rocket engine test

Application of Data Acquisition System to Solid Rocket Engine Test

数据采集系统在固体火箭发动机试验中的应用

Design of data curve drawing software for liquid rocket engine test

液体火箭发动机试验数据曲线绘制软件设计

Valve current signal acquisition system design for liquid attitude control rocket engine test

姿控发动机试验阀门电流信号采集系统设计

Design of Rocket Engine Test - bed with High - speed Rotation

固体火箭发动机高速旋转试验台设计

Application of MAP in the Measurement of Rocket Engine Test

MAP在火箭发动机试验计量及测量中的应用

Noise processing based on wavelet analysis for liquid propellant rocket engine test data

基于小波理论的液体火箭发动机试验数据噪声处理

The Effect of Density Measurement in Cryogenic Liquid Rocket Engine Test

密度测量在低温液体火箭发动机试验中的作用

Measurement technology of thermocouple sensor in the liquid rocket engine test

液体火箭发动机试验热电偶传感器测量工艺

The anti-interference technology of thermocouple channel used in rocket engine test system

火箭发动机测试系统热电偶通路抗干扰技术

Rocket engine test stand exerts force on a load cell .

火箭发动机试验的立场，施加武力对负载细胞。

It is very important to measure liquid density in cryogenic liquid rocket engine test .

在低温液体火箭发动机的试验中，对液体密度的测量是很重要的。

Application of Wavelet Analysis in Steady Data De-nosing for Liquid Propellant Rocket Engine Test

小波分析方法在液体火箭发动机试验稳态数据去噪中的应用

Safety method in hydrogen-oxygen rocket engine test

氢氧发动机试验安全技术

Application of Coriolis Force Mass Flowmeter in Gelled Propellant Rocket Engine Test

科氏力质量流量计在凝胶推进剂火箭发动机试车中的应用

The Application of Cryogenic Technology in LOX / LH 2 Rocket Engine Test Stand

低温技术在氢氧火箭发动机试车台上的应用

LOX / kerosene rocket engine test system

液氧/煤油发动机试验系统

Noise in the raw acquired data of liquid propellant rocket engine test can reduce accuracy and creditability of the data .

液体火箭发动机试验的原始测量数据中存在着噪声，影响了数据的准确性和可信性。

Firstly , the pulse rocket engine test system has been built and provides hardware constitute plan and test every aspect of the application of the test .

本文首先对脉冲火箭发动机的测试系统进行组建，提出了测试系统的硬件组成方案，并对测试系统的各个应用环节加以论证。

The measuring methods used and the key technologies to be resolved in the flowrate measurement of H2O2 / kerosene rocket engine test are discussed in the paper .

论述了液体火箭发动机用过氧化氢作为推进剂进行试验的过程中流量测量可采用的方式。

Quality control and management of rocket engine ground test software

火箭发动机地面试验软件质量管理和控制

Solid Propellant Rocket Engine Modal Test and Analysis Technique

固体火箭发动机试验模态分析技术研究

Test Data Validation and Reconstruction Based on Regression Model for Liquid Propellant Rocket Engine Ground Test

基于回归模型的液体火箭发动机试验数据的验证与重构

And rocket engine function test occupy the important status in the all kinds of tests of rocket .

而火箭发动机性能测试在火箭武器各类试验中占有重要地位。

At last , the sensor fault diagnostic software of liquid rocket engine ground test system is developed successfully , including the designs of arithmetic , database and interface software .

本文开发了液体火箭发动机试车台传感器故障诊断系统，包括算法实现、数据库设计和用户界面设计。

This paper , based on the characteristics of rocket engine reliability test , use liner model and regression method to forecast the measurement parameters in weibull distribution model , see , in the new stage reliability test .

基于液体火箭发动机可靠性增长试验的特点，结合数理统计中的线性回归方法对新阶段试验下发动机的可靠性试验结果进行预测。

The results demonstrate that the wavelet analysis method can fulfill the test data processing in the test steady stage and operation condition change stage . It is very suitable for the test data processing for liquid propellant rocket engine ground test .

结果表明，小波分析方法能够同时完成稳态过程和工况变化时刻的测量数据分析处理，非常适合液体火箭发动机的试验数据处理。

The reliability of liquid rocket engine ground test bed is a key factor to ensure the success of ground test for liquid rocket engine . Once the ground test bed goes wrong , the whole test will fail and which might cause huge economic losses .

液体火箭发动机地面试验台的可靠运行是保证火箭发动机地面试验成功的关键因素，一旦试验台发生故障整个试验将失败，将会造成巨大的经济损失。

Mechanical and Error Characteristics of Rocket Engine Thrust Vector Test System

火箭发动机六分力试验系统力学和误差特性

The LS-Bayes Analysis for Rocket Engine Reliability Growth Test under Weibull Life Model

Weibull寿命模型下火箭发动机可靠性增长试验的LS-Bayes分析

The paper presents the composition , functions , technical performance and research of the solid rocket ramjet engine ground test equipment and measurement control system in detail .

介绍了固体火箭冲压发动机地面实验装置及测控系统组成、功能、技术指标和可以开展的研究工作。