虽然混合推进系统这一概念容易被想象成是一种辅助设计组合系统,实际上这种混合系统几乎最接近自然的燃烧过程。以最好的液体火箭技术与最好的固体发动机系统组合成的混合推进系统的设想并不新,它是近半个世纪来人们一直在研究的课题。最初的混合推进系统的分系统包括:氧化剂箱、供给系统和喷射系统以及装在加压密封 Although the concept of a hybrid propulsion system can easily be conceived of as an aided design portfolio, in fact the hybrid system is almost the closest to the natural combustion process. The idea of ​​a hybrid propulsion system with the best liquid rocket technology combined with the best solid-state engine system is not new and has been the subject of much discussion for nearly half a century. The original hybrid propulsion system subsystems included: oxidizer tanks, feed systems and injection systems, and pressure seals