Rocket and spacecraft propulsion: principles, practice and new developments
Gespeichert in:
| 1. Verfasser: | |
|---|---|
| Format: | Buch |
| Sprache: | English |
| Veröffentlicht: |
Berlin [u.a.]
Springer
2005
|
| Ausgabe: | 2. ed. |
| Schriftenreihe: | Springer Praxis books in astronautical engineering
|
| Schlagworte: | |
| Online-Zugang: | Inhaltsverzeichnis |
| Beschreibung: | XXII, 313 S. Ill., graph. Darst. |
| ISBN: | 3540221905 |
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Datensatz im Suchindex
| _version_ | 1804138993622712320 |
|---|---|
| adam_text | MARTIN J. L. TURNER ROCKET AND SPACECRAFT PROPULSION PRINCIPLES,
PRACTICE AND NEW DEVELOPMENTS (SECOND EDITION) FUDIISNEA IN ASSOCIATION
WITN SPRINGER PRAXIS PUBLISHING PUBLISHED IN ASSOCIATION WITH RIS
PUBLISL CHICHESTER, UK CONTENTS PREFACE TO THE SECOND EDITION XIII
PREFACE TO THE FIRST EDITION XV ACKNOWLEDGEMENTS XVII LIST OF FIGURES
XIX LIST OF TABLES XXIII LIST OF COLOUR PLATES XXV 1 HISTORY AND
PRINCIPLES OF ROCKET PROPULSION 1 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 : 31 1.5 ACCESS
TO SPACE 34 VIII CONTENTS 2 THE THERMAL ROCKET ENGINE 35 2.1 THE BASIC
CONFIGURATION 35 2.2 THE DEVELOPMENT OF THRUST AND THE EFFECT OF THE
ATMOSPHERE 37 2.2.1 OPTIMISING THE EXHAUST NOZZLE 41 2.3 THE
THERMODYNAMICS OF THE ROCKET ENGINE 42 2.3.1 EXHAUST VELOCITY 43 2.3.2
MASS FLOW RATE 46 2.4 THE THERMODYNAMIC THRUST EQUATION 51 2.4.1 THE
THRUST COEFFICIENT AND THE CHARACTERISTIC VELOCITY 52 2.5 COMPUTING
ROCKET ENGINE PERFORMANCE 56 2.5.1 SPECIFIC IMPULSE 57 2.5.2 EXAMPLE
CALCULATIONS 58 2.6 SUMMARY 60 3 LIQUID PROPELLANT ROCKET ENGINES 61 3.1
THE BASIC CONFIGURATION OF THE LIQUID PROPELLANT ENGINE 61 3.2 THE
COMBUSTION CHAMBER AND NOZZLE 62 3.2.1 INJECTION 63 3.2.2 IGNITION 64
3.2.3 THRUST VECTOR CONTROL 67 3.3 LIQUID PROPELLANT DISTRIBUTION
SYSTEMS 69 3 3.1 CAVITATION 71 3.3.2 POGO 71 3.4 COOLING OF
LIQUID-FUELLED ROCKET ENGINES 72 3.5 EXAMPLES OF ROCKET ENGINE
PROPELLANT FLOW 74 3.5.1 THE AESTUS ENGINE ON ARIANE 5 74 3.5.2 THE
ARIANE VIKING ENGINES 75 3.5.3 THE ARIANE HM7 B ENGINE 77 3.5.4 THE
VINCI CRYOGENIC UPPER-STAGE ENGINE FOR ARIANE 5 78 3.5.5 THE ARIANE 5
VULCAIN CRYOGENIC ENGINE 78 3.5.6 THE SPACE SHUTTLE MAIN ENGINE 81 3.5.7
THE RS 68 ENGINE 83 3.5.8 THE RL 10 ENGINE 85 3.6 COMBUSTION AND THE
CHOICE OF PROPELLANTS 86 3.6.1 COMBUSTION TEMPERATURE 86 3.6.2 MOLECULAR
WEIGHT 87 3.6.3 PROPELLANT PHYSICAL PROPERTIES 88 3.7 THE PERFORMANCE OF
LIQUID-FUELLED ROCKET ENGINES 90 3.7.1 LIQUID OXYGEN-LIQUID HYDROGEN
ENGINES 91 3.7.2 LIQUID HYDROCARBON-LIQUID OXYGEN ENGINES 93 3.7.3
STORABLE PROPELLANT ENGINES 93 4 SOLID PROPELLANT ROCKET MOTORS 97 4.1
BASIC CONFIGURATION ! . . . . 97 4.2 THE PROPERTIES AND THE DESIGN OF
SOLID MOTORS 99 CONTENTS IX 4.3 PROPELLANT COMPOSITION 100 4.3.1
ADDITIVES 102 4.3.2 TOXIC EXHAUST 103 4.3.3 THRUST STABILITY 103 4.3.4
THRUST PROFILE AND GRAIN SHAPE 104 4.4 INTEGRITY OF THE COMBUSTION
CHAMBER 106 4.4.1 THERMAL PROTECTION 107 4.4.2 INTER-SECTION JOINTS 109
4.4.3 NOZZLE THERMAL PORTECTION 110 4.5 IGNITION 110 4.6 THRUST VECTOR
