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

Research output: Contribution to journalResearch articleContributedpeer-review

Contributors

Details

Original languageEnglish
Pages (from-to)422-428
Number of pages7
JournalActa astronautica
Volume144
Publication statusPublished - 2018
Peer-reviewedYes

External IDs

Scopus 85041428598
ORCID /0000-0002-7406-7588/work/172570963

Keywords