This study investigates the feasibility and performance of a missile propelled by Hybrid Rocket-Based Combined Cycle (HRBCC) engine, which combines hybrid rocket air-breathing engines. The HRBCC engine could enable intra extra-atmospheric hypersonic flight in future. Using bring several advantages as reduced costs, increased reliability simplicity. research presents unique feature developed HyP...

Intake design for supersonic engines, in common with other engineering design problems, is application dependent and the true challenges are in meeting performance targets over the required Mach and Reynolds number ranges while complying with the multitude of constraints imposed by the aircraft/missile and its mission. The fundamentals and limitations of efficient ram compression are well under...

Introduction The latest studies of the overall characteristics of hypersonic flying vehicles with airbreathing engines have shown that these vehicles are fairly promising. Some additional problems arise, however, that are related to the definition of the general shape of the aircraft, the choice of propulsion type and operation regimes, the engine size and position on the aircraft body. There h...

In this work, a new configuration of strut-based scramjet is proposed, and series simulations are conducted to investigate its possibility practical application. The simulation results verified via the classical DLR ramjet an experiment on connected pipe facility. inlet area ( A in </...