Analytical Shaping of a Rocket Nose as a Stage of Preliminary Aerodynamic Modification

The article discusses the problem of a preliminary analytical method for modifying the shape of a rocket’s nose. The purpose of this method is to determine the shape that minimizes aerodynamic drag, in the context of modifying a ballistic missile to incorporate guidance systems. The traditional desi...

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Bibliographic Details
Main Authors: Adrian Szklarski, Robert Głębocki
Format: Article
Language:English
Published: MDPI AG 2025-06-01
Series:Aerospace
Subjects:
Online Access:https://www.mdpi.com/2226-4310/12/7/594
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