Evaluation of the Performance Potential of Aerodynamically Thrust Vectored Aerospike Nozzles

Research output: Contribution to book/conference proceedings/anthology/report › Conference contribution › Contributed

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Details

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

Keywords