Chapter 1 Brief introduction to iht vehicles
1.1 Basic concepts
1.2 Overview o fiht vehicles
1.2.1 Rockets
1.2.2 Missiles
1.. Air vehicles
1.2.4 Spacecrafts
1.2.5 Hypersonic iht vehicles
1.3 Development history o fiht vehicles
1.3.1 Flight vehicle exploration
1.3.2 Typical examples of aeronautics & astronautics
1.3.3 Prominent figures in aerospace
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Words and phrases
References
Chapter 2 Flight principles o fiht vehicles
2.1 Rocket motion
2.1.1 Rocket movement
2.1.2 Rocket motion equation
2.1.3 Multistage rocket theory
2.2 Flight environment
2.2.1 Earth atmosphere
2.2.2 Near space
2.. Outer space
. Fundamental principle of fluid flowing
..1 Basic concepts & typical parameters
..2 Fundamental principles of fluid motion
.. Applications of the principlesHigh-speed flow
2.4 Reference system
2.4.1 Reference frames and transformations
2.4.2 European-American coordinate system and Soviet Trion cnordinate system
2.5 Flight mechanics description
2.5.1 Forces acted on iht vehicles
2.5.2 Moments acted on iht vehicles
2.6 Flight vehicle motion equation
2.6.1 Basic assutin
2.6.2 Fundamental principles
2.6.3 Flight vehicle motion equation establishment
2.7 Flight performances
2.7.1 Flight mission profile
2.7.2 Flight envelope
2.7.3 Typical iht parameters
2.8 Flight stability & control
2.8.1 Stability
2.8.2 Control
2.9 Space vehicles iht principles
2.9.1 Kepler laws
2.9.2 Orbit equation & universal velocities
2.9.3 Satellite orbits
2.9.4 Lunar exploration orbit
2.9.5 Mars exploration orbit
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References
Chapter 3 Flight vehicle system coition
3.1 Flight vehicle system
3.2 Missile system
3.2.1 Missile system coition
3.2.2 Typical examples of the missile system
3.3 Rocket system
3.3 . 1 Multiple rokt ancher system
3.3.2 Carrier rocket system
3.4 Air vehicle system
3.4 . 1 Airplane system
3.4.2 U system
3.5 Spacecraft system
3.5 . 1 Space engineering system
3.5.2 Typical examples of the spacecraft system
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Words and phrases
References
Chapter 4 Flight vehicle propulsion system
4.1 Aeroengine system
4.1.1 Aviation piston engines
4.1.2 Turbojet engines & turbofan engines
4.1.3 Turboprop engines & turboshaft engines
4.1.4 Ram-engines
4.2 Rocket engine system
4.2.1 Main performance parameters
4.2.2 Solid rocket propulsion system
4.. Liquid rocket propulsion system
4.2.4 Combination engines
4.3 Thrust vector control system
4.3.1 Classification of thrust vector control system
4.3.2 Performance and selection of thrust vector control system
4.4 New-type propulsion system
4.4.1 Solar energy propulsion system
4.4.2 Nuclear energy propulsion system
4.4.3 Electric propulsion system
4.4.4 Micro propulsion system
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References
Chapter 5 Flight vehicle aerodynamic configuration
5.1 Design requirements for configuration
5.2 Flight vehicle configuration & parameters
5.2.1 Airfoil
5.2.2 Wing form & tail configuration
5.. Fuselage
5.3 Typical iht vehicle configuration
5.3.1 Typical missile configuration
5.3.2 Typical aircraft configuration
5.3.3 Control surfaces
5.3.4 High-lift devices
5.4 Configuration of hyper-velocity vehicles
5.4.1 Lifting body configuration
5.4.2 Blended-wing-body
5.4.3 Waverider configuration
5.5 Flight vehicle configuration variation & development
5.5.1 Missile configuration variations
5.5.2 Aireraft configuration variations
5.5.3 Morphing iht vehicle configuration
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Words and phrases
References
Chapter 6 Flight vehicle structures
6.1 Requirements o fiht vehicle structure design
6.1.1 Flight vehicle structure design philosophy
6.1.2 Basic iht vehicle structure design requirements
6.1.3 Basic iht vehicle structure design contents
6.1.4 Flight vehicle structure design methods
6.2 Wing
6.2.1 Function and loads
6.2.2 Main load-bearing members of a wing
6.. Load transfer analysis
6.2.4 Wing structure form
6.2.5 Connection
6.3 Body
6.3.1 Function and loads
6.3.2 Main load-bearing members of body
6.3.3 Body structure form
6.4 Tail
6.4.1 Function and constitution of tail
6.4.2 Basic requirements of tail
6.4.3 Loads of tail
6.5 Flight vehicle laminated coite structures
6.5.1 Characteristics of coites
6.5.2 Application of coite materials to airframe structures
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Words and phrases
References
Chapter 7 Flight vehicle guidance and control system
7.1 Basic concepts of guidance and control system
7.1.1 Function and coition
7.1.2 Classification of guidance system
7.1.3 Basic design requirements
7.2 Guidance and control components
7.2.1 Sensitive components
7.2.2 Seeker
7.. Star sensor
7.2.4 Actuation
7.3 Guidance system
7.3.1 Autonomous guidance system
7.3.2 Remote guidance system
7.3.3 Homing guidance system
7.3.4 Combination guidance system
7.4 Guidance laws
7.4.1 Autonomous guidance law
7.4.2 Remote guidance law
7.4.3 Optimal guidance law
7.4.4 Differential game guidance law
7.4.5 Cooperative guidance law
7.5 Control system
7.5.1 Control modes
7.5.2 Skid-to-turn (STT) and bank-to-turn (BTT)
7.5.3 Autopilot
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Words and phrases
References
Chapter 8 Ground equimn ad launch
8.1 Carrier rocket & space vehicle launch
8.1.1 Spa anch base
8.1.2 Space vehicle return & reentry
8.2 Missile launch
8.2.1 Missile launch modes
8.2.2 Missile launch equipment
8.3 Airporndgrund equipment
8.3.1 Airport
8.3.2 Ground equipment
8.3.3 Weather observation
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Words and phrases
References
Chapter 9 Payloads
9.1 Rocket payloads
9.2 Missile payloads
9.2.1 Warhead coition
9.2.2 Typical warheads
9.. Fuses
9.3 Air vehicle payloads
9.4 Space vehicle payloads
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Words and phrases
References
Chapter 10 Flight vehicle system research and development
10.1 Flight vehicles design concepts
10.1.1 The R&D process
10.1.2 System analysis
10.2 Basic stages for R&D
10.2.1 Idea proposition
10.2.2 Proof of tactical and technical requirements
10.. Preliminary design stage
10.2.4 Technical design stage
10.2.5 Trial-manufacture and test stage
10.2.6 Finality of design stage
10.2.7 Manufacture an tization stage
10.3 Basic design requirements
10.3.1 Design requirements for iht vehicle systems
10.3.2 lity management for iht vehicle system R&D
10.4 Design methods
10.5 Typical tests
10.5.1 Wind tunnel test
10.5.2 Simulation tests
10.5.3 Flight test
10.5.4 Environmental test
10.5.5 System performance test
10.5.6 Reliability test
10.6 Summary
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Words and phrases
References
本书系统地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、地面设备与发方式、有效载荷等。同时，对飞行器设计与研究的基本阶段、研究方法、典型试验及其发展等进行了介绍。本书再版修改、补充了较新的相关内容。
本书可作为高等学校有关专业教材，也可供从事飞行器设计、研究、试验和管理的相关人员使用参考。
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