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Performance of a Regenerative Fuel Cell System for the Lunar SurfaceRegenerative fuel cells (RFCs) are an attractive energy storage solution for lunar missions as a technology capable of providing a higher specific energy (i.e., W∙h/kg) than state-of-the-art packaged Li-ion battery systems. An RFC consists of the (1 & 2) electrochemical stacks (chemical to electrical energy conversion to supply electricity to an external load, i.e. the fuel cell reaction, and electrical to chemical energy conversion of supplied electrical power to dissociate water into hydrogen and oxygen gases, i.e. water electrolysis), (3) fluidic conditioning, (4) reactant storage, (5) avionics, (6) power management and distribution (PMAD), and (7) thermal management.
NASA’s Glenn Research Center has designed, assembled, and tested a breadboard RFC sys-tem capable of operating autonomously for multiple simulated lunar day/night cycles in a laboratory environment.
The system is comprised of a non-flow through proton exchange membrane (PEM) fuel cell stack and a liquid-anode feed PEM electrolyzer (EZ) stack designed to electrochemically compress the reactants at balanced pressures up to 12.4 MPa (1800 psia). The fluidic conditioning, avionics, PMAD, and thermal management sub-systems are largely comprised of commercial-off-the-shelf components for this system-level development effort. The hardware is controlled by a CubeSat space processor running an operational program based on core flight architecture that can control the RFC hardware autonomously through a state machine with fault monitoring.
The testing results highlighted here were completed with the system in an open-loop configuration such that reactants generated through water electrolysis were vented while gas cylinders supplied fuel cell operation. The breadboard operated autonomously, but there were five unplanned transitions to a safe state that required a manual restart after reviewing the data, determining a root cause, and implementing a solution. Four of the transitions were caused by the thermal management subsystem and the fifth was caused by a water management control issue in the EZ sub-system. The RFC system operated for over 550 hours with the final cycle being slightly abbreviated due to reasons unrelated to system performance.
Document ID
20260002731
Acquisition Source
Glenn Research Center
Document Type
Poster
Authors
Kerrigan Cain
(Glenn Research Center Cleveland, United States)
Phillip Smith
(Glenn Research Center Cleveland, United States)
Devon Powers
(HX5, LLC)
Mat McCaskey
(HX5, LLC)
Jessica Cashman
(Glenn Research Center Cleveland, United States)
Ryan Grotenrath
(Glenn Research Center Cleveland, United States)
Chris Heldman
(Glenn Research Center Cleveland, United States)
Ian Jakupca
(Glenn Research Center Cleveland, United States)
Date Acquired
April 3, 2026
Subject Category
Lunar and Planetary Science and Exploration
Meeting Information
Meeting: Lunar Surface Innovation Consortium (LSIC) Spring Meeting
Location: Laurel, MD
Country: US
Start Date: April 28, 2026
End Date: April 30, 2026
Sponsors: Johns Hopkins University Applied Physics Laboratory
Funding Number(s)
WBS: 328085.07.01.04.22
Distribution Limits
Public
Copyright
Public Use Permitted.
Technical Review
Single Expert
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