某改型导弹折叠舵的设计

详细介绍了××改型导弹折叠舵研究课题的成果。内容包括：主要设计要求、研制程序、方案的拟定、设计、试验及结果分析、结论等部分。通过试制及试验，证明把高强度扭力杆应用于折叠舵的展开机构具有展开能量大、展开时间短、重量轻、体积小、结构简单等优点。该项技术不但使××改型导弹折叠舵课题获得成功，而且可以推广应用到需要折叠与展开的其他飞行器上

FOLDING RUDDER DESIGN OF SOME MODIFIED MISSILE

The achievements in study on folding rubber of some modified missile are introduced in detail, involving main design requirements, developing procedure, plan draught, design, test, analysis of results and conclusion. The development work and test show that the application of torsion bar with high strength in deploying mechanism of folding rubber had the advantages of short deploying time, light, small volume and simple structure. This technology not only makes the development of some modified missile's folding rubber suceed, but also can be extended to other flyers that need to be folded and deployed.