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Study On The Processing And Application Of GAP Modified Single Base Spherical Propellant

Posted on:2020-10-17Degree:MasterType:Thesis
Country:ChinaCandidate:G Z ZhaoFull Text:PDF
GTID:2381330575453197Subject:Ordnance Science and Technology
Abstract/Summary:PDF Full Text Request
In order to improve the energy performance of single-base spherical propellant,the energy-containing binder polyazide glycidyl azide polymer?GAP?was added into the single-base spherical propellant by internal solution method to obtain the GAP modified single-base spherical propellant.The influence of various process parameters on the rotundness,particle size and density of the spherical propellant was explored.Butyl-nitroxyethyl nitramine?BuNENA?is used as a plasticizer,isophorone diisocyanate?IPDI?and dipropynyl succinate?BPS?are used as curing agents.GAP modified spherical propellant film was prepared by the polyurethane reaction and the 1,3-dipolar cycloaddition reaction,respectively.The isocyanate reaction system?polyurethane reaction?curing parameters RIPDIPDI and non-isocyanate reaction system?1,3-dipolar cycloaddition?curing parameters RBPSPS were studied in the double-curing system.And the influence of different solid additives?graphene,carbon fiber and activated carbon fiber?on film properties were explored.The effect of process parameters on the density of GAP spherical propellant was studied by the density bottle method.It was found that when the nitrocellulose nitrogen content,the dehydrating agent content,the amount of pre-exclude solvent and the formed temperature of the GAP spherical propellant increased,the density of the spherical propellant increased.When the GAP content increased,the density of the spherical propellant decreased.The particle size of the spherical propellant was studied.It was found that the concentration of surfactant,the amount of pre-exclude solvent and the formed temperature of the spherical propellant increased,and the particle size of the spherical propellant decreased.The morphology of the spherical propellant was studied by electron microscopy.As the nitrocellulose nitrogen content increased,there were more irregular particles;the GAP content increased,the surface of the spherical propellant turned rougher,and the optimal forming temperature for spherical propellant is 60°C.The GAP modified film was characterized by infrared spectrometer.It was found that the polyurethane and 1,3-dipolar cycloaddition reaction occurred in this GAP modified film.The thermal decomposition properties of this film were studied by differential scanning calorimetry?DSC?method.The results showed that the peak temperature of different formula films was about 20°C lower than that of C#NC.With the RIPDI increased,the apparent activation energy?Ea?and the pre-exponential factor?A?decreased first and then increased.With the RBPSPS increased,Ea and A increased first and then decreased.The static tension test showed that when the RIPDI=1,the maximum tension strength?max of the sample increased with the RBPSPS increased.When RBPS=0,the maximum elongation?max of the films reached the maximum value?173%?.And when RBPS=0.5,the?max was the lowest value?15.24%?;When RBPS=1,as the RIPDI increased,the value of?max for the films decreased.When RIPDI=0.5,?max reached the maximum value?22.59%?,and when RIPDI=1.25,?max got the lowest value?19.71%?.When solied additives,such as graphene,carbon fiber and activated carbon fiber,were added into the GAP modified film,the tension strength of the film can be greatly improved,but the value of elongation is lower.The tested results of linear thermal expansion coefficient showed that when RIPDI=1,the linear thermal expansion coefficient of film decreased with RBPS increased;when RBPS=1,the linear thermal expansion coefficient of this film increases slightly with the RIPDI increased.When activated carbon fiber,carbon fiber and graphene were added into the samples,the change of linear thermal expansion coefficient was unconspicuous.
Keywords/Search Tags:polyazide glycidyl ether (GAP), Single Base Spherical propellant, preparation process, linear thermal expansion coefficient, mechanical property
PDF Full Text Request
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