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Introduction to Rocket Science and Engineering 2nd edition [Kõva köide]

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  • Formaat: Hardback, 352 pages, kõrgus x laius: 254x178 mm, kaal: 822 g, 200 Illustrations, color; 65 Illustrations, black and white
  • Ilmumisaeg: 07-Jul-2017
  • Kirjastus: CRC Press Inc
  • ISBN-10: 1498772323
  • ISBN-13: 9781498772327
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Introduction to Rocket Science and Engineering 2nd editionSuurem pilt
  • Formaat: Hardback, 352 pages, kõrgus x laius: 254x178 mm, kaal: 822 g, 200 Illustrations, color; 65 Illustrations, black and white
  • Ilmumisaeg: 07-Jul-2017
  • Kirjastus: CRC Press Inc
  • ISBN-10: 1498772323
  • ISBN-13: 9781498772327
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Teised raamatud sellest sooduspakkumisest: Taylor & Francis teadusraamatud International Student Editions hindadega
Püsilink: https://www.kriso.ee/db/9781498772327.html
Märksõnad:

Introduction to Rocket Science and Engineering, Second Edition, presents the history and basics of rocket science, and examines design, experimentation, testing, and applications. Exploring how rockets work, the book covers the concepts of thrust, momentum, impulse, and the rocket equation, along with the rocket engine, its components, and the physics involved in the generation of the propulsive force. The text also presents several different types of rocket engines and discusses the testing of rocket components, subsystems, systems, and complete products. The final chapter stresses the importance for rocket scientists and engineers to creatively deal with the complexities of rocketry.

Arvustused

"This book is an excellent reference for the rocket enthusiast and for anyone interested in participating in any kind of rocket competition. It is a very useful complement to the library of anyone teaching a rocket class." Riccardo Bonazza, University of Wisconsin Madison, USA

