本文讨论了使神号航天飞机推进系统初步的基准方案,今后进一步研究会对这种基准方案加以改进。文中介绍了这种推进系统的一般设计原则,并且还验证了主推进系统发动机和辅助推进系统的推力器的设计性能。另外还讨论了有关安全、可靠性、寿命和维修性能等方面的工作要求,并介绍了使神号推进系统初步的基准流程。 This article discusses the initial benchmarking solution to make the Space Shuttle Shenzhou advanced. Future studies will improve this benchmarking solution. This paper presents the general design principles of this propulsion system and also verifies the design performance of thrusters for main propulsion system engines and auxiliary propulsion systems. Work requirements related to safety, reliability, longevity and serviceability were also discussed, and a baseline process was introduced to make the Gospel advance the system.