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

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...

Ausführliche Beschreibung

Bibliographische Detailangaben
Hauptverfasser: Gligorijević Nikola I., Rodić Vesna Ž., Živković Saša Ž., Pavković Bojan M., Nikolić Momčilo M., Kozomara Stevan M., Subotić Sredoje D.
Format: Artikel
Sprache:English
Veröffentlicht: Association of Chemical Engineers of Serbia 2016-01-01
Schriftenreihe:Hemijska Industrija
Schlagworte:
composite propellant
viscoelasticity
mechanical characterization
tensile strength
ultimate strain
time-temperature shift factor
relaxation modulus
safety factor
reduced time
Online Zugang:http://www.doiserbia.nb.rs/img/doi/0367-598X/2016/0367-598X1500067G.pdf

Online

http://www.doiserbia.nb.rs/img/doi/0367-598X/2016/0367-598X1500067G.pdf

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