COMBUSTION OF COMPOSITE PROPELLANTS WITH TITANIUM

The combustion of 12 composite propellants of the following composition was studied: 60 μ m), 20 D=32-71 μ m and rolled pseudospherical particles of size D= 71- 500 μ m). The burning rates and agglomeration parameters of the metallic component at a pressure of 0.35 MPa in nitrogen and 0.1 MPa in air were determined. It was found that agglomerates of minimum size were formed when using titanium powder with minimum particles size.