Static Engine Test on CTN Model Rocket Engine with 1/2 A6-2 Propellant

Solid propellant rocket engines are characterized as the basic model for rocket propellants. They are highly utilized in the industry due to their simplicity and high combustible range. Even though solid rocket engines are widely used, the concept still appears to be lacking for some engineers, hence developing a working prototype of a unique design is proposed. This will help study the advantages and prove the concept of solid rocket engines through visual tests. This paper focuses on the construction of a mini-solid fuel rocket engine, stand test, and the conduction of static test to evaluate the prototype performance and thrust production.