31 Jul Phoebe Wall
Improving spacecraft heat pipes and other capillarity-driven flows with triangular features In a microgravity environment, capillary forces dominate the behavior of liquids. I have experience conducting capillary action experiments using 2 seconds of microgravity in a drop tower. However, in suborbital flight, I could utilize microgravity on the order of minutes rather than seconds. My research shows that adding triangular cavities to heat pipes could improve spacecraft heat transfer systems. However, I have only proposed this through mathematical analysis of liquid behavior. To fully prove the benefit of triangular features, I would conduct a longer experiment on a suborbital flight that tests heat pipe designs with my proposed modifications, directly measuring their rate of heat transfer. The objective of this experiment is to improve the heat pipe design currently used on the ISS by determining the shape and size of the triangular feature most beneficial to heat transfer. To conduct this experiment, heat pipes will be flown on a suborbital spacecraft (a minimum of three heat pipes, a maximum determined by size constraints). One heat pipe will replicate the design used on the ISS. The remaining will be identical to this control except for the addition of triangular cavities. Triangles’ shapes and sizes will vary per heat pipe. The coolant will enter the pipes upon the start of the microgravity environment with a simple mechanism controlled by an Arduino. Each heat pipe will be in a thermodynamically isolated box and surrounded by hot air. A temperature probe will record the temperature inside each box...