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Design of Rockets and Space Launch Vehicles [Kõva köide]

  • Formaat: Hardback, 255 pages
  • Ilmumisaeg: 30-Oct-2020
  • Kirjastus: American Institute of Aeronautics & Astronautics
  • ISBN-10: 1624105939
  • ISBN-13: 9781624105937
Teised raamatud teemal:
  • Formaat: Hardback, 255 pages
  • Ilmumisaeg: 30-Oct-2020
  • Kirjastus: American Institute of Aeronautics & Astronautics
  • ISBN-10: 1624105939
  • ISBN-13: 9781624105937
Teised raamatud teemal:
With growing interest in space activity and numerous new launchers in development, Design of Rockets and Space Launch Vehicles is a timely, comprehensive survey of important concepts and applications. It enhances understanding and provides exposure to practical aspects of design, manufacturing, testing, and engineering associated with these topics. The subject is mature, but the applications are changing and a new generation of engineers and designers are joining the aerospace industry. Intended for senior undergraduates and those with at least a bachelors level of engineering training, it contains many examples illustrated with photographs or line drawings of actual hardware or existing equipment.

The book begins with an introduction followed by a detailed history chapter. Next come requirements and performance estimation. At this point, the actual process of vehicle design is presented in a step-by-step method, introducing Level 1 sizing, mass, inboard profile, aerodynamic coefficients, trajectory simulation, mass distribution, loads distribution, Level 2 structural design, vehicle stability & control, vibration/shock/acoustic/thermal, flexible body effects and instabilities, manufacturing, launch pad facilities, cost estimation, range safety, failures and lessons learned. These topics are laid out in a logical order so as to follow a reasonable path through a Level 1 design effort.
Preface xiii
About the Authors xxi
Acknowledgements xxiii
Chapter 1 Launch Vehicles: Introduction, Operation, and the Design Process
1(34)
1.1 Introduction to Launch Vehicles
1(2)
1.2 Anatomy of a Launch Vehicle
3(6)
1.3 The Phases of Launch and Ascent
9(8)
1.4 Typical Launch Vehicle Mission and Mission Elements
17(2)
1.5 The Typical Launch Vehicle Design Process
19(2)
1.6 Launch Sites
21(2)
1.7 Launch Site Selection Criteria
23(7)
1.8 The Space Industry
30(2)
1.9 Summary
32(1)
References
32(1)
1.10 Further Reading
32(1)
1.11 Assignment: Launch Vehicle System Report
33(2)
Chapter 2 A Technical History of Space Launch Vehicles
35(96)
2.1 Rockets in the Early 20th Century
35(5)
2.2 World War II and the Development of the V-2
40(3)
2.3 The Cold War, ICBMs, and the First Space Launch Vehicles
43(48)
2.4 The Moon Race
91(5)
2.5 The Space Shuttle
96(5)
2.6 Launch Vehicle Oddities and Dead-Ends
101(10)
2.7 Other Launch Vehicles from Around the World
111(12)
2.8 Commercial Launch Vehicles: The Future?
123(1)
2.9 Small Launch Vehicles
124(7)
References
126(5)
Chapter 3 Missions, Orbits, and Energy Requirements
131(56)
3.1 Orbits, Orbital Parameters, and Trajectories
132(4)
3.2 Spacecraft Mission Orbits and Trajectories
136(6)
3.3 Required Energy to Be Delivered for Orbit
142(18)
3.4 Determining the Launch Vehicle Velocity Vector
160(6)
3.5 Direct Orbit
166(4)
3.6 Desired Inclination Less than Launch Latitude
170(2)
3.7 Launch Vehicle Performance Curves
172(2)
3.8 Launch Windows
174(6)
References
179(1)
3.9 Example Problems
180(7)
Chapter 4 Propulsion
187(52)
4.1 Combustion
188(3)
4.2 The Thrust Equation and Rocket Equation
191(8)
4.3 The Rocket Equation
199(4)
4.4 Solid-Propellant Motors
203(6)
4.5 Liquid-Propellant Engines
209(3)
4.6 Examples of Rocket Engine Performance
212(5)
4.7 Rocket Engine Power Cycles
217(12)
4.8 Aerospike Engines
229(3)
4.9 Hybrid Rockets
232(3)
4.10 Example Problems
235(4)
References
237(2)
Chapter 5 Launch Vehicle Performance and Staging
239(58)
5.1 The Three Categories of Launch Vehicle Mass
239(3)
5.2 Finding a Rocket's Speed Change in Free Space
242(1)
5.3 Burnout Speed
243(1)
5.4 Single-Stage-to-Orbit
243(1)
5.5 Staging
244(3)
5.6 Calculation of Speed Supplied by a Multistage Rocket
247(3)
5.7 Payload Ratio
250(1)
5.8 Unrestricted Staging
250(6)
5.9 Pitfalls of the Lagrangian "Optimization" Procedure
256(7)
