SOLID PROPELLANT COMPOSITION TO REDUCE INFRARED RAY SIGNAL IN ROCKET PLUME

摘要

The present invention relates to a solid propellant composition used in a solid rocket propulsion system. The solid propellant composition suitably uses a potassium compound in a thermosetting minimum smoke propellant composition to reduce an infrared ray signal radiating from a plume, when burning a propulsion system.;COPYRIGHT KIPO 2016