NASA NTRS · 19970041522
Electrolysis Propulsion for Spacecraft Applications
Abstract
Electrolysis propulsion has been recognized over the last several decades as a viable option to meet many satellite and spacecraft propulsion requirements. This technology, however, was never used for in-space missions. In the same time frame, water based fuel cells have flown in a number of missions. These systems have many components similar to electrolysis propulsion systems. Recent advances in component technology include: lightweight tankage, water vapor feed electrolysis, fuel cell technology, and thrust chamber materials for propulsion. Taken together, these developments make propulsion and/or power using electrolysis/fuel cell technology very attractive as separate or integrated systems. A water electrolysis propulsion testbed was constructed and tested in a joint NASA/Hamilton Standard/Lawrence Livermore National Laboratories program to demonstrate these technology developments for propulsion. The results from these testbed experiments using a I-N thruster are presented. A concept to integrate a propulsion system and a fuel cell system into a unitized spacecraft propulsion and power system is outlined.
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deGroot, Wim A., Arrington, Lynn A., McElroy, James F., Mitlitsky, Fred, Weisberg, Andrew H., Carter, Preston H., II, Myers, Blake, Reed, Brian D.. 1997-10-01. Electrolysis Propulsion for Spacecraft Applications. https://ntrs.nasa.gov/citations/19970041522
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