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The Measurement of Radar–Plasma Signatures in a Hypersonic Shock Tunnel: Simulation and Experiment

  • Published:2023-12 Issue:6 Volume:59 Page:8581-8597
  • ISSN:0018-9251
  • Container-title:IEEE Transactions on Aerospace and Electronic Systems
  • language:
  • Short-container-title:IEEE Trans. Aerosp. Electron. Syst.

Author:

Petervari René1ORCID,Weidner Stephan2ORCID,Nekris Alexander2ORCID,Brüggenwirth Stefan1ORCID,Knott Peter3ORCID

Affiliation:

1. Cognitive Methods Department, Fraunhofer Institute for High Frequency Physics and Radar Techniques (FHR), Wachtberg, Germany

2. Department of Aerodynamics, Measurements and Simulations, French-German Research Institute of Saint-Louis (ISL), Saint-Louis, France

3. Fraunhofer Institute for High Frequency Physics and Radar Techniques (FHR), Wachtberg, Germany

Funder

French and the German MoD

BAAINBw project

Publisher

Institute of Electrical and Electronics Engineers (IEEE)

Subject

Electrical and Electronic Engineering,Aerospace Engineering

Cited by 1 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Influence of the Atmospheric Plasma Sheath on the RCS of a Hypersonic Reentry Vehicle;2024 18th European Conference on Antennas and Propagation (EuCAP);2024-03-17
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