Double Stage Hall Effect Thruster Development Activities at SNECMA Moteurs

Details Double Stage Hall Effect Thruster Development Activities at SNECMA Moteurs Double Stage Hall Effect Thruster Development Activities at SNECMA Moteurs

Oct 2004

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=2004esasp.555e..33p&link_type=abstract

Proceedings of the 4th International Spacecraft Propulsion Conference (ESA SP-555). 2-9 June, 2004, Chia Laguna (Cagliari), Sard

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To prepare the development of future versatile thrusters Snecma Moteurs is currently involved in technological research activities on Double Stage Hall Effect Thruster. This concept is based on the separation of the two main functions in Hall effect thrusters : ionisation is performed in the first stage while acceleration is achieved in a second stage. First promising results obtained with different prototypes DSHET using magnetic ionisation stage are presented as well as the design of a 3kW prototype intended to consolidate the concept and confirm these promising characteristics in cryogenic vacuum conditions.

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