Development and Numerical validation of an Aerospike nozzle Contour Design
Sam Daniel Fenny A,
Deepak Sampathkumar,
Nishant B. Mayekar
et al.
Abstract: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 of overall performance. This study analyses the development and flow analysis of an aerospike nozzle at sea level, validating their results by taking into account currently used bell nozzles. The flow over the aeros… Show more
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