List of Figures
xiii
List of Tables
xxv
Preface xxvii
Author xxix
Introduction xxxi
1 What Are Rockets?
1(38)
1.1 The History of Rockets
1(19)
1.1.1 400 BCE
1(1)
1.1.2 100 to 0 BCE
2(1)
1.1.3 0 to 100 AD
2(1)
1.1.4 850 AD
3(1)
1.1.5 904 AD
3(1)
1.1.6 1132 to 1279 AD
3(1)
1.1.7 1300 to 1600 AD
4(1)
1.1.8 1600 to 1800 AD
4(1)
1.1.9 1800 to 1900 AD
5(1)
1.1.10 1900 to 1930 AD
6(1)
1.1.10 1 A Perspective
7(1)
1.1.11 1930 to 1957 AD
7(2)
1.1.12 1957 to 1961 AD
9(3)
1.1.13 1961 to Present
12(5)
1.1.14 X PRIZE
17(1)
1.1.15 Other Space Agencies
18(2)
1.2 Rockets of the Modern Era
20(13)
1.2.1 ESA and CNES
20(1)
1.2.2 ISRO (India)
21(1)
1.2.3 ISA (Iran)
21(1)
1.2.4 Israeli Space Agency
22(1)
1.2.5 JAXA (Japan)
22(1)
1.2.6 CNSA (People's Republic of China)
23(1)
1.2.7 Russian FSA (also known as RKA in Russian---Russia/Ukraine)
24(1)
1.2.8 United States of America: NASA and the U.S. Air Force
25(2)
1.2.9 Other Systems Are on the Way
27(2)
1.2.10 NASA Constellation Program
29(3)
1.2.11 NASA SLS Program
32(1)
1.3 Rocket Anatomy and Nomenclature
33(4)
1.4
Chapter Summary
37(2)
Exercises
38(1)
2 Why Are Rockets Needed?
39(40)
2.1 Missions and Payloads
39(3)
2.1.1 Missions
40(1)
2.1.2 Payloads
40(2)
2.2 Trajectories
42(7)
2.2.1 Example 2.1: Hobby Rocket
43(3)
2.2.2 Fundamental Equations for Trajectory Analysis
46(1)
2.2.3 Missing the Earth
47(1)
2.2.4 Example 2.2: Dong Feng 31 ICBM
47(2)
2.3 Orbits
49(16)
2.3.1 Newton's Universal Law of Gravitation
49(1)
2.3.2 Example 2.3: Acceleration due to Gravity on a Telecommunications Satellite
50(2)
2.3.3 A Circular Orbit
52(3)
2.3.4 The Circle Is a Special Case of an Ellipse
55(2)
2.3.5 The Ellipse Is Actually a Conic Section
57(1)
2.3.6 Kepler's Laws
58(3)
2.3.7 Newton's Vis Viva Equation
61(4)
2.4 Orbit Changes and Maneuvers
65(9)
2.4.1 In-Plane Orbit Changes
65(2)
2.4.2 Example 2.4: Hohmann Transfer Orbit
67(1)
2.4.3 Bielliptical Transfer
68(1)
2.4.4 Plane Changes
69(1)
2.4.5 Interplanetary Trajectories
69(2)
2.4.6 Gravitational Assist
71(3)
2.5 Ballistic Missile Trajectories
74(1)
2.5.1 Ballistic Missile Trajectories Are Conic Sections
74(1)
2.6
Chapter Summary
75(4)
Exercises
76(3)
3 How Do Rockets Work?
79(38)
3.1 Thrust
79(3)
3.2 Specific Impulse
82(3)
3.2.1 Example 3.1: Isp of the Space Shuttle Main Engines
85(1)
3.3 Weight Flow Rate
85(1)
3.4 Tsiolkovsky's Rocket Equation
86(5)
3.5 Staging
91(3)
3.5.1 Example 3.2: Two-Stage Rocket
93(1)
3.6 Rocket Dynamics, Guidance, and Control
94(18)
3.6.1 Aerodynamic Forces
95(2)
3.6.2 Example 3.3: Drag Force on the Space Shuttle
97(1)
3.6.3 Rocket Stability and the Restoring Force
97(5)
3.6.4 Rocket Attitude Control Systems
102(1)
3.6.5 Eight Degrees of Freedom
103(3)
3.6.6 Inverted Pendulum
106(6)
3.7
Chapter Summary
112(5)
Exercises
113(4)
4 How Do Rocket Engines Work?
117(28)
4.1 Basic Rocket Engine
117(2)
4.2 Thermodynamic Expansion and the Rocket Nozzle
119(6)
4.2.1 Isentropic Flow
121(4)
4.3 Exit Velocity
125(7)
4.4 Rocket Engine Area Ratio and Lengths
132(6)
4.4.1 Nozzle Area Expansion Ratio
132(1)
4.4.2 Nozzle Design
133(2)
4.4.3 Properly Designed Nozzle
135(2)
4.4.4 Expansion Chamber Dimensions
137(1)
4.5 Rocket Engine Design Example
138(5)
4.6
Chapter Summary
143(2)
Exercises
143(2)
5 Are All Rockets the Same?
145(44)
5.1 Solid Rocket Engines
145(6)
5.1.1 Basic Solid Motor Components
146(2)
5.1.2 Solid Propellant Composition
148(1)
5.1.3 Solid Propellant Grain Configurations
148(1)
5.1.4 Burn Rate
149(2)
5.1.4.1 Example 5.1: Burn Rate of the Space Shuttle SRBs
151(1)
5.2 Liquid Propellant Rocket Engines
151(5)
5.2.1 Cavitation
154(1)
5.2.2 Pogo
154(1)
5.2.3 Cooling the Engine
155(1)
5.2.4 A Real-World Perspective: The SSME Ignition Sequence
156(1)
5.3 Hybrid Rocket Engines
156(2)
5.4 Electric Rocket Engines
158(17)
5.4.1 Electrostatic Engines
158(2)
5.4.2 Example 5.2: The Deep Space Probe's NASA Solar Technology Application Readiness Ion Engine
160(3)
5.4.3 Electrothermal Engines
163(1)
5.4.4 Electromagnetic Engines
164(2)
5.4.5 Example 5.3: The PPT Engine
166(3)
