Development and Testing of a Low-Current Applied-Field Magnetoplasmadynamic Thruster with a Rectangular Discharge Channel

Research output: Contribution to book/Conference proceedings/Anthology/ReportConference contributionContributed

Contributors

Details

Original languageEnglish
Title of host publication37th International Electric Propulsion Conference
Place of PublicationJune 19-23
Publication statusPublished - 2022
Peer-reviewedNo

External IDs

ORCID /0000-0002-7406-7588/work/172571114

Keywords