Electrolysis propulsion for spacecraft applications
Author(s) -
W. de Groot,
Lynn Arrington,
James F. McElroy,
Fred Mitlitsky,
Andrew H. Weisberg,
Preston Carter,
Blake Myers,
Brian Reed
Publication year - 1997
Publication title -
33rd joint propulsion conference and exhibit
Language(s) - English
Resource type - Conference proceedings
DOI - 10.2514/6.1997-2948
Subject(s) - propulsion , in space propulsion technologies , electrically powered spacecraft propulsion , spacecraft , spacecraft propulsion , testbed , aerospace engineering , ion thruster , engineering , automotive engineering
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 1-N thruster are presented. A concept to integrate a propulsion system and a
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