- Introduction
The proposed project will be divided into three main stages. The first phase of research will be aimed on preparation
of cast composite rocket propellants based on ammonium perchlorate and HTPB (hydrox terminated polybutadiene) as a binder.
The second phase of the project will be focused on the preparation of pressed composite propellants based on thermoplastics
polymers (Kraton, Estane etc.) as a binder. Burning rate of those propellants will be measured at a atmospheric pressure.
We suppose utilization of those propellants in the car and aircraft emergency systems. The third phase of the project
will be aimed on the preparation of silicone propellants with their using in the temperature range from -100 up to +100 °C.
of cast composite rocket propellants based on ammonium perchlorate and HTPB (hydrox terminated polybutadiene) as a binder.
The second phase of the project will be focused on the preparation of pressed composite propellants based on thermoplastics
polymers (Kraton, Estane etc.) as a binder. Burning rate of those propellants will be measured at a atmospheric pressure.
We suppose utilization of those propellants in the car and aircraft emergency systems. The third phase of the project
will be aimed on the preparation of silicone propellants with their using in the temperature range from -100 up to +100 °C.
