Validating a Novel Theoretical Expression for Burn time and Average Thrust in Solid Rocket Motor Design
B. K. Aliyu, C. A. Osheku, E. O. Oyedeji, M. A. L. Adetoro, A. A. Okon & C. M. Idoko · Advances in Research · 2015
A major application of solid propellants is in gun propulsion systems and rockets. The performance of a rocket depends greatly on the design of the solid propellant that meets a specific mission. Performance characteristics such as the burn time, burn rate, average thrust, specif...
Open access
Research Article
10.9734/AIR/2015/18468