Future spacecraft propulsion systems and integration: enabling technologies for space exploration
Gespeichert in:
| Hauptverfasser: | , , |
|---|---|
| Format: | Buch |
| Sprache: | English |
| Veröffentlicht: |
Berlin
Springer
[2018]
|
| Ausgabe: | Third edition |
| Schriftenreihe: | Astronautical engineering
Springer Praxis books |
| Schlagworte: | |
| Online-Zugang: | Inhaltstext Inhaltsverzeichnis |
| Beschreibung: | lxi, 463 Seiten Illustrationen, Diagramme 24 cm x 16.8 cm |
| ISBN: | 9783662547427 3662547422 |
Internformat
MARC
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| 028 | 5 | 2 | |a Bestellnummer: 978-3-662-54742-7 |
| 028 | 5 | 2 | |a Bestellnummer: 86398943 |
| 035 | |a (OCoLC)979562999 | ||
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| 100 | 1 | |a Czysz, Paul A. |e Verfasser |4 aut | |
| 240 | 1 | 0 | |a Future spacecraft propulsion systems |
| 245 | 1 | 0 | |a Future spacecraft propulsion systems and integration |b enabling technologies for space exploration |c Paul A. Czysz, Claudio Bruno, Bernd Chudoba |
| 250 | |a Third edition | ||
| 264 | 1 | |a Berlin |b Springer |c [2018] | |
| 264 | 4 | |c © 2018 | |
| 300 | |a lxi, 463 Seiten |b Illustrationen, Diagramme |c 24 cm x 16.8 cm | ||
| 336 | |b txt |2 rdacontent | ||
| 337 | |b n |2 rdamedia | ||
| 338 | |b nc |2 rdacarrier | ||
| 490 | 0 | |a Astronautical engineering | |
| 490 | 0 | |a Springer Praxis books | |
| 650 | 0 | 7 | |a Raketentriebwerk |0 (DE-588)4176905-3 |2 gnd |9 rswk-swf |
| 653 | |a Electric Rockets | ||
| 653 | |a IAC | ||
| 653 | |a Launch Vehicle Design | ||
| 653 | |a Point-to-Point Hypersonic Transportation | ||
| 653 | |a Propulsion Concepts | ||
| 653 | |a Propulsion Space | ||
| 653 | |a Reusable Space Access | ||
| 653 | |a Space Tourism | ||
| 653 | |a Technology Forecasting | ||
| 689 | 0 | 0 | |a Raketentriebwerk |0 (DE-588)4176905-3 |D s |
| 689 | 0 | |5 DE-604 | |
| 700 | 1 | |a Bruno, Claudio |e Verfasser |4 aut | |
| 700 | 1 | |a Chudoba, Bernd |e Verfasser |4 aut | |
| 776 | 0 | 8 | |i Erscheint auch als |n Online-Ausgabe |z 978-3-662-54744-1 |
| 780 | 0 | 0 | |i Vorangegangen ist |z 978-3-540-88813-0 |
| 856 | 4 | 2 | |m X:MVB |q text/html |u http://deposit.dnb.de/cgi-bin/dokserv?id=b9129e9c66834d3e99c7fec6019e742d&prov=M&dok_var=1&dok_ext=htm |3 Inhaltstext |
| 856 | 4 | 2 | |m DNB Datenaustausch |q application/pdf |u http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&local_base=BVB01&doc_number=029954363&sequence=000001&line_number=0001&func_code=DB_RECORDS&service_type=MEDIA |3 Inhaltsverzeichnis |
| 943 | 1 | |a oai:aleph.bib-bvb.de:BVB01-029954363 | |
Datensatz im Suchindex
| _version_ | 1809773746969378816 |
|---|---|
| adam_text |
CONTENTS
1
OVERVIEW.
1
1.1 THE
CHALLENGE.
1
1.2 HISTORICAL
DEVELOPMENTS.
1
1.3 CHALLENGE OF FLYING TO
SPACE.
2
1.3.1 VEHICLE-INTEGRATED ROCKET
PROPULSION. 3
1.3.2 VEHICLE-INTEGRATED AIRBREATHING PROPULSION
.
