Mechanical characterization of composite solid rocket propellant based on hydroxy-terminated polybutadiene

This paper presents the procedure of uniaxial mechanical characterization of composite solid rocket propellant based on hydroxy-terminated polybutadiene (HTPB), whose mechanical properties strongly depend on temperature, strain rate, natural aging and accumulated damage. A method of process...

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Autors principals:	Gligorijević Nikola I., Rodić Vesna Ž., Živković Saša Ž., Pavković Bojan M., Nikolić Momčilo M., Kozomara Stevan M., Subotić Sredoje D.
Format:	Artigo
Idioma:	Inglês
Publicat:	Association of Chemical Engineers of Serbia 2016-01-01
Col·lecció:	Hemijska Industrija
Matèries:	composite propellant viscoelasticity mechanical characterization tensile strength ultimate strain time-temperature shift factor relaxation modulus safety factor reduced time
Accés en línia:	http://www.doiserbia.nb.rs/img/doi/0367-598X/2016/0367-598X1500067G.pdf
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