关键词: 飞机座舱盖;弹射座舱;固体火箭发动机

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