z-logo
open-access-imgOpen Access
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

The content you want is available to Zendy users.

Already have an account? Click here to sign in.
Having issues? You can contact us here
Accelerating Research

Address

John Eccles House
Robert Robinson Avenue,
Oxford Science Park, Oxford
OX4 4GP, United Kingdom