This two-part article introduces a novel hybrid propulsion system based on the DEA compressor. The system encompasses a Pulse Detonation TurboDEA as the master engine that supplies several full-electric ancillary thrusters called DEAThruster. The system, called the propulsion set, can be categorized as a distributed propulsion system based on the design mission and number of ancillary thrusters. Part A of this article explains the design process comprising intake, compressor, detonation process, diffuser, axial turbine, and the exit nozzle. The main target is to design a high-performance low emission propulsion system capable of serving in a wide range of altitudes and flight Mach numbers that covers altitudes up to 20,000 m and flight Mach number up to the hypersonic edge. Designing the propulsion set, the design point is considered at the static condition in the sea level. Design results show the propulsion set can satisfy all requirements necessary for its mission.

这篇由两部分组成的文章介绍了一种基于 DEA 压缩机的新型混合推进系统。该系统包含一个脉冲爆震 TurboDEA 作为主发动机，它提供几个称为 DEAThruster 的全电动辅助推进器。该系统称为推进装置，可根据设计任务和辅助推进器的数量归类为分布式推进系统。本文的 A 部分解释了设计过程，包括进气、压气机、爆震过程、扩压器、轴流涡轮和出口喷嘴。主要目标是设计一种高性能低排放推进系统，能够在广泛的高度和飞行马赫数范围内服务，覆盖高度高达 20,000 米，飞行马赫数高达高超音速边缘。设计推进装置，设计点是在海平面的静态条件下考虑的。设计结果表明，推进装置可以满足其任务所需的所有要求。