Rocket and spacecraft propulsion: principles, practice and new developments
Gespeichert in:
| 1. Verfasser: | |
|---|---|
| Format: | Elektronisch E-Book |
| Sprache: | English |
| Veröffentlicht: |
Berlin
Springer Berlin
2009
|
| Ausgabe: | 3. ed |
| Schriftenreihe: | Springer Praxis Books Astronautical Engineering
|
| Schlagworte: | |
| Online-Zugang: | TUM01 Volltext Inhaltsverzeichnis |
| Beschreibung: | 1 Online-Ressource (XXVI, 414 S.) |
| ISBN: | 9783540692034 |
| DOI: | 10.1007/978-3-540-69203-4 |
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Datensatz im Suchindex
| _version_ | 1804138514261999616 |
|---|---|
| adam_text | CONTENTS PREFACE TO THE THIRD EDITION XI PREFACE TO THE SECOND EDITION
XIII PREFACE TO THE FIRST EDITION XV ACKNOWLEDGEMENTS XVII LIST OF
FLGURES XIX LIST OF TABLES XXIII LIST OF COLOUR PLATES XXV 1 HISTORY AND
PRINCIPLES OF ROCKET PROPULSION ] 1.1 THE DEVELOPMENT OF THE ROCKET 1
1.1.1 THE RUSSIAN SPACE PROGRAMME 6 1.1.2 OTHER NATIONAL PROGRAMMES 6
1.1.3 THE UNITED STATES SPACE PROGRAMME 8 1.1.4 COMMENTARY 13 1.2
NEWTON S THIRD LAW AND THE ROCKET EQUATION 14 1.2.1 TSIOLKOVSKY S ROCKET
EQUATION 14 1.3 ORBITS AND SPACEFLIGHT 17 1.3.1 ORBITS 18 1.4 MULTISTAGE
ROCKETS 25 1.4.1 OPTIMISING A MULTISTAGE ROCKET 28 1.4.2 OPTIMISING THE
ROCKET ENGINES 30 1.4.3 STRAP-ON BOOSTERS 32 1.5 ACCESS TO SPACE 34
BIBLIOGRAFISCHE INFORMATIONEN HTTP://D-NB.INFO/990586766 DIGITALISIERT
DURCH VI CONTENTS 2 THE THERMAL ROCKET ENGINE * * . 37 2.1 THE BASIC
CONFIGURATION 37 2.2 THE DEVELOPMENT OF THRUST AND THE EFFECT OF THE
ATMOSPHERE ... 39 2.2.1 OPTIMISING THE EXHAUST NOZZLE 43 2.3 THE
THERMODYNAMICS OF THE ROCKET ENGINE 44 2.3.1 EXHAUST VELOCITY 46 2.3.2
MASS FLOW RATE 48 2.4 THE THERMODYNAMIC THRUST EQUATION 53 2.4.1 THE
THRUST COEFFICIENT AND THE CHARACTERISTIC VELOCITY. ... 54 2.5 COMPUTING
ROCKET ENGINE PERFORMANCE 58 2.5.1 SPECIFIC IMPULSE 59 2.5.2 EXAMPLE
CALCULATIONS 60 2.6 WORKED EXAMPLE. ... 62 2.7 SUMMARY 65 LIQUID
PROPELLANT ROCKET ENGINES 67 3.1 THE BASIC CONFIGURATION OF THE LIQUID
PROPELLANT ENGINE . 67 3.2 THE COMBUSTION CHAMBER AND NOZZLE 68 3.2.1
INJECTION 69 3.2.2 IGNITION 70 3.2.3 COMBUSTION INSTABILITY 73 3.2.4
THRUST VECTOR CONTROL 78 3.3 LIQUID PROPELLANT DISTRIBUTION SYSTEMS 81
3.3.1 CAVITATION 83 3.3.2 POGO 84 3.4 COOLING OF LIQUID-FUELLED ROCKET
ENGINES 85 3.5 EXAMPLES OF ROCKET ENGINE PROPELLANT FLOW 86 3.5.1 THE
AESTUS ENGINE ON ARIANE 5 . 87 3.5.2 THE ARIANE VIKING ENGINES 88 3.5.3
THE ARIANE HM7 B ENGINE . 90 3.5.4 THE VINCI CRYOGENIC UPPER-STAGE
ENGINE FOR ARIANE 5 91 3.5.5 THE ARIANE 5 VULCAIN CRYOGENIC ENGINE 92
3.5.6 THE SPACE SHUTTLE MAIN ENGINE 93 3.5.7 THE RS 68 ENGINE 96 3.5.8
THE RL 10 ENGINE 96 3. CONTENTS VII SOLID PROPELLANT ROCKET MOTORS 109
4.1 BASIC CONFIGURATION 109 4.2 THE PROPERTIES AND THE DESIGN OF SOLID
MOTORS 111 4.3 PROPELLANT COMPOSITION 112 4.3.1 ADDITIVES 114 4.3.2
TOXIC EXHAUST 115 4.3.3 THRUST STABILITY 115 4.3.4 THRUST PROFILE AND
GRAIN SHAPE 116 4.4 INTEGRITY OF THE COMBUSTION CHAMBER 118 4.4.1