5.10 All-Hydrogen Saturn V?
263(5)
5.11 Parallel Burns and Staging
268(5)
5.72 Launch Vehicle Design Sensitivities
273(10)
5.73 Some Useful Results: Determining Component Mass Values
283(1)
5.74 Summary
284(1)
References
284(1)
5.15 Exercises
285(12)
Chapter 6 Ascent Trajectory Analysis and Optimization
297(66)
6.1 Vertical Flight in Gravity, No Atmosphere
298(4)
6.2 Inclined Flight in Gravity, No Atmosphere
302(4)
6.3 General Flight with Gravity, Atmosphere Effects
306(7)
6.4 Aerodynamics of Launch Vehicles
313(14)
6.5 Getting to Orbit
327(2)
6.6 Launch Vehicle Trajectory Simulation
329(5)
6.7 Trajectory Optimization
334(4)
6.8 Some Examples of Launch Profiles and Trajectories
338(8)
6.9 Some Typical Launch Trajectories
346(7)
6.10 Conclusion
353(2)
References
354(1)
6.11 Exercises
355(8)
Chapter 7 Space Launch Vehicle Structures and Layout
363(50)
7.1 The Thor IRBM
363(1)
7.2 The Delta II: Evolved from Thor
364(4)
7.3 Atlas Takes Tank Structure Principle to Extremes
368(3)
7.4 The Mighty Saturns
371(4)
7.5 The Saturn V
375(10)
7.6 Another Way to Save Mass: Tank Dome Shapes
385(1)
7.7 Spherical vs Cylindrical Tanks: Which Have Less Mass?
385(6)
7.8 The Space Shuttie
391(4)
7.9 Delta IV
395(1)
7.10 Other Design Layout Considerations
396(1)
7.11 Payload Accommodations
396(6)
7.12 Launch Vehicle Structure Types
402(3)
7.73 Structural Materials
405(8)
References
410(3)
Chapter 8 Sizing, Inboard Profile, Mass Properties
413(80)
8.1 Inboard Profile
413(2)
8.2 Vehicle or Step Mass Calculations
415(2)
8.3 Liquid Propulsion System Real-Life Additions to Mass and Volume
417(11)
8.4 Other Launch Vehicle Components
428(7)
8.5 Solid Propulsion System Sizing
435(4)
8.6 Comments about Upper Steps and Payload Fairings
439(1)
8.7 Mass Estimation Process
440(37)
8.8 Calculation of Tank or Shell Thicknesses
477(7)
8.9 Launch Vehicle Symmetry
484(2)
References
485(1)
8.10 Exercises: Sizing, Inboard Profile, and Mass Properties of TSTO LV
486(7)
Chapter 9 Surface and Launch Environments, Launch and Flight Loads Analysis
493(76)
9.1 Launch Vehicle Load Cases
494(36)
9.2 Example: Max-q Air Load Calculation for Saturn V/Apollo 11 (SA-506)
530(20)
9.3 Load Curves Rules of Thumb
550(2)
9.4 Global vs. Local Loads
552(1)
9.5 Real Calculation of Vehicle Loads
553(2)
9.6 Dealing with High-Altitude Winds
555(1)
9.7 Design Issues for Ascent Phase
555(1)
9.8 Load Relief During Launch
556(2)
9.9 Endnote
558(1)
References
558(1)
9.10 Exercises
559(10)
Chapter 10 Launch Vehicle Stress Analysis
569(42)
10.1 Strength and Stress Analysis
570(4)
10.2 Stress Determination Using External Loads
574(7)
10.3 Allowable Stresses Based on Stability (Buckling) Criteria
581(5)
10.4 Effect of Internal Pressure on Stresses
