Add to ORKGAluminum size and loading effects on burning rate of centrifugal accelerated solid propellant
There are many parameters affecting the size and behavior of aluminum (Al) droplets on and near the ...
A one-dimensional model of a gel-fueled rocket combustion chamber has been developed. This model inc...
Several industrial- and research – type fuel rich solid rocket propellants containing nano-metric al...
Instantaneous burning rate data for a polybutadiene acrylic acid propellant, containing 16 weight pe...
The average burning rates of composite solid rocket propellant were measured in acceleration field...
This work was conducted to define further the effects of propellant composition variables on the acc...
Acceleration effects on aluminized composite solid propellants combustion by high speed color cinema...
WOS: 000325647000093The burning rate of the solid rocket propellants is one of the most important fa...
The paper presents a physical-mathematical model for metallized solid propellant combustion under ac...
Instantaneous burning rate data for a polybutadiene acrylic acid propellant, containing 16 weight pe...
Alumina size distributions were obtained for both a coarse and a fine oxidizer composite propellant ...
The functional dependence of acceleration-induced burning-rate augmentation on the magnitude and ori...
S. F. Li, Z. K. Lin, T. F. Wang, Y. L. Sun, X. Han and S. Q. Yuhttp://www.aiaa.org/agenda.cfm?lumeet...
Aluminum combustion in solid propellants generates condensed products leaving the burning surface. T...
Les poudres d'aluminium possèdent des propriétés énergétiques intéressantes et sont couramment intég...
There are many parameters affecting the size and behavior of aluminum (Al) droplets on and near the ...
A one-dimensional model of a gel-fueled rocket combustion chamber has been developed. This model inc...
Several industrial- and research – type fuel rich solid rocket propellants containing nano-metric al...
Instantaneous burning rate data for a polybutadiene acrylic acid propellant, containing 16 weight pe...
The average burning rates of composite solid rocket propellant were measured in acceleration field...
This work was conducted to define further the effects of propellant composition variables on the acc...
Acceleration effects on aluminized composite solid propellants combustion by high speed color cinema...
WOS: 000325647000093The burning rate of the solid rocket propellants is one of the most important fa...
The paper presents a physical-mathematical model for metallized solid propellant combustion under ac...
Instantaneous burning rate data for a polybutadiene acrylic acid propellant, containing 16 weight pe...
Alumina size distributions were obtained for both a coarse and a fine oxidizer composite propellant ...
The functional dependence of acceleration-induced burning-rate augmentation on the magnitude and ori...
S. F. Li, Z. K. Lin, T. F. Wang, Y. L. Sun, X. Han and S. Q. Yuhttp://www.aiaa.org/agenda.cfm?lumeet...
Aluminum combustion in solid propellants generates condensed products leaving the burning surface. T...
Les poudres d'aluminium possèdent des propriétés énergétiques intéressantes et sont couramment intég...
There are many parameters affecting the size and behavior of aluminum (Al) droplets on and near the ...
A one-dimensional model of a gel-fueled rocket combustion chamber has been developed. This model inc...
Several industrial- and research – type fuel rich solid rocket propellants containing nano-metric al...