Burning rate and characterization of hydroxyl terminated natural rubber/isophorone diisocyanate/glycerol propellant composites

Also available in printed version : TL783.3 J85 2014 raf

Bibliographic Details
Main Author:	Juliana Jaafar
Other Authors:	Hussin Mohd. Nor, supervisor
Format:	Master's thesis
Language:	English
Published:	Universiti Teknologi Malaysia 2025
Subjects:	Solid propellant > Mechanical properties Rockets (Aeronautics) > Fuel
Online Access:	https://utmik.utm.my/handle/123456789/54184
Abstract	Abstract here

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