固体火箭冲压发动机在空空导弹上应用的优势

Predominance of Ducted Solid Rocket Ramjet Applied to Airborne Missile

通过对采用固体火箭冲压发动机和固体火箭发动机的导弹在不同高度下的弹道性能计算和分析,得出采用固体火箭冲压发动机的导弹在射程、速度、机动性等方面都比采用固体火箭发动机的导弹具有很大的优越性,希望能够为我国今后发展固体火箭冲压发动机技术提供一些理论支撑。

The trajectory performance of airborne missile in different altitude is investigated and analyzed by comparing dueted solid rocket ramjet with solid rocket motor. The results show that the airborne missile adopting ducted solid rocket ramjet is superior at the aspects of firing range, velocity and maneuverability. The conclusions are instructional to the research of ducted solid rocket ramjet.