Performance, mechanical and thermal properties of double base rocket propellant including copper oxide as burning rate modifier

EXPERIMENTAL AND NUMERICAL INVESTIGATIONS FOR THE COMBUSTION OF SELECTED COMPOSITE SOLID PROPELLANT

Combustion characteristics of extruded nitramine double-base propellants

Burning rate measurement of composite propellant using acoustic wave emission in comparison with other techniques

Experimental Study and Modeling of the Combustion Wave of Metalized Solid Rocket Propellants

Stability of double base propellants, a comparison between classical stability tests and modern analytical techniques

EXPERIMENTAL STUDY OF LAB-SCALE HTPB/GOX HYBRID ROCKET MOTOR

PERFORMANCE AND STABILITY OF MODERN GUN PROPELLANTS

Performance of advanced composite solid rocket propellants based on novel oxidizers

An experimental study on mechanical and ballistic characteristics of different HTPB composite propellant formulations