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Completed TRL 4 (started at 3, targeting 4)
While we have already created an analytical ice growth model, it is based on methods used for growth in air. An extensive literature review has found very little previous work at the conditions specific to the lunar polar ice tanker: very low pressure, low water inlet rates, no carrier gas, and very cold wall temperatures. We plan to conduct one-dimensional ice growth tests in a vacuum chamber to gather data to validate and update our model, and then use the model to design and demonstrate a sub-scale ice tanker in a vacuum chamber.
There are at least four STMD Programs (GCD, ESI, Tipping Point, NIAC) that are actively funding projects to develop either raw resource collection and water extraction components, or water purification, electrolysis, and product liquefaction and storage components, but very little effort is being place on the critical water capture and transport system that will connect the two. IN addition, the Lunar Surface Innovation Initiative strategic plans call for a Polar Water to Ice Demonstration in FY24 - 26, and a Pilot ISRU Consumablel Production System in FY28+. Upon successful demonstration of the Ice Tanker, we will offer up the design and models to any teams proposing to these two potential flight opportunities.
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