液氧煤油发动机

液氧煤油发动机低温组元两相充填过程研究

Research on two-phase filling process of cryogenic propellant for a LOX / Kerosene LRE

GB/T14455.9-1993精油填充柱气相色谱分析通用法液氧煤油发动机低温组元两相充填过程研究

Essential oils Analysis by gas Chromatography on packed columns General method Research on two-phase filling process of cryogenic propellant for a LOX / Kerosene LRE

液氧/煤油发动机试车主要参数测量方法研究

Research of measuring method in the LOX / kerosene engine tests

液氧/煤油发动机试验控制系统软件架构与设计

Software structure and design of LOX / kerosene engine test control system

液氧/煤油发动机摇摆测控系统技术要求及实现

Development of the swinging measurement system for LOX / kerosene rocket engine

液氧/煤油发动机试验起动过程推进剂供应技术

Technology of propellant supply in starting of LOX / kerosene engine testing

液氧/煤油发动机燃料节流阀试验技术

LOX / kerosene engine fuel throttle valve test technology

液氧/煤油发动机涡轮泵密封材料的研制

Sealing Material Used in Turbine Pump of Liquid Oxygen / Kerosene Rocket Engine

液氧/煤油发动机煤油预压涡轮泵技术

Techniques of kerosene booster turbopump for LOX / kerosene staged combustion cycle engine

液氧煤油火箭发动机起动故障检测

LOX / Kerosene Rocket Engine Starting Fault Detection

液氧/煤油发动机地面试验故障紧急关机系统研制

Development of test fault emergency cut-off system for LOX / kerosene engine ground test

液氧/煤油发动机煤油高低温试验工艺技术

High and low temperature test technology of kerosene of the LOX / kerosene engine

液氧/煤油发动机稳态参数分布特性的仿真

Monte-Carlo simulation on static characteristics of a liquid oxygen / kerosene staged combustion cycle engine

液氧/煤油发动机试验系统

LOX / kerosene rocket engine test system

液氧/煤油发动机换热器试车台配气系统设计

Design of air rationing system of heat exchanger test bench for LOX / kerosene rocket engine

介绍了液氧/煤油发动机试验起动过程中的煤油供应技术。

The article discusses the technology of kerosene supplying in the starting of LOX / kerosene rocket engine testing .

所设计的配气系统满足了液氧/煤油发动机换热器系统的试验要求。

An air rationing system was designed and test proved that it can meet the requirement of the engine test .

由于商业卫星发射业务量的增加，以及某新型火箭采用液氧+煤油发动机，使得基地配属的小型空分设备不能满足需要，因此必须研究空分设备的增产和降耗问题。

The small air separating equipment of the Base does not meet needs from increasing launch business of commercial satellites , still owing to an new type of rocket adopting " LO2 + kerosene " engine .

论述了液氧/煤油发动机研制地面试车中，出现故障时所采用的紧急关机系统的原理和系统结构、设计程序、设计指标、关机判断准则、验证及应用等。

Principles , program , design parameters and cut-off decision making criteria for LOX / Kerosene engine ground test emergency cut-off system were presented in this paper . The system has been applied to the LOX / kerosene engine ground test and verified .

但由于其密度比冲比液氧/煤油发动机低，使用安全性也不如煤油；性能又比液氧/液氢发动机低，这些都限制了液氧/甲烷发动机的发展和应用。

However , its lower density specific impulse than liquid oxygen / kerosene engine , inferior safety than kerosene and lower performance than liquid oxygen / liquid hydrogen engine , altogether has limited the development and application of liquid oxygen / methane engine .

为分析补燃循环液氧/煤油发动机工作的稳定性，建立了发动机的线性小偏差动力学模型，在小扰动的条件下研究了发动机工况变化、燃气导管容积对系统工作稳定性的影响。

The linear small deviation dynamic model is developed for the analysis of a LOX / Kerosene staged combustion cycle engine . Based on linear method under small disturbance , the effects of engine working condition and gas vessel volume on system stability are analyzed .

液氧/煤油火箭发动机故障诊断与监控

Fault diagnosis and monitoring of a liquid oxygen / kerosene propellant rocket engine

液氧－煤油火箭发动机的燃烧不稳定性问题

Combustion instability problems in LOX-KEROSENE rocket engines

液氧/煤油火箭发动机推力和混合比的非线性调整研究

Non linear throttling analysis of thrust and mixture ratio for a liquid oxygen / kerosene rocket engine

介绍了美国F－1发动机和俄国RD－0110发动机的燃烧不稳定现象和解决办法，它们基本上概括了液氧－煤油火箭发动机研制中遇到的燃烧不稳定性问题。

He phenomena and the solution of the combustion instability in the American F-1 engine and the Russian RD-0110 engine are presented . The combustion instability problems encountered in the LOX-kerosene rocket engines are summarized mostly .

液氧/煤油补燃发动机系统稳定性分析

System stability analysis of a LOX / kerosene staged combustion cycle engine

液氧/煤油补燃发动机低频频率特性研究

Research on the low frequency characteristics of LOX / kerosene staged combustion cycle engine