In this paper, the study was conducted on the thermal properties of thermoplastic binder, Poly Vinyl Chloride(PVC), Vinyl Chloride-Vinyl Acetate Copolymer(VC-VA), Poly Ether Block Amide (PEBAX), that were used to thermoplastic composite propellant.
All solid rocket propellants are divided in two basic classes according to chemical state: homogeneous(double base) and heterogeneous (composite). Today, composite propellants are extensively used as power sources covering the range from gas generat
In a situation that a needs of subminiature guided missile development is being magnified, an unguided missile appled thermoplastic propellant was developed to confirm a possibility of development on subminiature guided missile rocket motor. A requi