Maximizing Side Force Generation in Aerospike Nozzles for Attitude and Trajectory Control

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

Contributors

Details

Original languageUndefined
Title of host publication69th International Astronautical Congress
Place of PublicationBremen, 1-5 Oct.
Publication statusPublished - 2018
Peer-reviewedNo

External IDs

ORCID /0000-0002-7406-7588/work/172571047

Keywords