The cohesive law of particle/binder interfaces in solid propellants

Research output: Book/ReportCommissioned Report

Abstract

Solid propellants are treated as composites with high volume fraction of
particles embedded in the polymeric binder. A micromechanics model
is developed to establish the link between the microscopic behavior of
particle/binder interfaces and the macroscopic constitutive information.
This model is then used to determine the tension/shearing coupled in-
terface cohesive law of a redesigned solid rocket motor propellant, based
on the experimental data of the stress-strain and dilatation-strain curves
for the material under slow rate uniaxial tension.
Original languageEnglish
Place of PublicationMoscow
PublisherTorus Press
Number of pages8
Volume2
Publication statusPublished - 2011

Publication series

NameAdvances in Aerospace Sciences

Fingerprint

Solid propellants
Binders
Micromechanics
Rocket engines
Propellants
Shearing
Volume fraction
Composite materials

Cite this

Tan, H. (2011). The cohesive law of particle/binder interfaces in solid propellants. (Advances in Aerospace Sciences). Moscow: Torus Press.

The cohesive law of particle/binder interfaces in solid propellants. / Tan, Henry.

Moscow : Torus Press, 2011. 8 p. (Advances in Aerospace Sciences).

Research output: Book/ReportCommissioned Report

Tan, H 2011, The cohesive law of particle/binder interfaces in solid propellants. Advances in Aerospace Sciences, vol. 2, Torus Press, Moscow.
Tan H. The cohesive law of particle/binder interfaces in solid propellants. Moscow: Torus Press, 2011. 8 p. (Advances in Aerospace Sciences).
Tan, Henry. / The cohesive law of particle/binder interfaces in solid propellants. Moscow : Torus Press, 2011. 8 p. (Advances in Aerospace Sciences).
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