Brine de-watering is the final unit operation required to close the water cycle for life support aboard spacecraft. Though no such system has been demonstrated in space to date, numerous methods have been proposed and developed to various degrees. In this Phase I effort we propose to develop a versatile microgravity-compatible brine de-watering method that exploits the Brine Residual in Containment (BRIC) approach. The system is essentially passive, employing the combined effects of surface tension, wetting, and system geometry to drive and stably support the fluids involved. Our approach balances performance with simplicity, the latter which leads to a safe, clean, low-cost, fast-to-flight device with high probability of success. The broad solution approach is expected to be tolerant of pretreatments, contaminates, particulates, and widely varying input feed lines. Preliminary data suggests that the compact and lightweight approach requires only ~0.02kg of disposable support material for ~1L (~1.8 kg) of solid brine produced, and that maintenance expectations are as low as 30 minutes per 50 days per crew member. Our Phase I deliverable is a low-g drop tower-demonstrated prototype with a clear plan for rapid construction and flight qualification of a flight version for verification and validation aboard the International Space Station.