3
1.3.3 CHOICE OF PROPULSION SYSTEM: A MULTI-DISCIPLINARY CHALLENGE . . .
3
1.4 OPERATIONAL
REQUIREMENTS.
4
1.5 OPERATIONAL SPACE DISTANCES, SPEED, AND TIM
ES. 6
1.6 IMPLIED PROPULSION
PERFORMANCE.
9
1.7 PROPULSION CONCEPTS AVAILABLE FOR SOLAR SYSTEM EXPLORATION
.
13
BIBLIOGRAPHY.
17
2 OUR PROGRESS APPEARS TO BE
IMPEDED.
19
2.1 MEETING THE C
HALLENGE.
19
2.2 EARLY PROGRESS IN
SPACE.
19
2.3 HISTORICAL
ANALOG.
22
2.4 EVOLUTION OF SPACE LAUNCHERS FROM BALLISTIC M
ISSILES. 24
2.5 CONFLICTS BETWEEN EXPENDABLE ROCKETS AND REUSABLE AIRBREATHERS
.
29
2.6 COMMERCIALIZATION AND EXPLORATION ROAD M AP
.
34
2.6.1 COMMERCIAL NEAR-EARTH LAUNCHERS ENABLE THE FIRST STEP
.
34
2.6.2 ON-ORBIT OPERATIONS IN NEAR-EARTH ORBIT ENABLE THE SECOND
S
TEP.
38
2.6.3 EARTH-MOON SYSTEM ENABLES THE THIRD STEP
.
38
2.6.4 NUCLEAR OR HIGH-ENERGY SPACE PROPULSION ENABLES THE FOURTH
S
TEP.
39
2.6.5 VERY HIGH-ENERGY SPACE PROPULSION ENABLES THE FIFTH STEP . 39
2.6.6 LIGHT SPEED-PLUS PROPULSION ENABLES THE SIXTH STEP
.
39
BIBLIOGRAPHY.
40
3 COMMERCIAL NEAR-EARTH SPACE LAUNCHER: UNDERSTANDING SYSTEM
INTEGRATION.
43
3.1 MISSIONS AND GEOGRAPHICAL C
ONSIDERATIONS. 45
3.2 ENERGY, PROPELLANTS, AND PROPULSION
REQUIREMENTS. 46
3.3 ENERGY REQUIREMENTS TO CHANGE ORBITAL A LTITUDE
.
48
3.4 OPERATIONAL CONCEPTS ANTICIPATED FOR FUTURE M ISSIO N S
.
50
3.5 CONFIGURATION
CONCEPTS.
51
3.6 TAKEOFF AND LANDING M
ODE.
60
3.7 TRANSATMOSPHERIC LAUNCHER S
IZING.
62
3.7.1 VEHICLE DESIGN R
ATIONALE. 62
3.7.2 VEHICLE SIZING A P
PROACH. 63
3.7.3 PROPULSION S YSTEM
S. 72
3.7.4 SIZING METHODOLOGY AND SOFTWARE
IMPLEMENTATION. 81
3.8 AVAILABLE SOLUTION SPACES: EXAM PLES
.
105
3.8.1 SINGLE-STAGE-TO-ORBIT (SSTO) SOLUTION S P A C E
.
105
3.8.2 TRANSATMOSPHERIC SPACE LAUNCHER: LESSONS LEARNED
.
109
3.9 HYPERSONIC CONFIGURATIONS: GEOMETRIC
CHARACTERISTICS. 110
3.9.1 CONFIGURATION C ONTINUUM
.
110
3.9.2 CONFIGURATION GEOMETRY PROPERTIES
.
114
BIBLIOGRAPHY.
118
4 COMMERCIAL N EAR-EARTH LAUNCHER: PROPULSION C HOICES
.
123
4.1 PROPULSION SYSTEM A
LTERNATIVES.
124
4.2 PROPULSION SYSTEM
CHARACTERISTICS.
125
4.3 AIRFLOW ENERGY ENTERING THE
ENGINE.
125
4.4 INTERNAL FLOW ENERGY L O
SSES.
