1. J.M. Gottschlich, Capillary pumped loops for aerospace application, SAE Tech. Ser., Paper No. 892318, 1989.
2. J.F. Stenger, Experimental feasibility study of water-filled capillary-pumped heat transfer loops, NASA TM X-1310, 1966.
3. Low-temperature heat pipe with divided channels for vapour and liquid, high temp;Gerasimov;Teplofizika Vysokikh Temperatur,1974
4. A.K. Goncharov, V.L. Barantsevich, A.A. Orlov, Experience of development of heat pipes applied in Russian spacecrafts, in: Proc. Fifth Minsk Int. Sem. Heat Pipes, Heat Pumps, Refrigerators, Minsk, Belarus, September 8–11, 2003.
5. Thermal control technologies for complex spacecraft systems;Swanson,2004