| 摘要: |
| 文中对用固体火箭发动机应急打开并抛弃座舱盖方案进行了探索。并根据飞机座舱盖抛放总体方案的要求,确定了固体火箭发动机的设计参数。通过地面试验说明该方案是切实可行的。所设计的固体火箭发动机,其性能满足总体要求。 |
| 关键词: 飞机座舱盖 弹射座舱 固体火箭发动机 |
| DOI： |
| 分类号: |
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| INVESTIGATION ON OPENING AND THROWING OF AEROPLANE CANOPY BY USING SOLID ROCKET ENGINE |
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Xie Yunwu
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Northwestern Polytechnical University
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| Abstract: |
| An investigation on opening and throwing of aeroplane canopy by using solid rocket engine is made in order to save pilot’s life in an emergency. The design parameters of SPRM are determined according to the demand of total project for aeroplane canopy being thrown out. Ground tests verity that the design is practicable, and that the performance of engine can satisfy the demand of total project. |
| Key words: Aircraft canopy Bailout capsule Solid rocket engine |
