Design and Analysis of Nozzle Exit Area for Science Technology Engineering and Mathematics (STEM) Based Solid Rocket Propellant.

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Bibliographic Details
Title: Design and Analysis of Nozzle Exit Area for Science Technology Engineering and Mathematics (STEM) Based Solid Rocket Propellant.
Authors: Rahimi, Muhammad Fadhli Hairi Abd1, Ariffin, Ahmad Hamdan1, ahmadh@uthm.edu.my
Source: Progress in Aerospace & Aviation Technology (PAAT); 2025, Vol. 5 Issue 2, p8-16, 9p
Database: Applied Science & Technology Source
Description
ISSN:28212924
DOI:10.30880/paat.2025.05.02.002