5.4.6 Solar Electric Propulsion
169(1)
5.4.7 Nuclear Electric Propulsion
170(5)
5.5 Nuclear Rocket Engines
175(3)
5.5.1 Solid Core
175(2)
5.5.2 Liquid Core
177(1)
5.5.3 Gas Core
177(1)
5.6 Solar Rocket Engines
178(3)
5.6.1 Example 5.4: The Solar Thermal Collector
178(1)
5.6.2 Example 5.5: The STR Exit Velocity, Isp, and Thrust
179(2)
5.7 Photon-Based Engines
181(5)
5.8
Chapter Summary
186(3)
Exercises
187(2)
6 How Do We Test Rockets?
189(50)
6.1 Systems Engineering Process and Rocket Development
190(8)
6.1.1 Systems Engineering Models
193(2)
6.1.2 Technology, Integrated, and Systems Readiness
195(3)
6.2 Measuring Thrust
198(12)
6.2.1 Deflection-Type Thrustometers
199(2)
6.2.2 Hydraulic Load Cells
201(1)
6.2.3 Strain Gauge Load Cells
201(9)
6.3 Pressure Vessel Tests
210(8)
6.4 Shake `n' Bake Tests
218(1)
6.5 Drop and Landing Tests
219(3)
6.6 Environment Tests
222(3)
6.7 Destructive Tests
225(1)
6.8 Modeling and Simulation
226(1)
6.9 Roll-Out Test
227(1)
6.10 Flight Tests
227(8)
6.10.1 Logistics
229(1)
6.10.2 Flight Testing Is Complicated
230(5)
6.11
Chapter Summary
235(4)
Exercises
236(3)
7 How Do We Design Rockets?
239(26)
7.1 Designing a Rocket
239(12)
7.1.1 Derived Requirements
240(2)
7.1.2 OpenRocket
242(1)
7.1.2.1 OpenRocket Step #1: Choose a Body Tube for the First Stage
242(1)
7.1.2.2 OpenRocket Step #2: Choose an Inner Tube Engine Mount and Engine for the First Stage
242(1)
7.1.2.3 OpenRocket Step #3: Fix the Center of Gravity (cg) and the Center of Pressure (cp)
242(1)
7.1.2.4 OpenRocket Step #4: Add New Stage
243(1)
7.1.2.5 OpenRocket Step #5: Add New Stage
243(1)
7.1.2.6 OpenRocket Step #6: Finish the Top and Place the Payload
243(1)
7.1.2.7 OpenRocket Step #7: Simulate, Modify, Simulate, Modify
243(1)
7.1.2.8 OpenRocket Step #8: Realization
244(4)
7.1.3 From OpenRocket to Real Design
248(1)
7.1.4 Fineness Ratio and Structural Design
249(2)
7.2 Designing Bigger Rockets
251(9)
7.2.1 DRM #2: Orbital Liquid-Fueled Rocket
251(9)
7.3 Reverse Bifurcation Designing
260(2)
7.4
Chapter Summary
262(3)
Exercises
262(3)
8 How Reliable Are Rockets?
265(12)
8.1 Probability and Parts Count
265(3)
8.1.1 The Probability of Success and Quality Control
266(1)
8.1.2 Single Point Failure
267(1)
8.2 Testing Our Rockets for Reliability
268(1)
8.2.1 Reliability versus Testing
268(1)
8.3 Redundant Systems and Reliability
269(5)
8.3.1 Reliability Is Costly
270(1)
8.3.2 Reliability and Series Systems
271(1)
8.3.3 Reliability and Parallel Systems
271(1)
8.3.4 Reliability and Mixed Series and Parallel Systems
272(2)
8.4
Chapter Summary
274(3)
Exercises
274(3)
9 Are We Thinking Like Rocket Scientists and Engineers?
277(24)
9.1 Weather Cocking
277(3)
9.2 Propellant Sloshing
280(1)
9.3 Propellant Vorticity
281(3)
9.4 Tornadoes and Overpasses
284(1)
9.5 Flying Foam Debris
285(2)
9.6 Monocoque
287(2)
9.7 Space Mission Analysis and Design Process
289(2)
9.8 "Back to the Moon"
291(8)
9.9 A Perspective on the Big Picture, Rockets, and Dinosaurs
299(2)
9.10
Chapter Summary
301(1)
Exercises 301(2)
Suggested Reading for Rocket Scientists and Engineers 303(2)
Index 305
Travis S. Taylor has worked on various projects for NASA and the U.S. Department of Defense, including advanced propulsion concepts, space-based beamed energy systems, space launch concepts, and large space telescopes. Dr. Taylor was also one of the principle investigators for the Ares I Flight Test Planning effort for NASA Marshall Space Center. He holds a doctorate in Optical Science & Engineering from the University of Alabama - Huntsville, and additional degrees in Electrical Engineering, Physics, Aerospace Engineering, and Astronomy. Dr. Taylor is also known for his television shows - "Rocket City Rednecks" (National Geographic Network) and "Three Scientists Walk Into a Bar" (the Weather Channel). He has also written several science fiction novels, and two college textbooks. He and his family live in northern Alabama, within sight of the Saturn V rocket that's on exhibit at the untsville space flight center.