128
4.5 SPECTRUM OF AIRBREATHING
OPERATION.
132
4.6 DESIGN SPACE AVAILABLE*INTERACTION OF PROPULSION AND
M
ATERIALS/STRUCTURES.
134
4.7 MAJOR SEQUENCE OF PROPULSION CYCLES
.
137
4.8 ROCKET-DERIVED P
ROPULSION.
141
4.9 AIRBREATHING ROCKET
PROPULSION.
143
4.10 THERMALLY INTEGRATED COMBINED-CYCLE P
ROPULSION. 145
4.11 ENGINE THERMAL
INTEGRATION.
147
4.12 TOTAL SYSTEM THERMAL
INTEGRATION.
148
4.13 THERMALLY INTEGRATED ENRICHED AIR COMBINED-CYCLE PROPULSION
.
152
4.14 COMPARISON OF CONTINUOUS OPERATION
CYCLES. 153
4.15 CONCLUSIONS WITH RESPECT TO CONTINOUS OPERATION C YCLES
.
158
4.16 PULSE DETONATION E N G IN
ES.
159
4.16.1 ENGINE
DESCRIPTION.
159
4.16.2 ENGINE
PERFORMANCE.
160
4.17 CONCLUSIONS WITH RESPECT TO PULSE DETONATION CYCLES
.
162
4.18 COMPARISON OF CONTINUOUS OPERATION AND PULSED CYCLES
.
163
4.19 INTEGRATED LAUNCHER SIZING WITH DIFFERENT PROPULSION SYSTEMS
.
166
4.20 STRUCTURAL CONCEPT AND STRUCTURAL I N D E X
.
168
4.21 SIZING RESULTS FOR CONTINUOUS AND PULSE DETONATION ENGINES
.
169
4.22 OPERATIONAL CONFIGURATION CONCEPTS: SSTO AND T S T O
.
172
4.23 EMERGING PROPULSION SYSTEM CONCEPTS IN D EVELOPM ENT
.
176
4.23.1 MAGNETOHYDRODYNAMIC (MHD) ENERGY BYPASS SYSTEM
.
177
4.23.2 ELECTROMAGNETIC RADIATION PROPULSION
.
181
4.23.3 VARIABLE CYCLE
TURBORAMJET.
182
4.23.4 AERO-SPIKE
NOZZLE.
183
4.23.5 ORBITEC VORTEX ROCKET
ENGINE. 183
BIBLIOGRAPHY.
186
5 E ARTH O RBIT ON-O RBIT OPERATIONS IN N E A R-E A RTH
. 193
5.1 ENERGY REQUIREM
ENTS.
195
5.1.1 GETTING TO LOW EARTH ORBIT: ENERGY AND PROPELLANT
REQUIREMENTS.
195
5.2 LAUNCHER PROPULSION SYSTEM CHARACTERISTICS
.
197
5.2.1 PROPELLANT RATIO TO DELIVER PROPELLANT TO L E O
.
198
5.2.2 GEOSTATIONARY ORBIT SATELLITE SIZE AND M A S S
.
201
5.3 MANEUVER BETWEEN LEO AND GEO, CHANGE IN ALTITUDE AT SAME
ORBITAL
INCLINATION.
201
5.3.1 ENERGY REQUIREMENTS FOR ALTITUDE
CHANGE. 203
5.3.2 MASS RATIO REQUIRED FOR ALTITUDE
CHANGE. 203
5.3.3 PROPELLANT DELIVERY RATIO FOR ALTITUDE CHANGE
.
206
5.4 CHANGES IN ORBITAL INCLINATION
.
207
5.4.1 ENERGY REQUIREMENTS FOR ORBITAL INCLINATION C H A N G E
.
208
5.4.2 MASS RATIO REQUIRED FOR ORBITAL INCLINATION CHANGE
.
210
5.4.3 PROPELLANT DELIVERY RATIO FOR ORBITAL INCLINATION CHANGE
.
212
5.5 REPRESENTATIVE SPACE TRANSFER VEHICLES
.
214
5.6 OPERATIONAL
CONSIDERATIONS.
215
5.6.1 MISSIONS PER PROPELLANT DELIVERY
.
