A solid rocket is a high powered solid propellant-driven rocket which has a motor with no movingparts. But mostly, it is used for single use purposes. So, we have designed a high-power solid propulsion rocket SS motor with parachute ejection system. Parachute ejection system refers to usage of parachutes namely, a main parachute, which deploys at the apogee, due to the max apogeerocket tilts and takes instantaneous recordings, and a main parachute which deploys at a preprogrammed altitude. The propellant of the rocket solid fuel which give high thrust ratio and couldlift the rocket at distant apogee. The motor is made up of Stainless steel and nozzle was made up of mild steel. The main aim of this experimental rocket is to ensure that the rocket parts was 3dprinted and ss motor with mild steel nozzle for experimental purposes, this rocket motor can be reuse it again and again. This paper deals with experimental work on rockets and ss motor.

Keywords : High Powered Rocket, Propellant, Deployment, Motor.