THEORETICAL AND PRACTICAL EVALUATION OF BURNING RATE OF DOUBLE BASE ROCKET PROPELLANTS

Burning rate of polyurethane composite propellant with energetic nano-composite additives

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

Performance characteristics of modified HMX-gun propellants

Combustion characteristics of extruded nitramine double-base propellants

PARAMETERS AFFECTING THE EROSIVE BURNING OF SOLID ROCKET MOTOR

Enhancing the propulsion characteristics of rockets by adding the energetic Nitro-hydroxyl-terminated polybutadiene (NHTPB) in the propellant compositions

Effect Of Different Parameters On Tensile Properties Of Polymeric Matrices Used In Composite Solid Rocket Propellant

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

EFFECT OF PACKING PARAMETERS ON THE COMBUSTION BEHAVIOR OF AP BASED COMPOSITE SOLID PROPELLANT