Kneading time is adjusted to change the dispersibility of nano-CuO in AP/HTPB (Ammonia Perchlorate/Hydroxyl-Terminated Polybutadiene) composite propellants. Nano-CuO/AP is prepared to serve as the other dispersing method of nano-CuO, named predispersing procedure. Several kinds of heat releasing, thermal decomposition by DSC, combustion heat in oxygen environment, and explosion heat in nitrogen environment, are characterized to learn the effect of dispersibility of nano-CuO catalyst on heat releasing of propellants. With pre-dispersing procedures, thermal decomposition temperature of nano-CuO/AP and its propellant are about 25∘C and 8.6∘C lower than that of AP simple mixed with nano-CuO and its propellant, respectively. Comparing propellant...
Thermal decomposition of ammonium perchlorate (AP), as a high energy oxidizer in composite solid roc...
Plateau propellants exhibit burning rate curves that do not follow the typical linear relationship b...
High burn rate propellants help maintain high levels of thrust without requiring complex, high surfa...
permits unrestricted use, distribution, and reproduction in any medium, provided the original work i...
In the present work, an attempt has been made to unveil the effect of micro- and nano-particles of c...
AbstractNano-catalysts containing copper–cobalt oxides (Cu–Co–O) have been synthesized by the citric...
The use of catalytic nanoparticle additives in composite solid propellant as burning rate modifiers ...
<p>Many factors and their mutual interactions induce complexity in the combustion of hydroxyl-termin...
Several industrial- and research-type composite solid propellants containing different nano metric m...
The ignition delay times tign of propellants provide insight for the fundamental understanding of th...
Nano-catalysts are a proven method for increasing the burning rate of propellants, and various synth...
Ammonium-nitrate-(AN-) based composite propellants prepared with a hydroxyl-terminated polybutadiene...
The use of catalytic nanoparticle additives in composite solid propellant as burning rate modifiers ...
Phase-stabilised ammonium nitrate (PSAN) and hydroxyl-terminated polybutadiene (HTPB) are the main i...
This thesis examines the effects of nanoparticle, metal-oxide additives on the burning rate of compo...
Thermal decomposition of ammonium perchlorate (AP), as a high energy oxidizer in composite solid roc...
Plateau propellants exhibit burning rate curves that do not follow the typical linear relationship b...
High burn rate propellants help maintain high levels of thrust without requiring complex, high surfa...
permits unrestricted use, distribution, and reproduction in any medium, provided the original work i...
In the present work, an attempt has been made to unveil the effect of micro- and nano-particles of c...
AbstractNano-catalysts containing copper–cobalt oxides (Cu–Co–O) have been synthesized by the citric...
The use of catalytic nanoparticle additives in composite solid propellant as burning rate modifiers ...
<p>Many factors and their mutual interactions induce complexity in the combustion of hydroxyl-termin...
Several industrial- and research-type composite solid propellants containing different nano metric m...
The ignition delay times tign of propellants provide insight for the fundamental understanding of th...
Nano-catalysts are a proven method for increasing the burning rate of propellants, and various synth...
Ammonium-nitrate-(AN-) based composite propellants prepared with a hydroxyl-terminated polybutadiene...
The use of catalytic nanoparticle additives in composite solid propellant as burning rate modifiers ...
Phase-stabilised ammonium nitrate (PSAN) and hydroxyl-terminated polybutadiene (HTPB) are the main i...
This thesis examines the effects of nanoparticle, metal-oxide additives on the burning rate of compo...
Thermal decomposition of ammonium perchlorate (AP), as a high energy oxidizer in composite solid roc...
Plateau propellants exhibit burning rate curves that do not follow the typical linear relationship b...
High burn rate propellants help maintain high levels of thrust without requiring complex, high surfa...