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内容简介
Launch vehicles include ballistic missiles used to carry warhead and launch vehicles are used to transport an orbiter into an orbit.
This book presents and illustrates the foundations of ballistic missiles and launch vehicles conceptual design. The concept of Concurrent Engineering, determination of main design parameters, and overall configuration of schemes, as well as multistage rockets design are the principal contents of the book.
This is a text book and suitable for both postgraduate and senior undergraduate students of flight vehicle design. Practising engineers may also find it useful if they are comparatively new to this field and desire to study some professional terminologies in English. | |
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目录
目录 Chapter One Introduction1
1.1 System Engineering1
1.2 CE—Concurrent Engineering4
1.3 Conceptual Design6
Chapter Two Mission Analysis and Design10
2.1 Operational Requirement and Specification of Ballistic Missiles10
2.2 Economic Requirements of Production17
2.3 Usage/Operation Requirements17
2.4 Design Requirements of Launch Vehicles21
Chapter Three Analysis and Selection of Overall Schemes25
3.1 Propulsion System25
3.2 Guidance System31
3.3 Structural System37
Part ⅠSingle Stage Rocket Design
Chapter Four Trajectories51
4.1 Introduction51
4.2 The Forces and Moments Applied on a Rocket During Flight52
4.3 Motion Equations of Powered Flight Phase66
4.4 Motion Equations of Unpowered Flight Phase71
Chapter Five Determination of Main Design Parameters89
5.1 Main Design Parameters89
5.2 Trajectory Analysis94
5.3 Weight (Mass) Analysis109
5.4 Selection of Main Design Parameters for Liquid Rockets115
5.5 Selection of Main Design Parameters of Solid Rockets128
Chapter Six Configuration and Structural Design143
6.1 Selection of Rocket Diameter143
6.2 Shape Design of Forebody(Nose/Head)147
6.3 Length Determination of Midsection(Tank)148
6.4 Aftersection and Instrument Section149
6.5 Structural Design Consideration152
6.6 Roughly Structural Layout and Structural Analysis159
6.7 Materials162
6.8 Types of Construction163
Chapter Seven Checking Computations166
7.1 Introduction166
7.2 Mass, Center of Mass and Rotational Inertia (Moment of Inertia)167
7.3 Flight Performance182
7.4 Aerodynamic Surfaces and Control Angles185
Part ⅡMultistage Rocket Design
Chapter Eight Foreword of Multistage Rocket191
8.1 Introduction191
8.2 Composition and DeScription191
8.3 The Burnout Velocity of a Multistage Rocket194
Chapter Nine Conceptual Design of Multistage Rockets200
9.1 Design Mission Analysis and Technique Approach200
9.2 The Number of Stages200
9.3 Selection of Propellants201
9.4 Mass Analysis of Multistage Rockets203
9.5 Mass Distribution206
9.6 The Steps of Main Design Parameter Selection214
9.7 Using Existing(Single stage)Rockets to Compose a Multistage Rocket218
9.8 Separationconnection Device Design219
9.9 Separating Parameters Calculation222
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