NASA SBIR 2018-I Solicitation

Proposal Summary

 18-1- Z10.01-1251
 Cryogenic Fluid Management
 Lightweight, Reliable Cryogenic Screen Channel Acquisition Devices with High Expulsion Efficiency
SMALL BUSINESS CONCERN (Firm Name, Mail Address, City/State/Zip, Phone)
Creare, LLC
16 Great Hollow Road
Hanover , NH 03755-3116
(603) 643-3800

Principal Investigator (Name, E-mail, Mail Address, City/State/Zip, Phone)
Weibo Chen
16 Great Hollow Road Hanover, NH 03755 - 3116
(603) 640-2425

Business Official (Name, E-mail, Mail Address, City/State/Zip, Phone)
Robert Kline-Schoder
16 Great Hollow Road Hanover, NH 03755 - 3116
(603) 640-2487
Estimated Technology Readiness Level (TRL) :
Begin: 3
End: 4
Technical Abstract

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’s unique fabrication processes to reliably maintain the pore structure of the screen near its bonding joints with its support frames. Creare’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’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.

Potential NASA Applications

The proposed screen channel technology will enable reliable spacecraft refueling in a microgravity environment. The resulting lightweight LAD will enable reliable cryogenic propellant transfer at high expulsion efficiency, and thus reduce cost of space missions. The technology also has applications as phase separators in two-phase bio and chemical reactors, as well as in fluid management for two-phase flow thermal management and power systems.

Potential Non-NASA Applications

The technology developed in this project has applications in propellant acquisition systems in commercial spacecraft, and gravity-insensitive aircraft fuel supply systems. The capillary structure fabrication technology developed in this program will also have many applications in terrestrial two-phase thermal management systems.

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