摘要
空气涡轮火箭发动机是适用于临近空间飞行器的吸气式组合动力装置,具有大空域、宽速域的特点,受到了世界各军事大国的重视。综述了空气涡轮火箭发动机的技术特点和国内外在这一领域的发展现状,对其研究中存在的技术难点和发展前景进行了分析讨论。
Air turbine rocket (ATR) is adequate for near space as an aspiration combination power. It possesses the characters of great air-space and broad velocity field and was attached importance by military powers all around the world. This paper summarizes the technical features and the developing status both home and abroad about ATR, furthermore the technical difficulties and challenges of ATR were also analyzed.
出处
《火箭推进》
CAS
2008年第6期31-35,共5页
Journal of Rocket Propulsion