Ramjet fuel studies. Part 2. Aluminum, boron, and boron carbide. Technical publication, Jul 1970--Jun 1972
G. W. Burdette, James T. Bryant
Abstract
G. W. Burdette, James T. Bryant
Abstract
Stable suspensions of aluminum and boron carbide in various hydrocarbons have been prepared for use as ramjet fuels. Many chemical and physical properties of these suspensions related to Navy storable propellant criteria were measured. Total burning times for concentrated dust flames of carbon, boron, boron carbide, and aluminum at atmospheric pressure are examined and compared. The implications of these rates with respect to the combustion efficiencies of gelled fuels in ramjet missiles are discussed. (Author) (GRA)
A significance statement is not available in the OpenAlex record.
A contribution statement is not available in the OpenAlex record.
Method details are not available in the OpenAlex metadata.
Findings are not separately available in the OpenAlex metadata.
Limitations are not available in the OpenAlex metadata.
Application details are not available in the OpenAlex metadata.
Stable suspensions of aluminum and boron carbide in various hydrocarbons have been prepared for use as ramjet fuels. Many chemical and physical properties of these suspensions related to Navy storable propellant criteria were measured. Total burning times for concentrated dust flames of carbon, boron, boron carbide, and aluminum at atmospheric pressure are examined and compared. The implications of these rates with respect to the combustion efficiencies of gelled fuels in ramjet missiles are discussed. (Author) (GRA)
Key concepts: Boron carbide, Ramjet, Boron, Combustion, Propellant, Materials science, Carbide, Aluminium