This improves the engine’s thrust-to-weight ratio, lowers expenses, and streamlines the engine’s structure. The engine’s ...

SABRE-Nozzle will design an additive manufactured nozzle that is capable of accelerating exhaust from the P90-RXi JetCat engine to supersonic conditions while maintaining the engine’s thrust-to-weight ...

eliminating the need for compressors and turbine components. This simplifies the structure, improves the thrust-to-weight ratio, and lowers costs.

Because of their simple structure and high thrust-to-weight ratio, such engines have been used for flight tests in many countries. Although various types of detonation engines have been proposed ...