Evaluation of the Performance Potential of Aerodynamically Thrust Vectored Aerospike Nozzles

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

Contributors

Details

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

External IDs

ORCID /0000-0002-7406-7588/work/172571022

Keywords