摘要
空气涡轮冲压喷气发动机是未来航天飞机吸气式推进系统最有希望的候选方案。日本航空宇宙技术研究所和石川岛播磨重工业公司目前正在开展这方面的研究工作。本文介绍了他们提出的膨胀循环空气涡轮冲压喷气发动机(ATREX)的系统设计、研制进展情况以及用于海平面静态试验的缩比型ATREX发动机的结构。
In Japan, Institute of Space and Astronautical Science (ISAS) in cooperation with Ishikawajima-Harima Heavy Industries Co., LTD(IHI) is conducting development study of Air Turbo-Ramjet(ATR) engine, which is one of the most preferable candidate as an air breathing propulsion system of future space plane. In this paper are presented the system design of the expander cycle ATR engine named ATREX, the scenario of de-velopment study and the ATR sub-scale engine model configuration for sea level static test.
