A statistical Taguchi L8 matrix was used to conduct a multi-parameter study of the use of nanoscale additives in composite solid propellants. The additives studied were TiO2 (titania) and CeO2 (ceria). The other parameters involved in the experiment were the oxidizer loading and distribution, additive percentage and size, additive size (nano-scale or μm-scale), and the mixing method. Four baseline propellants without additives were also produced for comparison. The propellants were tested from 3.45 to 13.78 MPa in a strand bomb, and burning rate curves were determined for all formulas. By analyzing the Taguchi matrix, the sensitivity of each parameter according to the pressure sensitivity and burning rate of the propellant was calculated. T...
Recent synthesis methods developed by the authors for producing titania premixed in the binder or gr...
The effect of anatase, rutile, and amorphous TiO 2 nanoparticles on the combustion of solid rocket p...
Several industrial- and research-type composite solid propellants containing different nano metric m...
A statistical Taguchi L8 matrix was used to conduct a multi-parameter study of the use of nanoscale ...
Plateau propellants exhibit burning rate curves that do not follow the typical linear relationship b...
This thesis examines the effects of nanoparticle, metal-oxide additives on the burning rate of compo...
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 ability of nano-particle additives to tailor the burning rate of composite solid rocket propella...
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 study presents a comparison of commercially available titania nano-particles produced using ele...
The use of catalytic nanoparticle additives in composite solid propellant as burning rate modifiers ...
Presented in this thesis is a study of the effects of nano-sized particles used as a catalytic addit...
Modern chemical synthesis techniques have allowed for improved incorporation of nano-scale additives...
Recent synthesis methods developed by the authors for producing titania premixed in the binder or gr...
The effect of anatase, rutile, and amorphous TiO 2 nanoparticles on the combustion of solid rocket p...
Several industrial- and research-type composite solid propellants containing different nano metric m...
A statistical Taguchi L8 matrix was used to conduct a multi-parameter study of the use of nanoscale ...
Plateau propellants exhibit burning rate curves that do not follow the typical linear relationship b...
This thesis examines the effects of nanoparticle, metal-oxide additives on the burning rate of compo...
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 ability of nano-particle additives to tailor the burning rate of composite solid rocket propella...
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 study presents a comparison of commercially available titania nano-particles produced using ele...
The use of catalytic nanoparticle additives in composite solid propellant as burning rate modifiers ...
Presented in this thesis is a study of the effects of nano-sized particles used as a catalytic addit...
Modern chemical synthesis techniques have allowed for improved incorporation of nano-scale additives...
Recent synthesis methods developed by the authors for producing titania premixed in the binder or gr...
The effect of anatase, rutile, and amorphous TiO 2 nanoparticles on the combustion of solid rocket p...
Several industrial- and research-type composite solid propellants containing different nano metric m...