Highly Miniaturized FEEP Propulsion System (NanoFEEP) for Attitude and Orbit Control of CubeSats

Research output: Contribution to book/Conference proceedings/Anthology/Report › Conference contribution › Contributed

Contributors

Details

Original languageEnglish
Title of host publication67th International Astronautical Congress
Place of PublicationGuadalajara, 26-30 Sept.
Number of pages8
Publication statusPublished - 2016
Peer-reviewedNo

External IDs

ORCID /0000-0002-7406-7588/work/172571015

Keywords