Open AccessDesign Optimization of Propellant Grain and Nozzle Contour to Improve Performance of Solid Rocket Propulsion
Author(s) -
Muhammad Ihsan Abyan,
Aang Nuryaman,
Bagus Hayatul Jihad,
Soleh Fajar Junjunan,
Asmiati Asmiati
Publication year - 2022
Publication title -
journal of engineering and technological sciences
Language(s) - English
Resource type - Journals
SCImago Journal Rank - 0.202
H-Index - 14
eISSN - 2338-5502
pISSN - 2337-5779
DOI - 10.5614/j.eng.technol.sci.2022.54.5.8
Subject(s) - propellant , aerospace engineering , specific impulse , solid fuel rocket , rocket (weapon) , nozzle , propulsion , spacecraft propulsion , missile , rocket propellant , rocket engine nozzle , characteristic velocity , engineering , liquid propellant rocket , aeronautics , automotive engineering
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