Dehydration Resistant And Dimensionally Stable High Performance Membrane

Award Information
Agency: National Aeronautics and Space Administration
Branch: N/A
Contract: 80NSSC18P1941
Agency Tracking Number: 186312
Amount: $124,675.00
Phase: Phase I
Program: SBIR
Solicitation Topic Code: H1
Solicitation Number: SBIR_18_P1
Timeline
Solicitation Year: 2018
Award Year: 2018
Award Start Date (Proposal Award Date): 2018-07-27
Award End Date (Contract End Date): 2019-02-15
Small Business Information
89 Rumford Avenue, Newton, MA, 02466-1311
DUNS: 066594979
HUBZone Owned: N
Woman Owned: N
Socially and Economically Disadvantaged: N
Principal Investigator
 Chao Lei
 (781) 529-0567
 clei@ginerinc.com
Business Contact
 Meagan Rich-Emar
Phone: (781) 529-0506
Email: mrich@ginerinc.com
Research Institution
N/A
Abstract

In several technologies within NASA’s In Situ Resource Utilization (ISRU) systems, such as fuel cell, water electrolysis and gas/water separations etc., polymeric membranes, especially proton exchange membranes (PEM), play an important role. These membranes are generally hygroscopic, subject to swelling in the presence of humidity or water. When restrained membranes undergo a hydration/dehydration changes, stresses are then generated which can lead to membrane failure. Given the harsh surface environmental conditions on the moon and Mars, more dehydration resistant and dimensionally stable PEM materials are highly desirable for better performance and durability and to allow for long term dry storage and delivery of ISRU systems.

Giner herein proposes to create a reinforced proton exchange membrane using a low equivalent weight (EW) short-side-chain (SSC) ionomer and Giner’s Dimensionally Stable Membranes®™ (DSM) matrix support. In this design, the DSM support is filled with low EW SSC PFSA ionomers. With the added strength inherent in the DSM support, these PEMs can be made thinner and be impregnated with a high-acid-content low EW ionomer to improve the water retention and maintain excellent dimensional stability. Our proposed design has multiple advantages to address the dehydration issues for NASA applications and is expected to achieve improved performance and reduced cost. The water retention property will be greatly enhanced by using a low EW SSC ionomer compared to Nafion. The other associated properties, e.g. protonic conductivity, dimensional stability, wet-dry cycling durability, and freeze/thaw thermal cycling durability are expected to improve significantly as well. In addition, our design has a more cost effective fabrication and ease of scaling up than Gore-Select membrane using e-PTFE support and other nanofiber electrospinning methods.

* Information listed above is at the time of submission. *

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