216
5.6.2 ORBITAL
STRUCTURES.
216
5.6.3 ORBITAL
CONSTELLATIONS.
217
5.6.4 DOCKING WITH SPACE FACILITIES AND THE I S S
.
219
5.6.5 EMERGENCY RESCUE VEHICLE
.
221
5.7 OBSERVATIONS AND RECOMMENDATIONS
.
222
BIBLIOGRAPHY.
222
6 E ARTH-M OON SYSTEM: ESTABLISHING A SOLAR SYSTEM P RESENCE
.
225
6.1 EARTH-MOON
CHARACTERISTICS.
225
6.2 REQUIREMENTS TO TRAVEL TO THE MOON
.
228
6.2.1 SUSTAINED OPERATION LUNAR
TRAJECTORIES. 230
6.2.2 LAUNCHING FROM THE MOON
SURFACE. 230
6.3 H
ISTORY.
233
6.3.1 USSR EXPLORATION H ISTO RY
.
234
6.3.2 USA EXPLORATION H ISTO RY
. 234
6.3.3 INDIA EXPLORATION H
ISTORY.
234
6.3.4 JAPAN EXPLORATION
HISTORY.
234
6.3.5 CHINA EXPLORATION
HISTORY.
235
6.4 NATURAL VERSUS ARTIFICIAL ORBITAL STATION ENVIRONMENTS
.
235
6.4.1 PRIOR ORBITAL S TATIONS
.
235
6.4.2 ARTIFICIAL ORBITAL S TATIO N
S. 236
6.4.3 NATURAL ORBITAL S TA TIO N S
.
237
6.5 MOON BASE
FUNCTIONS.
238
6.5.1 MARTIAN A
NALOG.
239
6.5.2 LUNAR
EXPLORATION.
239
6.5.3 MANUFACTURING AND PRODUCTION
SITE. 241
BIBLIOGRAPHY.
242
7 EXPLORATION OF O UR SOLAR SY S TE M
.
243
7.1 REVIEW OF OUR SOLAR SYSTEM DISTANCES, SPEEDS, AND PROPULSION
REQUIREMENTS.
243
7.2 ALTERNATIVE ENERGY SOURCES: NUCLEAR E N ERG Y
. 246
7.3 LIMITS OF CHEMICAL PROPULSION AND
ALTERNATIVES. 249
7.3.1 ENERGY SOURCES AND SPECIFIC IM PULSE
.
250
7.3.2 THE NEED FOR NUCLEAR SPACE PROPULSION
.
252
7.4 NUCLEAR PROPULSION
STRATEGIES.
253
7.5 NUCLEAR PROPULSION: A HISTORICAL
PERSPECTIVE. 256
7.6 NUCLEAR PROPULSION: CURRENT S CENARIOS
.
261
7.7 FUNDAMENTALS OF NUCLEAR F ISSIO N
.
268
7.8 SOLID-CORE N
TR.
269
7.9 PARTICLE BED REACTOR
TECHNOLOGY.
272
7.10 CERMET T
ECHNOLOGY.
274
7.11 M IT E E N T R
.
274
7.12 GAS-CORE
NTR.
276
7.13 RUBBIA*S
ENGINE.
277
7.14 CONSIDERATIONS ABOUT NTR
PROPULSION.
280
7.15 HYBRID NUCLEAR R O CK
ETS.
280
7.16 NUCLEAR-ELECTRIC PROPULSION (N E P )
.
282
7.17 NUCLEAR ARCJET R
OCKETS.
283
7.18 NUCLEAR-ELECTRIC
ROCKETS.
284
7.19 ELECTROSTATIC ION
THRUSTERS.
285
7.20 MPD/MHD
THRUSTERS.
287
7.21 HYBRID NTR/NER E N G IN E
S.
291
7.22 INDUCTIVELY HEATED N T R
.
292
7.22.1 NUCLEAR-THERMAL-ELECTRIC ROCKET (N
TER). 293
7.23 VASIMR (VARIABLE SPECIFIC IMPULSE MAGNETO-PLASMA-DYNAMIC ROCKET). .
. 294
7.24 PROPULSION STRATEGIES
COMPARED.