CONTROL ILL 4.7 TWO MODERN SOLID BOOSTERS ILL 4.7.1 THE SPACE SHUTTLE
SRB ILL 4.7.2 THE ARIANE MPS 113 5 LAUNCH VEHICLE DYNAMICS 115 5.1 MORE
ON THE ROCKET EQUATION 115 5.1.1 RANGE IN THE ABSENCE OF GRAVITY 117 5.2
VERTICAL MOTION IN THE EARTH S GRAVITATIONAL FIELD 120 5.2.1 VEHICLE
VELOCITY 120 5.2.2 RANGE 122 5.3 INCLINED MOTION IN A GRAVITATIONAL
FIELD 123 5.3.1 CONSTANT PITCH ANGLE 124 5.3.2 THE FLIGHT PATH AT
CONSTANT PITCH ANGLE 127 5.4 MOTION IN THE ATMOSPHERE 128 5.4.1
AERODYNAMIC FORCES 129 5.4.2 DYNAMIC PRESSURE 130 5.5 THE GRAVITY TURN
131 5.6 BASIC LAUNCH DYNAMICS 133 5.6.1 AIRLESS BODIES 133 5.7 TYPICAL
EARTH-LAUNCH TRAJECTORIES 135 5.7.1 THE VERTICAL SEGMENT OF THE
TRAJECTORY 136 5.7.2 THE GRAVITY TURN OR TRANSITION TRAJECTORY 136 5.7.3
CONSTANT PITCH OR THE VACUUM TRAJECTORY 137 5.7.4 ORBITAL INJECTION 137
5.8 ACTUAL LAUNCH VEHICLE TRAJECTORIES 139 5.8.1 THE MU-3-S-II LAUNCHER
: 139 5.8.2 ARIANE 4 141 5.8.3 PEGASUS 143 6 ELECTRIC PROPULSION 145 6.1
THE IMPORTANCE OF EXHAUST VELOCITY 145 6.2 REVIVED INTEREST IN ELECTRIC
PROPULSION 146 6.3 PRINCIPLES OF ELECTRIC PROPULSION. . .* 147 6.3.1
ELECTRIC VEHICLE PERFORMANCE 148 X CONTENTS 6.3.2 VEHICLE VELOCITY AS A
FUNCTION OF EXHAUST VELOCITY 149 6.3.3 VEHICLE VELOCITY AND
STRUCTURAL/PROPELLANT MASS 150 6.4 ELECTRIC THRUSTERS 152 6.4.1
ELECTROTHERMAL THRUSTERS 152 6.4.2 ARC-JET THRUSTERS 155 6.5
ELECTROMAGNETIC THRUSTERS 157 6.5.1 ION PROPULSION 158 6.5.2 THE SPACE
CHARGE LIMIT 160 6.5.3 ELECTRIC FIELD AND POTENTIAL 162 6.5.4 ION THRUST
163 6.5.5 PROPELLANT CHOICE 164 6.5.6 DECELERATION GRID 166 6.5.7
ELECTRICAL EFFICIENCY 166 6.6 PLASMA THRUSTERS 168 6.6.1 HALL EFFECT
THRUSTERS 170 6.6.2 RADIOFREQUENCY THRUSTERS 177 6.7 LOW-POWER ELECTRIC
THRUSTERS 179 6.8 ELECTRICAL POWER GENERATION 180 6.8.1 SOLAR CELLS 180
6.8.2 SOLAR GENERATORS 181 6.8.3 RADIOACTIVE THERMAL GENERATORS 181
6.8.4 NUCLEAR FISSION POWER GENERATORS 184 6.9 APPLICATIONS OF ELECTRIC
PROPULSION 187 6.9.1 STATION-KEEPING 189 6.9.2 LOW EARTH ORBIT TO
GEOSTATIONARY ORBIT 190 6.9.3 NINE-MONTH ONE-WAY MISSION TO MARS 191
6.9.4 GRAVITY LOSS AND THRUST 191 6.10 DEEP SPACE 1 AND THE NSTAR ION
ENGINE 193 6.11 SMART-1 AND THE PPS-1350 194 NUCLEAR PROPULSION 197 7.1
POWER, THRUST, AND ENERGY 197 7.2 NUCLEAR FISSION BASICS 199 7.3 A
SUSTAINABLE CHAIN REACTION 202 7.4 CALCULATING THE CRITICALITY 203 7.5
THE REACTOR DIMENSIONS AND NEUTRON LEAKAGE 205 7.6 CONTROL 209 7.7
REFLECTION 210 7.8 PROMPT AND DELAYED NEUTRONS 211 7.9 THERMAL STABILITY
F 212 7.10 THE PRINCIPLE OF NUCLEAR THERMAL PROPULSION 213 7.-11 THE
FUEL ELEMENTS 214 7.12 EXHAUST VELOCITY OF A NUCLEAR THERMAL ROCKET 1
.... 216 7.13 INCREASING THE OPERATING TEMPERATURE 218 CONTENTS XI 7.14
THE NUCLEAR THERMAL ROCKET ENGINE 221 7.14.1 RADIATION AND ITS
MANAGEMENT 221 7.14.2 PROPELLANT FLOW AND COOLING 224 7.14.3 THE CONTROL
DRUMS 226 7.14.4 START-UP AND SHUT-DOWN 227 7.14.5 THE NOZZLE AND THRUST
GENERATION 228 7.15 POTENTIAL APPLICATIONS OF NUCLEAR ENGINES 229 7.16
OPERATIONAL ISSUES WITH THE NUCLEAR ENGINE 230 7.17 INTERPLANETARY
