摘要
提出了一种TVC火箭包方案,即多喷管火箭包及相应的爆破切割技术,实现飞机座椅弹射后轨迹控制。该方案对大多数国产现役火箭弹射座椅具有较好的适用性。相应的内弹道性能与弹射轨迹的计算结果是令人满意的。
This paper presents a new design of TVC (thrust vector control) rocket-propelled installation. Multiple nozzles of rocket-propelled installation and pyrotechnic cutter are used to control the trajectory of rocket-propelled airborne ejection. It can be used for most of the airborne rocket ejection seat made in China and being on actve service. The calculation results of thrust-time relation and trajectory are satisfactory.
出处
《推进技术》
EI
CAS
CSCD
北大核心
1992年第6期59-65,18,共8页
Journal of Propulsion Technology
关键词
弹射座椅
飞行员
救生火箭
Bailout capsule, Pilot seat, Aviation safety, Life rocket,Escape rocket