1 power at 6500 W ( total system power of 7500 W) , and E11 deprimed when the plate 1 power was increased to 8000 W (total system ... Tests were conducted with a power input of 10 kw in the steady- state , capillary-mode operation, and 50 kw during the transient hybrid-mode. ... The transition between the capillary- mode and the hybrid-mode was made by a simple manual operation of a bypass valve.
|Title||:||Design and testing of a high power spacecraft thermal management system|
|Author||:||Michael E. Mccabe (Jr)|