586(9)
10.5 Determining the Overall Stress State
595(9)
10.6 Summary: Simple Rules for LV Structures
604(2)
References
605(1)
10.7 Exercises
606(5)
Chapter 11 Launch Vehicle and Payload Environments: Vibration, Shock, Acoustic, and Thermal Issues
611(62)
11.1 Mechanical Loads
611(23)
11.2 Acoustic Environment
634(10)
11.3 Launch Vehicle Thermal Environment
644(6)
11.4 Payload Environment: The Spacecraft's Point of View
650(3)
11.5 Spacecraft Structure Design Verification Process
653(15)
11.6 Summary
668(2)
References
668(2)
11.7 Exercises
670(3)
Chapter 12 Space Launch Vehicle Stability and Control: Higher-Order Dynamic Effects
673(78)
12.1 Guidance and Navigation vs Attitude Control
674(11)
12.2 Stability and Control
685(20)
12.3 Controlled Vehicle Equations of Motion
705(19)
12.4 Launch Vehicle Structural Vibrations and Instabilities
724(14)
12.5 Propulsion Instabilities
738(5)
12.6 Summary
743(3)
References
744(2)
12.7 Exercises: Vibration and TVC Analysis
746(5)
Chapter 13 Launch Vehicle Manufacturing
751(30)
13.1 Launch Vehicle Fabrication
751(1)
13.2 Saturn I Second Step (S-IV) Manufacturing Process
752(12)
13.3 Composite Structure Fabrication
764(9)
13.4 Manufacturing: The Future
773(1)
13.5 Vehicle Stacking and Assembly
774(4)
13.6 Postassembly Activities
778(1)
13.7 Summary
778(3)
References
779(2)
Chapter 14 Launch Vehicle Systems and Launch Pad Facilities
781(50)
14.1 Saturn V First-Step S-IC Systems Example
782(1)
14.2 Saturn V S-IC Fuel Tank and Fueling System
782(8)
14.3 Launch Vehicle Avionics
790(5)
14.4 Instrumentation and Telemetry
795(13)
14.5 Launch Pad Facilities and Ground Accommodations
808(21)
14.6 Summary
829(2)
References
829(2)
Chapter 15 Testing, Reliability, and Redundancy
831(34)
15.1 Testing
831(22)
15.2 Redundancy
853(9)
15.3 Summary
862(1)
References
862(1)
15.4 Exercise
863(2)
Chapter 16 Failures, Lessons Learned, Flight Termination Systems, and Aborts
865(30)
16.1 Causes of Expendable Launch Vehicle (ELV) Failures
865(3)
16.2 Failure Rates of Launch Vehicles
868(3)
16.3 Some Examples of Launch Vehicle Failures
871(11)
16.4 Additional Ways to Learn from Others' Mistakes
882(1)
16.5 Range Safety and Flight Termination Systems
883(9)
16.6 Best Practices to Avoid Failure
892(1)
16.7 Summary
893(2)
References
893(2)
Chapter 17 Launch Vehicle Financial Analysis and Project Management
895(44)
17.1 Stages of Mission Development
896(1)
17.2 The Design Cycle
897(2)
17.3 Design Decision Making
899(4)
17.4 Cost Engineering
903(5)
17.5 Cost Considerations
908(8)
17.6 Cost Modeling Examples
916(18)
17.7 Concluding Remarks
934(1)
References
935(1)
17.8 Exercises: LV Cost Estimation
935(4)
Glossary and Abbreviations 939(26)
Index 965(14)
Supporting Materials 979