Verifying QFPA's error model based on rocket sled testing
验证石英加速度计误差模型的火箭橇试验
Numerical analysis on the ignition mechanism of explosive in drop-weight test
炸药落锤试验点火机理的数值分析
Based on the data of Drop-weight test of various kinds of specimens with different thickness, it could be concluded that the value of T_(NDT) is not only dependent on the materials but also the thickness of the specimen.
以3种供应状态、5种钢材、6型试样的落锤试验数据说明钢材的无塑性转变温度TNDT不仅与材料有关,而且与试样厚度有关,二者的关系可用函数式TNDT=At-m+B表示,式中的A、B、m是与材料有关的参数。
The nil-ductility transition temperature of AH36 ship plate is -25℃ which is determined by drop weight test method.
利用落锤试验方法 ,测定了AH3 6级船板的无塑性转变温度为 -2 5℃ ,并对试验结果进行了评定。
The curves of impact acceleration vs time of some common explosives were experimentally determined in drop weight test.
在落锤试验中测量了落锤的撞击加速度，对几种炸药试验过程中落锤的加速度时间曲线进行了讨论。
Some equations of explosive explosion probability and probability of occurring number k successive explosion in one group (25sets) in drop hammer test are deduced with probabilistic method in this paper,as well as the relative table.
应用概率统计的方法 ,导出了炸药的爆炸概率与落锤试验中测试一组 (2 5发 )试样时 ,出现k发连续爆炸的概率的关系式 ,给出了相应的概率表 ,为测试结果的可靠性提供了检测方
The framing photographs of explosive samples under drop hammer test exhibit a fractal structure,in which the fractal dimension is related to the explosive’s impact sensitivity.
根据分形几何的周长面积公式及线性回归原理，对ＴＡＴＢ等六种炸药样品的落锤试验的分幅图像进行了图像处理和分形维数计算。
Verifying QFPA's error model based on rocket sled testing
验证石英加速度计误差模型的火箭橇试验
Oscillate Imulation of Missile Flight for IMU in Sled Testing
惯性系统火箭橇试验模拟导弹振动的方法
Stochastic Irregularity Analysis on High Accuracy Rocket Sled Test Track
高精度火箭橇试验轨道随机不平顺分析
Acceleration Simulation of Missile for IMU in Sled Testing
惯性系统火箭橇试验过载曲线设计方法
Research on Test Data Processing Scheme of Strapdown Inertial Measurement Unit Based on Rocket Sled
捷联惯组火箭橇试验数据处理方案研究
Acceleration Simulation of Missile flight for IMU in Sled Testing
惯性测量装置火箭橇试验模拟导弹飞行过载方法
The rocket sled test was carried out for overall investigating the dynamic process of missile turbojet engine starting and accelerating.
为了研究弹用涡轮喷气发动机动态启动加速过程,开展了发动机火箭橇试验研究。
The rocket sled test can imitate the dynamic conditions of missile launching, it is very important for missile turbojet engine design.
火箭橇试验能够真实的模拟导弹发射条件,它对于弹用涡轮喷气发动机研究具有十分重要的意义。
tie-down firing
试车台点火试验火箭
Temperature stress analysis of high accuracy rocket sled rail
高精度火箭橇滑轨长轨温度应力分析
Design of Solid Rocket Motor Ignition Test System
固体火箭发动机点火试验测试系统设计
That was where Wernher began experimenting with rockets.
柏林是韦恩赫开始试验火箭的地方。
Characteristics tests of pulse liquid rocket engine with high chamber pressure
高室压脉冲液体火箭发动机特性试验
High and Low Temperature Environment Test Method of Rockets Based on Bayes
基于Bayes的火箭弹高、低温环境试验方法
Dynamic Analysis about High-speed Entry Water of Rocket Sled Water Brake Structure;
火箭滑橇水刹车结构高速入水的动态分析
Numerical Analysis about High-speed Entry Water of Rocket Sled Water Brake Machine
火箭滑橇水刹车机构高速入水数值分析
A testing area at which rockets and missiles are launched and tracked.
火箭发射场进行火箭、导弹等发射、追踪的试验地区
Noise measuring analysis on the ground test of solid rocket motor
固体火箭发动机地面试验的噪声测试分析(英文)