Mechanical alloys of Al Mg, AI Zr, Al Ti, Al Li, Al C, Al Mg H, B Mg, B Al, and B Ti were produced and tested for possible applications as high energy density additives to fuels, propellants, explosives, and incendiaries. These new materials are metastable, supersaturated, nanocrystalline solid solutions that include a base metal as a solvent and another component (metal or gas, e.g. hydrogen) as a solute. Phase changes occurring in such materials during ignition and combustion are expected to significantly affect both ignition and bum rates. This experimental program focused on the characterization of ignition kinetics of these alloys. An experimental setup is built around an electrically heated filament coated with the powder of a tested ...
A description of an experimental facility used to determine the ignition and combustion characterist...
The ignition and combustion of Al, Mg, and Al/Mg alloy particles in 99 percent O2/1 percent N2 mixtu...
WOS: 000325647000093The burning rate of the solid rocket propellants is one of the most important fa...
Heating rate effect and particle size effect on ignition temperature of Al powder were studied to co...
A new type of metastable reactive powders for potential use as high energy density materials in prop...
Aluminum added to propellants, explosives, and pyrotechnics, boosts their energy density. Different ...
Metal additives are commonly added to explosives to increase the potential heat release and cause lo...
The thermal processes leading to ignition of metal powders in environments that experience rapid tem...
Metal additives have been widely used in combustion applications such as solid rocket motors and hig...
Though metals and metalloids have been widely considered as reactive fuels, the ability to tune thei...
The use of metal fuel in high-energy materials (HEM) for propulsion is the most energy efficient met...
Aluminum is a promising ingredient for high energy density compositions used in propulsion systems, ...
Agglomeration reduction techniques are important field in solid propellant industry, Large agglomera...
Predictive mechanisms for particle ignition and combustion rates are required in order to develop op...
The study of the ignition characteristics of highenergy materials (HEMs) is important in solving a n...
A description of an experimental facility used to determine the ignition and combustion characterist...
The ignition and combustion of Al, Mg, and Al/Mg alloy particles in 99 percent O2/1 percent N2 mixtu...
WOS: 000325647000093The burning rate of the solid rocket propellants is one of the most important fa...
Heating rate effect and particle size effect on ignition temperature of Al powder were studied to co...
A new type of metastable reactive powders for potential use as high energy density materials in prop...
Aluminum added to propellants, explosives, and pyrotechnics, boosts their energy density. Different ...
Metal additives are commonly added to explosives to increase the potential heat release and cause lo...
The thermal processes leading to ignition of metal powders in environments that experience rapid tem...
Metal additives have been widely used in combustion applications such as solid rocket motors and hig...
Though metals and metalloids have been widely considered as reactive fuels, the ability to tune thei...
The use of metal fuel in high-energy materials (HEM) for propulsion is the most energy efficient met...
Aluminum is a promising ingredient for high energy density compositions used in propulsion systems, ...
Agglomeration reduction techniques are important field in solid propellant industry, Large agglomera...
Predictive mechanisms for particle ignition and combustion rates are required in order to develop op...
The study of the ignition characteristics of highenergy materials (HEMs) is important in solving a n...
A description of an experimental facility used to determine the ignition and combustion characterist...
The ignition and combustion of Al, Mg, and Al/Mg alloy particles in 99 percent O2/1 percent N2 mixtu...
WOS: 000325647000093The burning rate of the solid rocket propellants is one of the most important fa...