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固体推进剂燃烧转爆轰研究于1986年9月25日在国防科技大学通过鉴定。现代固体火箭发动机装药量很大,发动机尺寸达数米;推进剂的能量也愈来愈高,有些推进剂中还加有高能炸药。人们担心,在推进剂生产、贮存和导弹使用中是否会出现燃烧向爆轰转变的灾难性后果?如何控制和避免这种现象?必须从实验和理论上进行研究。因此,该课题是固体推进剂技术与强动载荷技术领域中一项重要的研究课题。
Solid propellant combustion detonation transition on September 25, 1986 at the National Defense Science and Technology passed the appraisal. Modern solid rocket motors charge large, engine size of several meters; propellant energy is also getting higher and higher, some propellant also added high-energy explosives. Is there any concern about the catastrophic consequences of the transition from combustion to detonation in propellant production, storage and missile use? How to control and avoid this phenomenon? It must be studied experimentally and theoretically. Therefore, the subject is an important research topic in the field of solid propellant technology and strong dynamic load.