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

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

Détails bibliographiques
Auteur principal:	Juliana Jaafar
Autres auteurs:	Hussin Mohd. Nor, supervisor
Format:	Master's thesis
Langue:	anglais
Publié:	Universiti Teknologi Malaysia 2025
Sujets:	Solid propellant > Mechanical properties Rockets (Aeronautics) > Fuel
Accès en ligne:	https://utmik.utm.my/handle/123456789/54184
Abstract	Abstract here

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