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Development and Numerical validation of an Aerospike nozzle Contour Design

Aerospike nozzle simplified design and analysis, as well as test results, are presented. New techniques in nozzle design have been used to improve the performance of current rocket engines. The use of an aerospike nozzle is one such technique. It outperforms the existing proven bell nozzle in terms...

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Hlavní autoři: A Sam Daniel Fenny, Sampathkumar Deepak, Mayekar Nishant B., R Sree Adithya S.
Médium: Artigo
Jazyk:Inglês
Vydáno: EDP Sciences 2024-01-01
Edice:MATEC Web of Conferences
On-line přístup:https://www.matec-conferences.org/articles/matecconf/pdf/2024/05/matecconf_staaar2023_03004.pdf
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