Abstract
NASA is examining small fission reactors for future space transportation and surface power applications. The Kilopower system will use a nuclear reactor to supply energy to Stirling convertors to produce electricity. Titanium/water heat pipes will be used to carry the waste heat from the Stirling to a radiator, where the heat is rejected. Most current water heat pipe radiator designs are for surface fission power, and use gravity aided heat pipes (thermosyphons). The Kilopower system will be designed to operate in space, which will require a different heat pipe design than the thermosyphons used in surface applications. The heat pipe design needs to support the Kilopower system through four different operating conditions: operation in space, with zero gravity; operation on earth, with a slight adverse orientation, to estimate performance in space; ground testing, with the heat pipes operating gravity aided; and launch, with the evaporator elevated above the condenser. During the last two conditions, vertical ground testing and launch, the heat pipe wick will deprime and will need to re-prime for operation in space after launch. Two heat pipe wick designs were identified as potential candidates: grooved wick heat pipes and self-venting arterial heat pipes. In the grooved wick design a screen or sintered wick is required in the evaporator during start-up. This hybrid-wick design is necessary to supply liquid to the evaporator during vertical operation. The purpose of the self-venting arterial wick is to provide high performance in a zero gravity environment without de-priming. Grooved wick will not de-prime by nature. Two heat pipes were designed, fabricated and tested: one with self-venting arterial wick and one with a hybrid groove-screen wick. Both heat pipes successfully carried more than the 125 W required power at adverse elevation of 2.5 mm and 5 mm (to simulate operation in space). Repriming after operating as vertical thermosyphons was demonstrated, as was the ability to withstand a single freeze/thaw cycle.
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