Rocket Thrust measuring device and method

The present invention provides a thrust measurement device that is similar to an actual launch form of a rocket and capable of precise measurement in a short time in order to obtain continuous data from a moment the rocket is ignited and launched to a moment the launching of the rocket ends, and more specifically provides the thrust measurement method and device for measuring thrust that can definitely perform precise measurement in a short time by deriving an ignition device of a rocket propellant, installation and a structure of a propellant, and the thrust measurement device. In the present invention, a rocket candy (KNSU) is used as a solid fuel, and an indirect ignition device is manufactured using an electric resistance wire to ignite the rocket candy. 본 발명은 로켓이 점화되어 발사되는 순간부터 끝나는 순간까지 연속적인 데이터를 얻기 위해 실제 로켓의 발사 형태와 유사하고 짧은 시간 정밀한 측정이 가능한 추력측정 장치를 제공하는데 있으며, 더 상세하게는 로켓추진체의 점화장치, 추진체의 장착 및 구조, 추력측정장치를 고안함으로서 짧은 시간에 정밀하게 측정되어야 하는 추력측정 방법과 장치를 제공하고자 한다