全新正版 飞行器系统概论(第2版)(英文版) 编者:唐胜景//郭杰//李响//徐瑞//王晓芳|责编:王九贤 9787118124675 国防工业
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作者编者:唐胜景//郭杰//李响//徐瑞//王晓芳|责编:王九贤
出版社国防工业
ISBN9787118124675
出版时间2021-07
装帧其他
开本其他
定价108元
货号31663499
上书时间2023-06-09
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目录
Chapter 1 Brief Introduction to flightvehicles1.1 Basic concepts1.2 Overview of flight vehicles 1.2.1 Rockets 1.2.2 Missiles 1.2.3 Airvehicles 1.2.4 Spacevehicles 1.2.5 Hypersonicflight vehicles1.3 Development history of flight vehicles 1.3.1 Flight vehicle exploration 1.3.2 Typicalexamples of aeronautics & astronautics 1.3.3 Famouspersons in aerospace 1.4 Flight vehicles today 1.4.1 Rockets & missiles 1.4.2 Air vehicles 1.4.3 Space VehiclesChapter 2 Flight principles of flightvehicles2.1 Outlines2.2 Rocket motion 2.2.1Basic principles 2.2.2Multistage rocket theory2.3 Atmospheric environment 2.3.1 Atmosphericenvironment 2.3.2 Standard atmosphere 2.3.3Earth reference ellipsoid2.3 Physical properties of atmosphere 2.3.1 Gas state equation 2.3.2 Low speedflow 2.3.3 High speedflow 2.3.4 Basicprinciples of fluid2.4 Mechanics environment of a flight vehicle 2.4.1Gravity 2.4.2Thrust & thrust moments 2.4.3 Aerodynamics & aerodynamic moments2.5 Flight vehicle motion 2.5.1Reference frames and transformations 2.5.2Flight vehicle motion equation 2.6 Flight performances 2.6.1Flight mission profile 2.6.2Overload2.7 Flight stability & control 2.7.1Stability 2.7.2ControlChapter 3 Flight vehicle system compositions3.1 Overview of flight vehicle system3.2 Missile system composition 3.2.1 Surface toAir missile system 3.2.2 Antitank missile system3.3 Rocket system composition3.4 Aircraft system composition3.5 Spacecraft system composition 3.5.1 Satellitesystem 3.5.2 Spacecraftsystem 3.5.3 Spacestation system 3.5.4 Mannedspace flight systemChapter 4 Flight vehicle propulsion system4.1 Basic concepts and principles4.2 Main performance parameters4.3 Aviation engine system4.4 Rocket propulsion system 4.4.1 Solidrocket propulsion system 4.4.2 Liquidrocket propulsion system4.5 Combination engine system4.6 Thrust vector control system4.7 Special propulsion system4.8 Engine applicationChapter 5 Flight vehicle aerodynamic configuration5.1 Flight vehicle configuration 5.1.1Overview 5.1.2 Typicalmissile configuration 5.1.3 Aircraft configuration 5.1.4 Liftingsurfaces 5.1.5 Controlsurfaces5.2 Flight vehicle configuration parameters 5.2.1 Airfoil 5.2.2Wing platform 5.2.3Flight vehicle configuration geometric parameters5.2 Aircraft configuration variationChapter 6 Flight vehicle construction6.1 Flight vehicle construction6.2.1 Typical construction6.2.2 Body (fuselage) 6.2.3 Wing 6.2.4 Tail6.2 Loads on flight vehicles 6.3.1 Aerodynamicloads 6.3.2 Massdistribution loadsChapter 7 Flight vehicle GNC system7.1 Concepts of GNC system7.1.1 Guidance and control loop7.1.2 Navigation system 7.1.3 Guidance system7.1.4 Control system7.2 Guidance and control components7.2.1 Sensitive components 7.2.2Seeker7.3 Guidance modes 7.3.1 Automaticguidance system 7.3.2 Remoteguidance system 7.3.3 Homingguidance system 7.3.4 Combinationguidance system7.4 Control system 7.4.1 Threecontrol ways 7.4.2 Autopilot7.5 Guidance methods 7.5.1 Automaticguidance method 7.5.2 Remoteguidance method7.6 ActuationChapter 8 Ground equipment and launch8.1 Airport and ground equipment 8.1.1 Airport 8.1.2 Groundequipment8.2 Rocket & space vehicle launch 8.2.1 Space base 8.2.2 Space shuttlelaunch procedure 8.2.3 Spacevehicle return & reentry8.3 Missile launch 8.3.1 Missilelaunch system 8.3.2 Missilelaunch ways 8.3.3 Missilelaunch equipmentChapter 9 Payloads9.1 Outlines9.2 Rocket payloads9.2 Air vehicle payloads9.3 Space vehicle payloads9.4 Missile payloads 9.4.1 Warheadcomposition 9.4.2 Typicalwarhead 9.4.3 FusesChapter 10 Flight vehicle research anddevelopment10.1 Flight vehicle design concepts 10.1.1 Flightvehicle design process 10.1.2 Flightvehicle system analysis10.2 Basic stages of flight vehicle research anddevelopment10.2.1 Idea proposition10.2.2 Proof of tactical and technical requirements10.2.3 Preliminary design10.2.4 Technical design10.2.5 Trial-manufacture and test 10.2.6 Design finality10.2.7 Manufacture and utilization10.3 Design requirement10.4 Design methods10.5 Typical tests10.6 Design example for a flight vehicleReferences
内容摘要
书介绍了飞行器系统的基本概念和基本原理。主要包括空间环境、力学环境、飞行基本原理、系统组成、推进系统、外形与结构、制导与控制系统、地面设备与发射方式、有效载荷等。还介绍了飞行器设计与研究的基本概念、研究方法和典型实验等。
本书也可供从事飞行器设计、研究、生产和部队有关人员参考。
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