Tailoring the plateau burning rates of composite propellants by the use of nanoscale additives

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dc.contributor.advisor Petersen , Eric en_US
dc.contributor.committeeMember Cizmas , Paul en_US
dc.creator Stephens , Matthew Aaron en_US
dc.date.accessioned 2010 -01 -15T00 :06 :19Z
dc.date.accessioned 2014 -02 -19T19 :34 :50Z
dc.date.available 2010 -01 -15T00 :06 :19Z
dc.date.available 2014 -02 -19T19 :34 :50Z
dc.date.created 2008 -12 en_US
dc.date.issued 2009 -05 -15 en_US
dc.identifier.uri http : / /hdl .handle .net /1969 .1 /ETD -TAMU -3202
dc.description.abstract Composite propellants are composed of a solid oxidizer that is mixed into a hydrocarbon binder that when polymerized results in a solid mass capable of self -sustained combustion after ignition . Plateau propellants exhibit burning rate curves that do not follow the typical linear relationship between burning rate and pressure when plotted on a log -log scale , and because of this deviation their burning behavior is classified as anomalous burning . It is not unusual for solid -particle additives to be added to propellants in order to enhance burning rate or other properties . However , the effect of nano -size solid additives in these propellants is not fully understood or agreed upon within the research community . The current project set out to explore what possible variables were creating this result and to explore new additives . This thesis contains a literature review chronicling the last half -century of research to better understand the mechanisms that govern anomalous burning and to shed light on current research into plateau and related propellants . In addition to the review , a series of experiments investigating the use of nanoscale TiO2 -based additives in AP -HTPB composite propellants was performed . The baseline propellant consisted of either 70 % or 80 % monomodal AP (223 ?m ) and 30 % or 20 % binder composed of IPDI -cured HTPB with Tepanol . Propellants ? burning rates were tested using a strand bomb between 500 and 2500 psi (34 .0 -170 .1 atm ) . Analysis of the burning rate data shows that the crystal phase and synthesis method of the TiO2 additive are influential to plateau tailoring and to the apparent effectiveness of the additive in altering the burning rate of the composite propellant . Some of the discrepancy in the literature regarding the effectiveness of TiO2 as a tailoring additive may be due to differences in how the additive was produced . Doping the TiO2 with small amounts of metallic elements (Al , Fe , or Gd ) showed additional effects on the burning rate that depend on the doping material and the amount of the dopant . en_US
dc.format.medium electronic en_US
dc.format.mimetype application /pdf en_US
dc.language.iso en _US en_US
dc.subject Solid Propellant en_US
dc.title Tailoring the plateau burning rates of composite propellants by the use of nanoscale additives en_US
dc.type Book en
dc.type.genre Electronic Thesis en_US
dc.type.material text en_US
dc.format.digitalOrigin born digital en_US


Tailoring the plateau burning rates of composite propellants by the use of nanoscale additives. Available electronically from http : / /hdl .handle .net /1969 .1 /ETD -TAMU -3202 .

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