Composite Rocket Propellant

Composite rocket propellant is a solid propulsion material for rocket motors, produced as a heterogeneous mixture combining inorganic oxidisers, such as ammonium perchlorate, and metallic fuel components within an organic binder matrix.

Composite propellants are formed into grains with defined geometries in order to control combustion behaviour and thrust characteristics. They are intended for research, engineering and specialised defence-sector platforms, with mechanical and ballistic properties maintained through modern binding and material-protection technologies.

Transport, storage and use are carried out only in accordance with applicable regulations, approved technical documentation and safety procedures.