TRANSFER MANOEUVRES 231 7.18 FASTER INTERPLANETARY JOURNEYS 232 7.19
HYDROGEN STORAGE 234 7.20 DEVELOPMENT STATUS OF NUCLEAR THERMAL ENGINES
235 7.21 ALTERNATIVE REACTOR TYPES 241 7.22 SAFETY ISSUES 243 7.23
NUCLEAR PROPELLED MISSIONS 246 8 ADVANCED THERMAL ROCKETS 249 8.1
FUNDAMENTAL PHYSICAL LIMITATIONS 249 8.1.1 DYNAMICAL FACTORS 249 8.2
IMPROVING EFFICIENCY 252 8.2.1 EXHAUST VELOCITY 252 8.3 THERMAL ROCKETS
IN ATMOSPHERE, AND THE SINGLE STAGE TO ORBIT .... 255 8.3.1 VELOCITY
INCREMENT FOR SINGLE STAGE TO ORBIT 256 8.3.2 OPTIMISING THE EXHAUST
VELOCITY IN ATMOSPHERE 258 8.3.3 THE ROCKET EQUATION FOR VARIABLE
EXHAUST VELOCITY 259 8.4 PRACTICAL APPROACHES TO SSTO 261 8.4.1 HIGH
MASS RATIO 261 8.5 PRACTICAL APPROACHES AND DEVELOPMENTS 263 8.5.1
ENGINES 264 8.6 VEHICLE DESIGN AND MISSION CONCEPT 272 8.6.1 OPTIMISING
THE ASCENT 272 8.6.2 OPTIMISING THE DESCENT 272 8.7 SSTO CONCEPTS 273
8.7.1 THE USE OF AERODYNAMIC LIFT FOR ASCENT 274 APPENDIX 1 ORBITAL
MOTION 277 AL.L RECAPITULATION OF CIRCULAR MOTION 277 A 1.2 GENERAL
(NON-CIRCULAR) MOTION OF A SPACECRAFT IN A GRAVITATIONAL FIELD 278
APPENDIX 2 LAUNCHER SURVEY 283 A2.1 LAUNCH SITE : 283 A2.2 LAUNCHER
CAPABILITY 284 XII CONTENTS A2.3 HEAVY LAUNCHERS 284 A2.4 MEDIUM
LAUNCHERS 285 A2.5 SMALL LAUNCHERS 285 APPENDIX 3 ARIANE 5 299 A3.1 THE
BASIC VEHICLE COMPONENTS 300 A3.2 EVOLVED ARIANE 5 300 APPENDIX 4
GLOSSARY OF SYMBOLS 303 FURTHER READING 307 INDEX 309
|
| any_adam_object | 1 |
| author | Turner, Martin J. L. 1942- |
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| author_facet | Turner, Martin J. L. 1942- |
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| author_sort | Turner, Martin J. L. 1942- |
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| ctrlnum | (OCoLC)249633636 (DE-599)BVBBV023797218 |
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| discipline | Verkehr / Transport |
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| indexdate | 2024-07-09T21:37:01Z |
| institution | BVB |
| isbn | 3540221905 |
| language | English |
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| physical | XXII, 313 S. Ill., graph. Darst. |
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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. L. Turner 2. ed. Berlin [u.a.] Springer 2005 XXII, 313 S. Ill., graph. Darst. txt rdacontent n rdamedia nc rdacarrier Springer Praxis books in astronautical engineering Raketentriebwerk (DE-588)4176905-3 gnd rswk-swf Raketentriebwerk (DE-588)4176905-3 s DE-604 HEBIS Datenaustausch Darmstadt application/pdf http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&local_base=BVB01&doc_number=017439421&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. L. Turner |
| title_fullStr | Rocket and spacecraft propulsion principles, practice and new developments Martin J. L. Turner |
| title_full_unstemmed | Rocket and spacecraft propulsion principles, practice and new developments Martin J. L. 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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