CHLOE BERENGUER; KONSTANTINOS KATSONIS

DOI Number: 10.13009/EUCASS2023-004

4CDGM, a volume averaged detailed global model with the four initial components 0, 02 , N, N2 can analyse the functioning of air-breathing electric thrusters to foresee the plasma constitution and to diagnose it by OES. 4CDGM may also evaluate the atmospheric remnants in altitudes exceeding the Karman line set in about 100 km altitude on the basis of existing empirical models. In order to support air-breathing thrusters, 4CDGM provides Plasma Component Composition diagrams, Functioning Diagrams and also theoretical spectra emission line intensities, thus allowing for OES diagnostics. Such diagrams and theoretical spectra are presented and discussed herewith.

Read the full paper here

In Categories: 1. Aerospace Europe Conference 2023, 1.Events, 10. Propulsion Physics
Email
Print
LinkedIn
The paper above was part of  proceedings of a CEAS event and as such the author has signed a publication agreement to have their paper published in the repository. In the case this paper is found somewhere else CEAS always links to the other source.  CEAS takes great care in making the correct content available to the reader. If any mistakes are found  in the listings please contact us directly at papers@aerospacerepository.org and we will correct the listing promptly.  CEAS cannot be held liable either for mistakes in editorial or technical aspects, nor for omissions, nor for the correctness of the content. In particular, CEAS does not guarantee completeness or correctness of information contained in external websites which can be accessed via links from CEAS’s websites. Despite accurate research on the content of such linked external websites, CEAS cannot be held liable for their content. Only the content providers of such external sites are liable for their content. Should you notice any mistake in technical or editorial aspects of the CEAS site, please do not hesitate to inform us.