摘要
本文侧重分析直接影响小型无控火箭运载器落点精度的飞行稳定问题,提出了提高飞行德定性的设计方法和有效措施。最后,列出了用于稳定性量值设计和校核的稳定因子判据。
The flight stability influencing directly the accuracy for unguided mini-rocket carrier has been emphasised. The design methods and effective measures for increasing flight sta-bility have been given. Finally, the stability factors criterion for designing and checking stability value have been introduced.
出处
《战术导弹技术》
1990年第2期10-17,共8页
Tactical Missile Technology
关键词
运载器
无控火箭
飞行力学
稳定性
System structure——design
Stability
Flight mechanics
