The Study on Obturator of Rocket Engine for Compound Assisted Projectile 复合增程弹火箭发动机闭气装置及性能研究
The paper research fire angle of the projectile, firing time of the rocket motor, assisted time of the rocket motor, flying attitude of the glide phase and the terminal phase guidance law to add the projectile firing range. 在建立的模型的基础上,深入研究了炮弹的射角、火箭发动机的点火时间、火箭发动机的助推时间、滑翔段的飞行姿态以及末段制导律等对炮弹的射程及性能的影响。