The capillary pumped loop (CPL) is a state-of-the-art technique for cooling
of spacecraft and telecommunication devices. It provides substantially hig
her cooling capacity than most heat pipes, more flexibility of installation
, and much greater distance of heat transport because of the small diameter
of wickless transport lines. Major disadvantages of the CPL are long and c
omplicated startup procedures and the possibility of deprime at high heat i
nput or load variation, The present work was an experimental study to chara
cterize the start-up process for an electrohydrodynamically (EHD) assisted
CPL system. Startup is achieved by establishing stable differential pressur
e and average temperature at the evaporator wall. When an electric field is
applied to the evaporator wick, the liquid-vapor separation, the EHD pumpi
ng, and the instability-induced Maxwell stresses collectively contribute to
reduce the startup time, as well as provide substantial improvement in CPL
thermal performance. The experimental data in the present study show that
at a power level of 10 W, the EHD can reduce the startup time by as much as
50% at an applied voltage of 10 kV. A similar trend is observed at power l
evels of 20 and 50 W.