Empirical Research of Impulse Generation and Detecting the Motion of Rocket Body using Smart Ignition System

A rocket is a missile, spacecraft, aircraft that acquires thrust from a rocket engine. Rocket engine consists of chemical propellant that is used to get the moment in the rocket. The process to ignite this chemical propellant is done using various methods in the rocket science. Rocket engines work by action and reaction of the mixture present in it, by the igniting this mixture the pressure and impulse is produced in the rocket engine, due to this pressure and impulse moment is occurred in body of the rocket and it moves forward with a certain speed. In the proposed system the chemical propulsion mixture ratio is of 65:30:5 i.e KNO3: C12H22O11:K2S+N2+3CO2(Potassium Nitrate: Powdered Sugar: Black Powder). The black powder is the combination of one oxidizer and two fuels - Potassium nitrate (oxidizer),Sulfur and Carbon (fuels). Using this chemical propellant the estimated target to fly is about 200 meters from ground. We compared this proposed method with the preferred algorithms to verify the effectiveness and pretense of this method. The result show that the proposed data processing and prediction method can achieve performance. This project is about the way of igniting the rocket engine using smart ignition technique and also producing the moment in the body of the rocket by generating impulse.