Adding nanoparticles as a catalyst to solid propellant fuel to increase and enhance burn rates of the fuel by up to 10 times or more and or modifying the pressure index. A preferred embodiment uses titanium dioxide nanoparticles mixed with a solid propellant fuel, where the nanoparticles are approximately 2% or less of total propellant mixture. The high surface to volume ratio of the nanoparticles improve the performance of the solid propellant fuel
The ability of nano-particle additives to tailor the burning rate of composite solid rocket propella...
Presented in this thesis is a study of the effects of nano-sized particles used as a catalytic addit...
A statistical Taguchi L8 matrix was used to conduct a multi-parameter study of the use of nanoscale ...
Adding nanoparticles as a catalyst to solid propellant fuel to increase and enhance burn rates of th...
Adding nanoparticles as a catalyst to solid propellant fuel to increase and enhance burn rates of th...
The effect of anatase, rutile, and amorphous TiO2 nanoparticles on the combustion of solid rocket pr...
The effect of anatase, rutile, and amorphous TiO 2 nanoparticles on the combustion of solid rocket p...
Advancements in chemical synthesis techniques allow for the production of improved solid rocket prop...
The use of catalytic nanoparticle additives in composite solid propellant as burning rate modifiers ...
This thesis examines the effects of nanoparticle, metal-oxide additives on the burning rate of compo...
Recent synthesis methods developed by the authors for producing titania premixed in the binder or gr...
Recent advancements in chemical synthesis techniques have allowed for the production of improved sol...
Plateau propellants exhibit burning rate curves that do not follow the typical linear relationship b...
The use of catalytic nanoparticle additives in composite solid propellant as burning rate modifiers ...
Plateau propellants exhibit burning rate curves that do not follow the typical linear relationship b...
The ability of nano-particle additives to tailor the burning rate of composite solid rocket propella...
Presented in this thesis is a study of the effects of nano-sized particles used as a catalytic addit...
A statistical Taguchi L8 matrix was used to conduct a multi-parameter study of the use of nanoscale ...
Adding nanoparticles as a catalyst to solid propellant fuel to increase and enhance burn rates of th...
Adding nanoparticles as a catalyst to solid propellant fuel to increase and enhance burn rates of th...
The effect of anatase, rutile, and amorphous TiO2 nanoparticles on the combustion of solid rocket pr...
The effect of anatase, rutile, and amorphous TiO 2 nanoparticles on the combustion of solid rocket p...
Advancements in chemical synthesis techniques allow for the production of improved solid rocket prop...
The use of catalytic nanoparticle additives in composite solid propellant as burning rate modifiers ...
This thesis examines the effects of nanoparticle, metal-oxide additives on the burning rate of compo...
Recent synthesis methods developed by the authors for producing titania premixed in the binder or gr...
Recent advancements in chemical synthesis techniques have allowed for the production of improved sol...
Plateau propellants exhibit burning rate curves that do not follow the typical linear relationship b...
The use of catalytic nanoparticle additives in composite solid propellant as burning rate modifiers ...
Plateau propellants exhibit burning rate curves that do not follow the typical linear relationship b...
The ability of nano-particle additives to tailor the burning rate of composite solid rocket propella...
Presented in this thesis is a study of the effects of nano-sized particles used as a catalytic addit...
A statistical Taguchi L8 matrix was used to conduct a multi-parameter study of the use of nanoscale ...