This report is concerned with achieving improved combustion of the aluminum ingredient in solid propellant. The approach is to clarify understanding of the complex detailed process exhibited by aluminum and relate them to control of propellant burning rate, combustion stability, combustion efficiency and two phase flow behavior in the motor. A series of experiments were contrived to elucidate the microscopic details of aluminum behavior and their relation to microscopic details of the propellant, and to behavior of the other propellant ingredients. (Author)
Behavior of Aluminum in Solid Propellant Combustion
1982
98 pages
Report
Keine Angabe
Englisch
Rocket Propellants , Combustion & Ignition , Rocket Engines & Motors , Aluminum , Powder metals , Solid rocket propellants , Combustion , Burning rate , Drops , Particle size , Gas flow , Solid propellant rocket engines , Combustion chambers , Agglomerates , Accumulation , Oxides , Control , Stability , Efficiency , Microscopy
Behavior of aluminum in solid propellant combustion
Tema Archiv | 1976
|Aluminum Agglomeration in Solid-Propellant Combustion
AIAA | 1984
|Aluminum agglomeration in solid-propellant combustion
AIAA | 1983
|