as the working fluid. One obvious application for a neon CCPL is in thermally coupling redundant 35 K cryocoolers to a long-wave TR sensor operating at 40 K without the need for additional flexible links and with negligible (off-cooler) parasitic penalties. The test hardware utilized in this investigation is the 3rd-generation CCPL which was developed by Cullimore and Ring Technologies and Swales Aerospace under NASA/GSFC SBIR funding. Since neon melts at 24.5 K, boils at 27 K, and is a gas above 44.5 K, the practical operating range for a neon CCPL is 30-40 K. The specific demonstrations described herein include several start-ups from a supercritical state without the aid of a cooled shroud, power cycling from 0.1-3.5 W, long-term operation, and start-up/operation under 1.0 cm of adverse evaporator elevation. This paper describes the test set-up, analysis, and results associated with this first neon CCPL
Keywords :
cooling; cryogenics; heat pipes; heat transfer; neon; starting; 0.1 to 3.5 W; 30 to 40 K; Cullimore and Ring Technologies; NASA/GSFC SBIR funding; Ne; Swales Aerospace; adverse evaporator elevation; heat transfer; long-term operation; neon cryogenic capillary pumped loop; power cycling; start-ups; supercritical state; test set-up; thermally coupling redundant cryocoolers; working fluid; Aerospace testing; Cooling; Cryogenics; Hardware; Military satellites; Reservoirs; Space technology; Temperature; Thermal conductivity; Thermal sensors;
Conference_Titel :
Energy Conversion Engineering Conference, 1997. IECEC-97., Proceedings of the 32nd Intersociety
Conference_Location :
Honolulu, HI
Print_ISBN :
0-7803-4515-0
DOI :
10.1109/IECEC.1997.661975