Hari Prasath M, Amar GHAR, Honhar GUPTA, Priyanka CHAVAN, Mohammed Ibrahim SUGARNO

DOI Number: XXX-YYY-ZZZ

Conference number: HiSST2024-00210

Understanding plasma behaviour is crucial for designing effective thermal protection systems that withstand extreme heat generated during hypersonic flight. This work revolves around various techniques to quantify the temperature of air plasma using Atomic Emission Spectroscopy (AES) and discusses some interesting observations. Laser Induced Breakdown Spectroscopy (LIBS) is a technique to produce plasma by focusing a laser pulse to high irradiance. A 532 nm Q-switched Nd: YAG laser with a pulse duration of 10 ns and frequency of 10Hz is focused on atmospheric air to induce plasma at various laser powers of 250-500 mW. The plasma emission was captured by an optical spectrometer. The species present in the spectrum are identified using the NIST Atomic Spectra Database and the temperature of the air plasma at the range of different exposure times varying from 2-14 s are estimated. The results are discussed. The electronic temperature estimated using N II lines in the Boltzmann plot method under the assumption of local thermodynamic equilibrium (LTE) are in the order of approximately 37,000-38,000 K. This is a work in progress and further work will be presented at the conference.

Read the full paper here

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.