298
7.25
CONCLUSIONS.
299
BIBLIOGRAPHY.
302
8 STELLAR AND INTERSTELLAR P RECURSOR M ISSIO N
S. 311
8.1
INTRODUCTION.
311
8.1.1 QUASI-INTERSTELLAR
DESTINATIONS.
313
8.1.2 TIME AND
DISTANCE.
316
8.2 PROPULSION FOR QUASI-INTERSTELLAR AND STELLAR M
ISSIONS. 317
8.2.1 FUSION REQUIREMENTS AND IMPACT ON PROPULSION
.
320
8.3 TRAVELING AT RELATIVISTIC S
PEEDS.
322
8.4 POWER FOR QUASI-INTERSTELLAR AND STELLAR
PROPULSION. 325
8.5 FUSION
PROPULSION.
326
8.5.1 MISSION LENGTH ENABLED BY FUSION AND ANNIHILATION
PROPULSION.
327
8.6 FUSION FUELS AND THEIR
KINETICS.
328
8.7 FUSION PROPULSION S
TRATEGIES.
330
8.7.1 THERMAL VERSUS ELECTRIC FUSION PROPULSION
.
331
8.8 FUSION PROPULSION REACTOR
CONCEPTS.
332
8.8.1 CONFINEMENT
STRATEGIES.
332
8.9 MAGNETIC CONFINEMENT REACTORS (M C R )
.
333
8.10 MIRROR MAGNETIC CONFINEMENT ROCKETS (MIRROR MCR)
.
335
8.10.1 TOKAMAK MCE R O CK
ETS.
336
8.10.2 COMPARING THERMAL AND ELECTRIC MCE ROCKETS
.
339
8.11 INERTIAL CONFINEMENT
FUSION.
340
8.11.1 FUSION IG N ITIO N
.
344
8.12 INERTIAL ELECTROSTATIC CONFINEMENT (IEC) F U SIO N
. 344
8.13 MCE AND ICE FUSION: A COMPARISON
.
345
8.14 MAGNETIC-INERTIAL CONFINEMENT (MIC)
FUSION. 350
8.15 FUSION PROPULSION S UM M
ARY.
352
8.16 ANTIMATTER
PROPULSION.
353
8.17 IMPULSIVE P
ROPULSION.
354
8.18 PHOTONIC
PROPULSION.
355
8.19 CONCLUSIONS: CAN WE REACH THE
STARS?. 356
BIBLIOGRAPHY.
357
9 VIEW TO THE FUTURE AND EXPLORATION OF OUR G ALAXY
.
363
9.1
INTRODUCTION.
363
9.2 ISSUES IN DEVELOPING NEAR- AND FAR-GALACTIC SPACE EXPLORATION
.
364
9.3 BLACK HOLES AND GALACTIC T RA V E L
.
369
9.4 BREAKTHROUGH PHYSICS AND
PROPULSION.
372
9.5 SUPERLUMINAL SPEED: IS IT REQUIRED?
.
374
9.6
CONCLUSIONS.
377
BIBLIOGRAPHY.
377
APPENDIX A: RADIATION*RISKS, DOSE ASSESSMENT, AND SHIELDING
.
381
APPENDIX B: ASSESSMENT OF OPEN MAGNETIC FUSION FOR SPACE PROPULSION
.
403
AUTHOR I N D E X
.
437
SUBJECT I N D E X
.