THERMAL PROTECTION 119 4.4.2 INTER-SECTION JOINTS 120 4.4.3 NOZZLE
THERMAL PROTECTION 122 4.5 IGNITION 122 4.6 THRUST VECTOR CONTROL 123
4.7 TWO MODERN SOLID BOOSTERS 123 4.7.1 THE SPACE SHUTTLE SRB 123 4.7.2
THE ARIANE MPS 125 4.8 HYBRID ROCKET MOTORS 126 4.8.1 HYBRID MOTOR
HISTORY 127 4.8.2 THE BASIC CONFIGURATION OF A HYBRID MOTOR 128 4.8.3
PROPELLANTS AND IGNITION 128 4.8.4 COMBUSTION 130 4.8.5 GRAIN
CROSS-SECTION 131 4.8.6 PROPULSIVE EFFICIENCY 132 4.8.7 INCREASING THE
THRUST 133 LAUNCH VEHICLE DYNAMICS 135 5.1 MORE ON THE ROCKET EQUATION
135 5.1.1 RANGE IN THE ABSENCE OF GRAVITY 137 5.2 VERTICAL MOTION IN THE
EARTH S GRAVITATIONAL FIELD 140 5.2.1 VEHICLE VELOCITY 140 5.2.2 RANGE
143 5.3 INCLINED MOTION IN A GRAVITATIONAL FIELD 144 5.3.1 CONSTANT
PITCH ANGLE 144 5.3.2 THE FLIGHT PATH AT CONSTANT PITCH ANGLE 146 5.4
MOTION IN THE ATMOSPHERE 148 5.4.1 AERODYNAMIC FORCES 149 5.4.2 DYNAMIC
PRESSURE 150 5. VIII CONTENTS 5.7.4 ORBITAL INJECTION 157 5.8 ACTUAL
LAUNCH VEHICLE TRAJECTORIES 159 5.8.1 THE MU-3-S-II LAUNCHER 159 5.8.2
ARIANE 4 .... 162 5.8.3 PEGASUS 163 6 ELECTRIC PROPULSION 165 6.1 THE
IMPORTANCE OF EXHAUST VELOCITY 165 6.2 REVIVED INTEREST IN ELECTRIC
PROPULSION 167 6.3 PRINCIPLES OF ELECTRIC PROPULSION 167 6.3.1 ELECTRIC
VEHICLE PERFORMANCE 168 6.3.2 VEHICLE VELOCITY AS A FUNCTION OF EXHAUST
VELOCITY 169 6.3.3 VEHICLE VELOCITY AND STRUCTURAL/PROPELLANT MASS 170
6.4 ELECTRIC THRUSTERS 171 6.4.1 ELECTROTHERMAL THRUSTERS 172 6.4.2
ARC-JET THRUSTERS 175 6.5 ELECTROMAGNETIC THRUSTERS 177 6.5.1 ION
PROPULSION 178 6.5.2 THE SPACE CHARGE LIMIT 180 6.5.3 ELECTRIC FIELD AND
POTENTIAL 182 6.5.4 ION THRUST 183 6.5.5 PROPELLANT CHOICE 184 6.5.6
DECELERATION GRID 186 6.5.7 ELECTRICAL EFFICIENCY 186 6.6 PLASMA
THRUSTERS 189 6.6.1 HALL EFFECT THRUSTERS 191 6.6.2 RADIOFREQUENCY
THRUSTERS 197 6.7 LOW-POWER ELECTRIC THRUSTERS 199 6.8 ELECTRICAL POWER
GENERATION 200 6.8.1 SOLAR CELLS 200 6.8.2 SOLAR GENERATORS 201 6.8.3
RADIOACTIVE THERMAL GENERATORS 202 6.8.4 NUCLEAR FISSION POWER
GENERATORS 204 6.9 APPLICATIONS OF ELECTRIC PROPULSION 206 6.9.1 STATION
KEEPING 209 6.9.2 LOW EARTH ORBIT TO GEOSTATIONARY ORBIT 210 6.9.3
NINE-MONTH ONE-WAY MISSION TO MARS 211 6.9. CONTENTS IX 7.3 A
SUSTAINABLE CHAIN REACTION 224 7.4 CALCULATING THE CRITICALITY 225 7.5
THE REACTOR DIMENSIONS AND NEUTRON LEAKAGE 228 7.6 CONTROL 231 7.7
REFLECTION 233 7.8 PROMPT AND DELAYED NEUTRONS 233 7.9 THERMAL STABILITY
234 7.10 THE PRINCIPLE OF NUCLEAR THERMAL PROPULSION 235 7.11 THE FUEL
ELEMENTS 237 7.12 EXHAUST VELOCITY OF A NUCLEAR THERMAL ROCKET 239 7.13
INCREASING THE OPERATING TEMPERATURE 240 7.14 THE NUCLEAR THERMAL ROCKET
ENGINE 243 7.14.1 RADIATION AND ITS MANAGEMENT 244 7.14.2 PROPELLANT
FLOW AND COOLING 246 7.14.3 THE CONTROL DRUMS 248 7.14.4 START-UP AND
SHUT-DOWN 249 7.14.5 THE NOZZLE AND THRUST GENERATION 250 7.15 POTENTIAL
APPLICATIONS OF NUCLEAR ENGINES 251 7.16 OPERATIONAL ISSUES WITH THE
NUCLEAR ENGINE 252 7.17 INTERPLANETARY TRANSFER MANOEUVRES 253 7.18
FASTER INTERPLANETARY JOURNEYS 255 7.19 HYDROGEN STORAGE 256 7.20
