CREARE LLC — National Aeronautics and Space Administration SBIR Phase I: Z10

Description

<p>Refueling spacecraft in space offers tremendous benefits for increased spacecraft payload capacity and reduced launch cost. However, in a microgravity environment, acquiring vapor-free cryogenic liquid propellants from supply tanks and then transferring them to receiving tanks of a rocket engine is very challenging. To address this challenge, we propose to develop a robust, lightweight cryogenic screen channel Liquid Acquisition Device (LAD) with a novel configuration that is assembled by Creare&rsquo;s unique fabrication processes to reliably maintain the pore structure of the screen near its bonding joints with its support frames. Creare&rsquo;s configuration also provides mechanical support for the screen to withstand launch vibrations. The novel configuration significantly increases the screen area compared to existing screen channels for the same size and mass. Creare&rsquo;s LAD also significantly reduces the liquid holdup inside the screen channel. These features together significantly increase the expulsion efficiency of the LAD. In Phase I, we will demonstrate the feasibility of our approach through designing, fabricating, and testing a proof-of-concept screen channel at cryogenic temperature. In Phase II, we will build and demonstrate a laboratory-scale liquid acquisition device and deliver it to a NASA research lab for further evaluation.</p>