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Temperature dependence of high strain-rate impact fracture behaviour in highly filled polymeric composite and plasticized thermoplastic propellants
Authors:S Y Ho  C W Fong
Affiliation:(1) Defence Science and Technology Organization, Weapons Systems Research Laboratory, Defence Research Centre Salisbury, GPO Box 2151, 5001 Adelaide, South Australia, Australia
Abstract:The effect of temperature and strain-rate on the fracture behaviour during high strain-rate (sim 103 sec–1) impact of two highly filled polymeric composite propellants (containing segmented polyurethanes based on hydroxy-term inated polybutadiene (HTPB) or glycidyl azide polymer (GAP) filled with ammonium perchlorate (AP) particles) and a plasticized thermoplastic (cast double base (CDB) nitrocellulose-nitroglycerine) propellant have been examined over a wide temperature range encompassing the rtimesittle-ductilerdquo transition. In the ldquoelasticrdquo region of the loaddisplacement curve, the yield stress and fracture toughness is highest for GAP/AP and lowest for HTPB/AP. In the ldquoelasticrdquo and post-yield ldquoductilerdquo regions CDB is more fracture-resistant than GAP/AP and HTPB/AP over the temperature range –20 to 50° C, but below –40° C, where both CDB and GAP/AP are brittle, GAP/AP is more fracture-resistant than CDB (as observed in the ldquoelasticrdquo region). Although all the propellants are known to develop small cracks in the ldquoelasticrdquo and post-yield ldquoductilerdquo regions of the load-displacement curve, the overall fracture behaviour is largely governed by viscoelastic properties (because the cracks close up in compression). The good mechanical properties of CDB, above the ldquobrittle-ductilerdquo transition temperature, can be attributed to the presence of a largebeta-transition loss peak. In the composites, the fracture behaviour is also influenced to a lesser extent by the degree of filler-binder interactions. Dynamic mechanical analysis indicates that GAP/AP has a slightly higher degree of filler-binder interactions than HTPB/AP. A temperature-strain rate reduction has been obtained for the yield stress and the composite curve can be expressed by the equation sgry =K 1 +K 2 log (Gdotea T ) whereK 1 andK 2 are constants anda T is a shift factor.K 2 is a material constant which reflects the temperature and strain-rate sensitivity.
Keywords:
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