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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Bibliographic Details
Main Authors: A Sam Daniel Fenny, Sampathkumar Deepak, Mayekar Nishant B., R Sree Adithya S.
Format: Article
Language:English
Published: EDP Sciences 2024-01-01
Series:MATEC Web of Conferences
Online Access:https://www.matec-conferences.org/articles/matecconf/pdf/2024/05/matecconf_staaar2023_03004.pdf