Authors :
Ankit Kumar
Volume/Issue :
Volume 8 - 2023, Issue 5 - May
Google Scholar :
https://bit.ly/3TmGbDi
Scribd :
https://t.ly/LnaK
DOI :
https://doi.org/10.5281/zenodo.7982428
Abstract :
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.
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.