Loop heat pipe for spacecraft thermal control, part 2 : Ambient condition tests

Detailed results are presented of two ground-based tests carried out in September 1999 under ambient conditions (room temperature air and atmospheric conditions) to determine the thermal characteristics of loop heat pipes (LHP). One test (test 1) was carried out to quantify the effects that heat leaks have on the operational characteristics of the loop. In test 1, at various evaporator primary input power levels, auxiliary heating was applied to simulate heat leaks into the system. The intentional heat inputs representing heat leaks were located at the liquid return line and the compensation chamber. A second test (test 2) was conducted to verify the feasibility of temperature control of the LHP. Test 2 is motivated by the observation that it is desirable to control the temperature of an LHP to set the operating temperature for the system to which the LHP is attached