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- solid rocket projectile 固体火箭弹
- The external tank and solid rocket boosters are waiting in the VAB. 航天飞机外贮箱和火箭推进器就在该中心等待装配。
- solid propellant rocket projectile 固体火箭弹
- Did one of the solid rocket boosters somehow burn through its casing? 是否是其中一个助推火箭的外壳因某种原因被烧穿?
- Based on the principle of compound pendulum,the measurement method and corresponding equipment for the centroidal deviation and the rotary inertia of rocket projectile were described. 基于复摆原理,阐述了箭弹的质偏和转动惯量的测量方法及装置,推导出了质偏和转动惯量的计算公式。
- With the continuously increment of rocket projectile launching range, the influence from the measured accuracy of the engine charge temperature becomes increasingly evident for that of point of fall. 摘要随着火箭弹射击距离的不断增长，其发动机装药温度测量精度对落点精度的影响日益突出。
- A.Ciucci,et al. Numerical Analysis of Ignition Transients in Solid Rocket Motors. 余贞勇，固体火箭发动机翼槽内火焰传播机理研究，西北工业大学博士论文，2000.;3。
- 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 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。
- The article studys the diffuser in the active injector altitude simulated test system of solid rocket engine. 对固体火箭发动机主动引射高空模拟试车系统中的扩压器部分进行研究。
- 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。
- 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。
- 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]
- Finite element method is used in the study of nozzle damping of instable combustion in a solid rocket motor. 应用有限单元法研究固体火箭发动机不稳定燃烧中的喷管阻尼，并用波衰减对比法进行了试验研究。
- Carbon/carbon composites have become the most ideal materials for nozzles of solid rocket motor (SRM). 摘要C/C复合材料已成为固体火箭发动机(SRM)最理想的喷管材料。
- terminal trajectory correction rocket projectile 末修火箭弹
- radio-controlled rocket projectile 无线电控制火箭
- NASA is now checking on the damage of lightning on Endeavor and its solid rocket booster. 国家航空航天署正在检查奋进号航天飞机及其固体火箭助推器是否被闪电损坏。