451 |
| any_adam_object | 1 |
| author | Czysz, Paul A. Bruno, Claudio Chudoba, Bernd |
| author_facet | Czysz, Paul A. Bruno, Claudio Chudoba, Bernd |
| author_role | aut aut aut |
| author_sort | Czysz, Paul A. |
| author_variant | p a c pa pac c b cb b c bc |
| building | Verbundindex |
| bvnumber | BV044555623 |
| ctrlnum | (OCoLC)979562999 (DE-599)DNB1127877569 |
| dewey-full | 620 |
| dewey-hundreds | 600 - Technology (Applied sciences) |
| dewey-ones | 620 - Engineering and allied operations |
| dewey-raw | 620 |
| dewey-search | 620 |
| dewey-sort | 3620 |
| dewey-tens | 620 - Engineering and allied operations |
| discipline | Maschinenbau / Maschinenwesen |
| edition | Third edition |
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| id | DE-604.BV044555623 |
| illustrated | Illustrated |
| indexdate | 2024-09-10T02:19:00Z |
| institution | BVB |
| isbn | 9783662547427 3662547422 |
| language | English |
| oai_aleph_id | oai:aleph.bib-bvb.de:BVB01-029954363 |
| oclc_num | 979562999 |
| open_access_boolean | |
| owner | DE-83 |
| owner_facet | DE-83 |
| physical | lxi, 463 Seiten Illustrationen, Diagramme 24 cm x 16.8 cm |
| publishDate | 2018 |
| publishDateSearch | 2018 |
| publishDateSort | 2018 |
| publisher | Springer |
| record_format | marc |
| series2 | Astronautical engineering Springer Praxis books |
| spelling | Czysz, Paul A. Verfasser aut Future spacecraft propulsion systems Future spacecraft propulsion systems and integration enabling technologies for space exploration Paul A. Czysz, Claudio Bruno, Bernd Chudoba Third edition Berlin Springer [2018] © 2018 lxi, 463 Seiten Illustrationen, Diagramme 24 cm x 16.8 cm txt rdacontent n rdamedia nc rdacarrier Astronautical engineering Springer Praxis books Raketentriebwerk (DE-588)4176905-3 gnd rswk-swf Electric Rockets IAC Launch Vehicle Design Point-to-Point Hypersonic Transportation Propulsion Concepts Propulsion Space Reusable Space Access Space Tourism Technology Forecasting Raketentriebwerk (DE-588)4176905-3 s DE-604 Bruno, Claudio Verfasser aut Chudoba, Bernd Verfasser aut Erscheint auch als Online-Ausgabe 978-3-662-54744-1 Vorangegangen ist 978-3-540-88813-0 X:MVB text/html http://deposit.dnb.de/cgi-bin/dokserv?id=b9129e9c66834d3e99c7fec6019e742d&prov=M&dok_var=1&dok_ext=htm Inhaltstext DNB Datenaustausch application/pdf http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&local_base=BVB01&doc_number=029954363&sequence=000001&line_number=0001&func_code=DB_RECORDS&service_type=MEDIA Inhaltsverzeichnis |
| spellingShingle | Czysz, Paul A. Bruno, Claudio Chudoba, Bernd Future spacecraft propulsion systems and integration enabling technologies for space exploration Raketentriebwerk (DE-588)4176905-3 gnd |
| subject_GND | (DE-588)4176905-3 |
| title | Future spacecraft propulsion systems and integration enabling technologies for space exploration |
| title_alt | Future spacecraft propulsion systems |
| title_auth | Future spacecraft propulsion systems and integration enabling technologies for space exploration |
| title_exact_search | Future spacecraft propulsion systems and integration enabling technologies for space exploration |
| title_full | Future spacecraft propulsion systems and integration enabling technologies for space exploration Paul A. Czysz, Claudio Bruno, Bernd Chudoba |
| title_fullStr | Future spacecraft propulsion systems and integration enabling technologies for space exploration Paul A. Czysz, Claudio Bruno, Bernd Chudoba |
| title_full_unstemmed | Future spacecraft propulsion systems and integration enabling technologies for space exploration Paul A. Czysz, Claudio Bruno, Bernd Chudoba |
| title_short | Future spacecraft propulsion systems and integration |
| title_sort | future spacecraft propulsion systems and integration enabling technologies for space exploration |
| title_sub | enabling technologies for space exploration |
| topic | Raketentriebwerk (DE-588)4176905-3 gnd |
| topic_facet | Raketentriebwerk |
| url | http://deposit.dnb.de/cgi-bin/dokserv?id=b9129e9c66834d3e99c7fec6019e742d&prov=M&dok_var=1&dok_ext=htm http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&local_base=BVB01&doc_number=029954363&sequence=000001&line_number=0001&func_code=DB_RECORDS&service_type=MEDIA |
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