您要查找的是不是:
- Buckling analysis on rear dome of solid rocket motor case was studied by means of ANSYS. 用ANSYS软件对固体发动机壳体后封头进行了外压屈曲分析。
- Rocket motor cases and the specially designed production equipment therefor. 四、火箭发动机的壳体及为其专门设计的生产设备。
- Crose J G.Reliability of solid rocket motor cases and nozzles[R].NTI S,N93-22103. 王松柏.;固体火箭发动机壳体结构的动态可靠性设计[J]
- THE BURSTING STUDY OF FILAMENT WOUND ROCKET MOTOR CASE 维缠绕固体火箭发动机壳体爆破问题研究
- FAILURE ANALYSIS OF THE MODEL SOLID ROCKET MOTOR CASE IN HYDROTEST 某型号固体火箭发动机壳体水压破坏分析
- Numerical simulation computation of plastic flow of a working solid rocket motor case 固体发动机壳体工作状态塑性流动数值模拟
- Finite Element Analysis of Large Deformation and Emulation for Filament-Wound Solid Rocket Motor Case 纤维缠绕固体火箭发动机壳体大变形有限元分析与仿真软件介绍
- rocket motor case 火箭发动机体
- The filament-wound case (FWC) plays a more and more important role in the solid rocket motor chamber structure (SRMCS) with composite material widely used in spaceflight fields. 随着复合材料在各个领域的广泛应用,作为××××发动机燃烧室的纤维缠绕复合材料壳体在航天领域中越来越受到人们的重视。
- Rocket motors have many advantages over other forms of propulsion. 火箭发动机比其他推进器有许多优点。
- Four nozzles, canted outboard, split the exhaust of the solid rocket motor into four equal tails. 四个向外倾斜的喷管把固体火箭发动机的排气流分成四个相等的尾巴。
- The motor case is a steel cylinder closed tight at one end. The other end is the poen throat and nozzle. 发动机壳体为一个其一端为密封的钢铸圆柱缸体,另一端则为敞口的喉道及喷管。
- There is a rocket motor on the satellite by which the direction of the satellite can be changed if necessary. 在卫星上还有一个火箭马达,必要时可以用它来改变卫星的方向。
- The motor case is a steel cylinder closed tight at one end. The other end is the open throat and nozzle. 发动机壳体为一个其一端为密封的钢铸圆柱缸体,另一端则为敞口的喉道及喷管。
- According to the requirement of pasty propellant rocket motor, a composite plasma igniting plan was adopted. 摘要根据膏体推进剂火箭发动机。
- The result can be employed in motor case assessment and reliability design based on plastic deformation. 其结果可供基于塑性形变的壳体评估及可靠性设计参考。
- The influence of structure axial vibration on the internal ballistics of solid rocket motor was investigated. 文中研究了固体发动机结构的轴向振动对燃烧室内弹道性能的影响。
- Investigated charring erosive characters of internal insulation of solid rocket motor under flight acceleration. 研究了固体火箭发动机内绝热层在飞行加速度条件下的炭化烧蚀特性。
- The thrust vector control(TVC) performance test of solid rocket motor is presented in this paper. 本文介绍了固体火箭发动机水下推力矢量特性试验。
- A response surface method(RSM) for structure reliability analysis of solid rocket motor(SRM) grain was presented. 发展了一种固体火箭发动机药柱结构可靠度分析的响应面法。