About the Author | p. xi |
Preface | p. xiii |
What Are Rockets? | p. 1 |
The History of Rockets | p. 1 |
400 BCE | p. 1 |
100 to 0 BCE | p. 2 |
0 to 100 AD | p. 3 |
850 AD | p. 3 |
904 AD | p. 3 |
1132 to 1279 AD | p. 3 |
1300 to 1600 AD | p. 4 |
1600 to 1800 AD | p. 5 |
1800 to 1900 AD | p. 5 |
1900 to 1930 AD | p. 6 |
A Perspective | p. 9 |
1930 to 1957 AD | p. 9 |
1957 to 1961 AD | p. 10 |
1961 to Present | p. 14 |
X Prize | p. 18 |
Other Space Agencies | p. 21 |
Rockets of the Modern Era | p. 22 |
ESA and CNES | p. 23 |
Indian Space Research Organization (ISRO-India) | p. 23 |
Iranian Space Agency (ISA-Iran) | p. 24 |
Israeli Space Agency | p. 25 |
Japan Aerospace exploration Agency (JAXA-Japan) | p. 25 |
China National Space Administration (CNSA- People's Republic of China) | p. 26 |
Russian Federal Space Agency (FSA, also known as RKA in Russian-Russia/Ukraine) | p. 27 |
United States of America: NASA and the U.S. Air Force | p. 28 |
Other Systems Are on the Way | p. 31 |
The NASA Constellation Program | p. 31 |
Rocket Anatomy and Nomenclature | p. 36 |
Chapter Summary | p. 40 |
Exercises | p. 42 |
Why Are Rockets Needed? | p. 43 |
Missions and Payloads | p. 43 |
Missions | p. 44 |
Payloads | p. 45 |
Trajectories | p. 47 |
Example 2.1: Hobby Rocket | p. 47 |
Fundamental Equations for Trajectory Analysis | p. 51 |
Missing the Earth | p. 53 |
Example 2.2: The Dong Feng 31 ICBM | p. 54 |
Orbits | p. 54 |
Newton's Universal Law of Gravitation | p. 54 |
Example 2.3: Acceleration Due to Gravity on a Telecommunications Satellite | p. 56 |
A Circular Orbit | p. 58 |
The Circle Is a Special Case of an Ellipse | p. 62 |
The Ellipse Is Actually a Conic Section | p. 64 |
Kepler's Laws | p. 66 |
Newton's Vis Viva Equation | p. 69 |
Orbit Changes and Maneuvers | p. 73 |
In-Plane Orbit Changes | p. 73 |
Example 2.4: The Hohmann Transfer Orbit | p. 75 |
The Bielliptical Transfer | p. 78 |
Plane Changes | p. 78 |
Interplanetary Trajectories | p. 79 |
The Gravitational Assist | p. 81 |
Ballistic Missile Trajectories | p. 83 |
Ballistic Missile Trajectories Are Conic Sections | p. 83 |
Chapter Summary | p. 85 |
Exercises | p. 86 |
How Do Rockets Work? | p. 89 |
Thrust | p. 89 |
Specific Impulse | p. 92 |
Example 3.1: Isp of the Space Shuttle Main Engines | p. 95 |
Weight Flow Rate | p. 95 |
Tsiolkovsky's Rocket Equation | p. 98 |
Staging | p. 103 |
Example 3.2: The Two-Stage Rocket | p. 107 |
Rocket Dynamics, Guidance, and Control | p. 108 |
Aerodynamic Forces | p. 108 |
Example 3.3: Drag Force on the Space Shuttle | p. 110 |
Rocket Stability and the Restoring Force | p. 110 |
Rocket Attitude Control Systems | p. 116 |
8 Degrees of Freedom | p. 117 |
Chapter Summary | p. 120 |
Exercises | p. 122 |
How Do Rocket Engines Work? | p. 125 |
The Basic Rocket Engine | p. 125 |
Thermodynamic Expansion and the Rocket Nozzle | p. 128 |
Isentropic Flow | p. 130 |
Exit Velocity | p. 134 |
Rocket Engine Area Ratio and Lengths | p. 141 |
Nozzle Area Expansion Ratio | p. 141 |
Nozzle Design | p. 143 |
The Properly Designed Nozzle | p. 147 |
Expansion Chamber Dimensions | p. 148 |
Rocket Engine Design Example | p. 150 |
Chapter Summary | p. 154 |
Exercises | p. 155 |
Are All Rockets the Same? | p. 157 |
Solid Rocket Engines | p. 157 |
Basic Solid Motor Components | p. 158 |
Solid Propellant Composition | p. 161 |
Solid Propellant Grain Configurations | p. 161 |
Burn Rate | p. 162 |
Example 5.1: Burn Rate of the Space Shuttle SRBs | p. 164 |
Liquid Propellant Rocket Engines | p. 165 |
Cavitation | p. 167 |
Pogo | p. 168 |
Cooling the Engine | p. 169 |
A Real World Perspective: The SSME Ignition Sequence | p. 170 |
Hybrid Rocket Engines | p. 170 |
Electric Rocket Engines | p. 171 |
Electrostatic Engines | p. 172 |
Example 5.2: The Deep Space Probe's NSTAR Ion Engine | p. 175 |
Electrothermal Engines | p. 178 |
Electromagnetic Engines | p. 179 |
Example 5.3: The Pulsed Plasma Thruster (PPT) Engine | p. 182 |
Solar Electric Propulsion | p. 185 |
Nuclear Electric Propulsion | p. 186 |
Nuclear Rocket Engines | p. 193 |
Solid Core | p. 193 |
Liquid Core | p. 194 |
Gas Core | p. 195 |
Solar Rocket Engines | p. 195 |
Example 5.4: The Solar Thermal Collector | p. 196 |
Example 5.5: The STR Exit Velocity, Isp, and Thrust | p. 198 |
Photon-Based Engines | p. 200 |
Chapter Summary | p. 206 |
Exercises | p. 207 |
How Do We Test Rockets? | p. 209 |
The Systems Engineering Process and Rocket Development | p. 210 |
Systems Engineering Models | p. 213 |
Technology, Integrated, and Systems Readiness | p. 215 |
Measuring Thrust | p. 219 |
Deflection-Type Thrustometers | p. 220 |
Hydraulic Load Cells | p. 223 |
Strain Gauge Load Cells | p. 224 |
Pressure Vessel Tests | p. 229 |
Shake 'n Bake Tests | p. 241 |
Drop and Landing Tests | p. 243 |
Environment Tests | p. 246 |
Destructive Tests | p. 248 |
Modeling and Simulation | p. 250 |
Roll-Out Test | p. 251 |
Flight Tests | p. 253 |
Logistics | p. 256 |
Flight Testing Is Complicated | p. 257 |
Chapter Summary | p. 263 |
Exercises | p. 264 |
Are We Thinking Like Rocket Scientists and Engineers? | p. 267 |
Weather Cocking | p. 268 |
Fuel Sloshing | p. 270 |
Propellant Vorticity | p. 272 |
Tornadoes and Overpasses | p. 276 |
Flying Foam Debris | p. 277 |
Monocoque | p. 279 |
The Space Mission Analysis and Design Process | p. 280 |
Back to the Moon | p. 283 |
Chapter Summary | p. 294 |
Exercises | p. 294 |
Suggested Reading for Rocket Scientists and Engineers | p. 297 |
Index | p. 299 |
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