We present an approach to on-line monitor the interfacial damages between solid
propellants and carbon fiber reinforced epoxy (CF/epoxy) composites, as well as the
solid propellants themselves. A piezoresistive sensor based on the electric resistance
change ()
of multiwalled carbon nanotubes (MWCNT) is adopted to carry out the in situ
monitoring experiments. The thickness effect of the solid propellant block on the
monitoring performances of the MWCNT sensor is investigated. Meanwhile, the
monitoring results by MWCNT sensors embedded in different positions in
the solid propellants are also considered. With the assist of microscopic
morphology observation, the damage mechanism of the viscoelasticity solid
propellants under various compressive loads is discussed. The relationship between
and
the compressive load-displacement curve is built. The results indicate that the
proposed method is capable of in situ monitoring of the compressive performances of
solid propellants.
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