DEVELOPMENT STATUS OF NUCLEAR THERMAL ENGINES 258 7.21 ALTERNATIVE
REACTOR TYPES 264 7.22 SAFETY ISSUES 265 7.23 NUCLEAR PROPELLED MISSIONS
269 8 ADVANCED THERMAL ROCKETS 271 8.1 FUNDAMENTAL PHYSICAL LIMITATIONS
271 8.1.1 DYNAMICA] FACTORS 27) 8.2 IMPROVING EFFICIENCY 274 8.2.1
EXHAUST VELOCITY 274 8.3 THERMAL ROCKETS IN ATMOSPHERE, AND THE SINGLE
STAGE TO ORBIT . . . 277 8.3. X CONTENTS 8.8 SSTO CONCEPTS 299 8.8.1 THE
USE OF AERODYNAMIC LIFT FOR ASCENT 300 9 HUMAN SPACE FLIGHT AND
PLANETARY EXPLORATION 303 9.1 LAUNCH SYSTEMS FOR HUMAN SPACE FLIGHT 303
9.1.1 ESTABLISHING THE RELIABILITY OF COMPONENTS 305 9.1.2 THE TEST
PROGRAMME 306 9.2 CREWED LAUNCHERS AND RE-ENTRY VEHICLES 310 9.3 PROJECT
CONSTELLATION, THE NEW NASA HUMAN SPACE FLIGHT PRO- GRAMME 334 9.3.1 THE
ORION SPACECRAFT 336 9.3.2 THE ARES I LAUNCHER 339 9.3.3 THE ARES V
LAUNCHER 342 9.4 SOFT LANDING AND PLANETARY EXPLORATION 343 9.4.1 THE
CHALLENGE OF DEEP THROTTLING 346 9.4.2 DEEP THROTTLING WITH CRYOGENIC
PROPELLANTS 348 APPENDICES A ORBITAL MOTION 351 B LAUNCHER SURVEY 357 C
ARIANE 5 373 D GLOSSARY OF SYMBOLS 379 FURTHER READING 383 INDEX 385
|
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| spelling | Turner, Martin J. L. 1942- Verfasser (DE-588)121556190 aut Rocket and spacecraft propulsion principles, practice and new developments Martin J. Turner 3. ed Berlin Springer Berlin 2009 1 Online-Ressource (XXVI, 414 S.) txt rdacontent c rdamedia cr rdacarrier Springer Praxis Books Astronautical Engineering Raketentriebwerk (DE-588)4176905-3 gnd rswk-swf Raketentriebwerk (DE-588)4176905-3 s DE-604 Erscheint auch als Druck-Ausgabe 978-3-540-69202-7 https://doi.org/10.1007/978-3-540-69203-4 Verlag Volltext DNB Datenaustausch application/pdf http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&local_base=BVB01&doc_number=017047346&sequence=000001&line_number=0001&func_code=DB_RECORDS&service_type=MEDIA Inhaltsverzeichnis |
| spellingShingle | Turner, Martin J. L. 1942- Rocket and spacecraft propulsion principles, practice and new developments Raketentriebwerk (DE-588)4176905-3 gnd |
| subject_GND | (DE-588)4176905-3 |
| title | Rocket and spacecraft propulsion principles, practice and new developments |
| title_auth | Rocket and spacecraft propulsion principles, practice and new developments |
| title_exact_search | Rocket and spacecraft propulsion principles, practice and new developments |
| title_full | Rocket and spacecraft propulsion principles, practice and new developments Martin J. Turner |
| title_fullStr | Rocket and spacecraft propulsion principles, practice and new developments Martin J. Turner |
| title_full_unstemmed | Rocket and spacecraft propulsion principles, practice and new developments Martin J. Turner |
| title_short | Rocket and spacecraft propulsion |
| title_sort | rocket and spacecraft propulsion principles practice and new developments |
| title_sub | principles, practice and new developments |
| topic | Raketentriebwerk (DE-588)4176905-3 gnd |
| topic_facet | Raketentriebwerk |
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