1) cartridge stop
弹头止动器
2) snap spring
止动弹簧
1.
The snap spring of Rate Governor occured brittle fracture or insufficient elasticity, dimension change, uncleanliness of surface during the trial manufacture.
RQV调速器的重要零件止动弹簧在试制期间 ,常常出现脆性断裂或弹性不足 ,尺寸变化 ,表面不清洁等质量问题 ,经过多次热处理工艺试验和工艺改进 ,对设备和工艺参数调整和优化后 ,很好地解决了这些质量问
3) maneuvering warhead
机动弹头
1.
A new idea of aerodynamic configuration for maneuvering warhead design;
机动弹头气动布局的一种新思路
2.
A new kind of maneuvering warhead aerodynamic configuration with the use of two retractile control surfaces was proposed,which avoided such severely aerothermodynamic environment in reentry flying like traditional maneuvering warhead configuration.
提出了一种伸缩舵面机动弹头气动布局设计的新理念,避免了普通全动舵面布局方案中舵轴设计面临的严峻热环境和力环境等问题。
4) Maneuverable Warhead
机动弹头
1.
Maneuverable warhead are the complex nonlinear system,which take a great challenge to the attitude control system designers.
机动弹头是复杂的非线性系统,它给姿态控制系统设计人员以极大的挑战。
2.
Aiming at the optimization problem of attack area of maneuverable warhead,an Aerial Hybrid Genetic Algorithms(AHGA) consisting of Genetic Algorithms(GA) and Constrained Flexible Polyhedrow Method(CFPM) was designed.
针对机动弹头攻击区优化问题,设计了改进遗传算法加约束可变多面体法的串行混合遗传算法,采用直接优化方法,基于分段优化思想,对再入段最大纵程、最小纵程和最大横程等边界弹道分别进行了优化设计,得到了满足约束条件的最优边界弹道,从而确定了机动弹头的最大可攻击范围。
5) maneuver warhead
机动弹头
1.
When the reentry maneuver warhead flies,control force of guidance system is provided by aero-fin defluxions.
机动弹头再入飞行时,其控制系统是由空气舵偏转产生的空气动力作为控制力的,文中研究了空气舵三个通道之间的交连耦合影响并建立了再入机动弹道的气动环境模型。
2.
We would try to apply it for designing the project of the laser terminal guidance system of maneuver warhead in this paper.
比例导引律是当前研究最活跃和应用最广泛的制导规律之一,文中试图将其应用于机动弹头激光末制导系统的方案研究和设计。
6) maneuvering missile
机动弹头
1.
Finally,the numerical simulation results of maneuvering missile with the control helm are shown under the conditions:M ∞=7 3,α=20°.
最后给出带控制舵机动弹头在M∞ =7 3,α =2 0°下所计算的流场等值线、表面压强分布及表面极限流
2.
Finally, the numerical simulation results of maneuvering missile were shown under the conditions: M∞ = 7.
最后给出了机动弹头在M_∞=7。
补充资料：弹头气动加热(见弹头防热)
弹头气动加热(见弹头防热)
aerodynamic heating of warhead
dantou qidong iiare弹头气动加热(aerodynam，c heating。fWarhead)见弹头防热。
说明：补充资料仅用于学习参考，请勿用于其它任何用途。
参考词条