Operating Characteristics of Loop Heat Pipes

The loop heat pipe (LHP) was invented in Russia in the early 1980’s. It is a two-phase heat transfer device that utilizes the evaporation and condensation of a working fluid to transfer heat, and the capillary forces developed in fine porous wicks to circulate the fluid. The LHP is known for its high pumping capability and robust operation because it uses finepored metal wicks and the integral evaporator/hydroaccumulator design. It has gained rapid acceptance in recent years as a thermal control device in space applications. This paper presents an overview of the LHP operation. The physical processes and the thermal-hydraulic behaviors of the LHP are first described. Operating characteristics as functions of various parameters including the heat load, sink temperature, ambient temperature, and elevation are presented. Peculiar behaviors in LHP operation such as temperature hysteresis and temperature overshoot during start-up are explained. Issues related to multiple -evaporator LHP’s are also addressed.

[1]  Yury F. Maidanik,et al.  Design and Investigation of a Capillary Pumped Loop for Advanced Thermal Control Systems of Space Vehicles , 1995 .

[2]  Michael N. Nikitkin,et al.  Non Condensable Gases and Loop Heat Pipe Operation , 1998 .

[3]  Walter B. Bienert,et al.  Investigation of temperature control characteristics of loop heat pipes , 1994 .

[4]  Jentung Ku,et al.  Recent advances in capillary pumped loop technology , 1997 .

[5]  Yu. G. Fershtater,et al.  Design and Investigation of Methods of Regulation of Loop Heat Pipes for Terrestrial and Space Applications , 1994 .

[6]  Brent A. Cullimore,et al.  CPL and LHP Technologies: What are the Differences, What are the Similarities? , 1998 .

[7]  J. Ku Overview of Capillary Pumped Loop Technology , 1993 .

[8]  Jentung Ku,et al.  Thermodynamic aspects of capillary pumped loop operation , 1994 .

[9]  Jentung Ku,et al.  Investigation of the Temperature Hysteresis Phenomenon of a Loop Heat Pipe , 1999 .

[10]  Walter B. Bienert,et al.  LOOP HEAT PIPE FLIGHT EXPERIMENT , 1998 .

[11]  Tarik Kaya,et al.  Testing of the Geoscience Laser Altimeter System (GLAS) prototype loop heat pipe , 1999 .

[12]  K. A. Goncharov,et al.  Loop Heat Pipes in Thermal Control Systems for “OBZOR” Spacecraft , 1995 .

[13]  Jentung Ku,et al.  Ground Tests of Capillary Pumped Loop (CAPL 3) Flight Experiment , 1998 .

[14]  Jentung Ku,et al.  Thermal Performance and Operational Characteristics of Loop Heat Pipe (NRL LHP) , 1998 .

[15]  Jentung Ku,et al.  Mathematical Modeling of Loop Heat Pipes , 1999 .

[16]  Triem T. Hoang,et al.  Verification of a Transient Loop Heat Pipe Model , 1999 .

[17]  N. W. Dunbar,et al.  ATLID Laser Head Thermal Control-Design and Development of a Two-Phase Heat Transport System for Practical Application , 1996 .

[18]  Yu. G. Fershtater,et al.  Loop Heat Pipes: Design, Investigation, Prospects of Use in Aerospace Technics , 1994 .

[19]  Jentung Ku,et al.  A Parametric Study of Performance Characteristics of Loop Heat Pipes , 1999 .

[20]  Stéphane Van Oost,et al.  High Performance Capillary Loop, Operation Mapping and Applications on STENTOR , 1996 .

[21]  K. A. Goncharov,et al.  Thermoregulation of Loops with Capillary Pumping for Space Use , 1992 .