Combustion of aluminized solid propellants exhibits phenomena associated with accumulation, agglomeration, ignition, and combustion of ultra-fine aluminium particles. In this study, agglomeration phenomenon of ultra-fine aluminium in solid propellant combustion is investigated using quench collection experimental technique over the pressure ranges from 2MPa to 8MPa. The ultra-fine aluminium powder synthesized by Radio Frequency Induction Plasma technique having harmonic mean size of 438nm is used for agglomeration study. The quenching distance is varied from 5mm to 71mm from the propellant burning surface to estimate the effect on agglomerate size. The morphology and chemical compositions of the collected products were then studied by using...
Several industrial- and research – type fuel rich solid rocket propellants containing nano-metric al...
The effects of coated nano-sized aluminum (Al) powder (n-Al) and micron-sized Al powder(g-Al) in pro...
Aluminium is universal and vital constituent in composite propellants and typically used to improve ...
Aluminum combustion in solid propellants generates condensed products leaving the burning surface. T...
Combustion of aluminized solid propellants exhibits phenomena associated with accumulation, agglomer...
The nanosized powders have gained attention to produce materials exhibiting novel properties and for...
The nanosized powders have gained attention to produce materials exhibiting novel properties and for...
Aluminum is a promising metal fuel for solid propellants due to the high heat of combustion and prop...
Aluminized composite propellant used in solid rocket motors contain a lot of aluminium particles bec...
Agglomeration reduction techniques are important field in solid propellant industry, Large agglomera...
Alumina size distributions were obtained for both a coarse and a fine oxidizer composite propellant ...
The currently used micrometric Al powders (30-50 μm nominal size) were replaced by nanometric powde...
An innovative collection methodology based on a recently developed supersonic probe enabled the coll...
Nano-aluminized propellants are investigated and compared with micro-aluminized propellants in order...
Several industrial- and research – type fuel rich solid rocket propellants containing nano-metric al...
The effects of coated nano-sized aluminum (Al) powder (n-Al) and micron-sized Al powder(g-Al) in pro...
Aluminium is universal and vital constituent in composite propellants and typically used to improve ...
Aluminum combustion in solid propellants generates condensed products leaving the burning surface. T...
Combustion of aluminized solid propellants exhibits phenomena associated with accumulation, agglomer...
The nanosized powders have gained attention to produce materials exhibiting novel properties and for...
The nanosized powders have gained attention to produce materials exhibiting novel properties and for...
Aluminum is a promising metal fuel for solid propellants due to the high heat of combustion and prop...
Aluminized composite propellant used in solid rocket motors contain a lot of aluminium particles bec...
Agglomeration reduction techniques are important field in solid propellant industry, Large agglomera...
Alumina size distributions were obtained for both a coarse and a fine oxidizer composite propellant ...
The currently used micrometric Al powders (30-50 μm nominal size) were replaced by nanometric powde...
An innovative collection methodology based on a recently developed supersonic probe enabled the coll...
Nano-aluminized propellants are investigated and compared with micro-aluminized propellants in order...
Several industrial- and research – type fuel rich solid rocket propellants containing nano-metric al...
The effects of coated nano-sized aluminum (Al) powder (n-Al) and micron-sized Al powder(g-Al) in pro...
Aluminium is universal and vital constituent in composite propellants and typically used to improve ...