Reaching high altitudes on Mars with an inflatable hypersonic drag balloon (ballute):
Gespeichert in:
| 1. Verfasser: | |
|---|---|
| Format: | Abschlussarbeit Buch |
| Sprache: | English |
| Veröffentlicht: |
Wiesbaden
Vieweg + Teubner
2011
|
| Ausgabe: | 1. ed. |
| Schriftenreihe: | Vieweg + Teubner research
|
| Schlagworte: | |
| Online-Zugang: | Inhaltsverzeichnis |
| Beschreibung: | XXX, 236 S. zahlr. Ill., graph. Darst. 21 cm |
| ISBN: | 9783834814258 3834814253 |
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Datensatz im Suchindex
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| adam_text | IMAGE 1
TABLE OF CONTENTS
ACKNOWLEDGEMENTS VII
LIST OF FIGURES XIII
LIST OF TABLES XXIII
LIST OF SYMBOLS XXV
LIST OF CONSTANTS XXVII
ACRONYMS AND ABBREVIATIONS XXIX
1 INTRODUCTION 1
1.1 SCIENTIFIC BACKGROUND 1
1.2 ENGINEERING BACKGROUND 2
2 RELATED TECHNOLOGIES AND STATE OF THE ART 3
2.1 ABOUT PLANETARY AEROPLANES AND BALLOONS 3
2.2 ABOUT AUTOMATIC INFLATABLES 4
2.2.1 GAS GENERATOR SYSTEMS 4
2.2.2 COMPRESSED GAS SYSTEMS 5
2.2.3 CRYOGENIC GAS STORAGE SYSTEMS 6
2.2.4 GENERAL MOTORS AIR CUSHION RESTRAINT SYSTEM FROM 1973 TO 1976 6
2.3 ABOUT SPACE INFLATABLES 8
2.4 ABOUT HYPERSONIC INFLATABLE DRAG DEVICES 9
2.4.1 THE GOODYEAR BALLUTE 10
2.4.2 THE GEMINI EJECTION SEAT RECOVERY SYSTEM 11
2.4.3 1RDT 12
2.5 STATE OF THE ART 13
3 BASIC CONSIDERATIONS ON PROBES WITH LOW BALLISTIC COEFFICIENTS 15
3.1 THE SPACECRAFT ELEMENTS 15
3.1.1 THE BALLUTE SPACECRAFT 15
3.1.2 THE SERVICE SPACECRAFT AND MISSION INFRASTRUCTURE 16
3.1.3 BASIC SIMPLIFICATION 16
3.2 BASIC EQUATIONS OF MOTION 17
3.3 ABOUT ATMOSPHERE MODELS AND THEIR SUITABILITY 18
3.4 THE BALLISTIC COEFFICIENT AND ITS IMPACT ON MISSION DESIGN 22
3.5 ENTRY ANGLE AND ENTRY ALTITUDE 26
4 BALLUTE SPACECRAFT CONFIGURATION OPTIONS 33
4.1 GENERAL BALLUTE SHAPES AND ATTACHMENT OPTIONS 33
4.2 FINAL CONFIGURATION 34
4.3 MISSION DESIGN OPTIONS 35
4.3.1 DESCENDING TO A FLOTATION ALTITUDE 36
4.3.2 DESCENDING TO THE SURFACE OF MARS 41
4.3.3 AEROBREAKING BEFORE DESCENDING DEEPER INTO THE ATMOSPHERE 42
BIBLIOGRAFISCHE INFORMATIONEN HTTP://D-NB.INFO/1010163671
DIGITALISIERT DURCH
IMAGE 2
TABLE OF CONTENTS
5 FLIGHT DYNAMICS ANALYSIS 45
5.1 OVERVIEW 45
5.2 MISSION AND SENSITIVITY ANALYSIS WITH THE RADIO SCIENCE SIMULATOR 45
5.2.1 ATMOSPHERIC ENTRY TRAJECTORIES 46
5.2.2 MISSION DESIGN ANALYSIS 48
5.3 AEROTHERMODYNAMICS AND AEROELASTICITY 50
5.3.1 COMPUTATIONAL FLUID DYNAMICS ANALYSIS OF CRITICAL TRAJECTORY
POINTS 50 5.3.2 FEM STRESS AND MODAL ANALYSES 54
5.4 THERMAL ANALYSIS 59
5.4.1 OVERVIEW AND COORDINATE SYSTEM 59
5.4.2 BASIC EQUATIONS 60
5.4.3 RADIATIVE HEAT EXCHANGE 61
5.4.4 EXAMPLE RESULTS 65
6 MATERIAL ANALYSIS 67
6.1 MATERIAL SELECTION 67
6.2 TESTS AND RESULTS 69
6.2.1 UPILEX 69
6.2.2 PBO 73
6.3 CONCLUSION 77
7 BALLUTE 79
7.1 SYSTEM DESIGN 79
7.2 THEORY OF OPERATION (BALLUTE THEORY) 80
7.2.1 AN APPROXIMATE ANALYTICAL METHOD TO DETERMINE THE DESIRED
BALLISTIC COEFFICIENT AND BALLUTE PERFORMANCE 82
7.2.2 DETERMINATION OF THE REQUIRED INFLATION PRESSURE RANGE 96 7.2.3
ACCESSIBLE LANDING TERRAIN, USABLE ALTITUDE RANGE AND USABLE DESCENT
TIME. .101 7.2.4 SIZING THE BALLUTE 116
7.2.5 SIZING THE FITTINGS 124
7.3 DESIGN CONSIDERATIONS 126
7.3.1 GENERAL LAYOUT CONSIDERATIONS 126
7.3.2 ENVELOPE PRODUCTION PATTERNS AND SEGMENTS 127
7.3.3 FITTINGS AND REINFORCEMENTS 135
7.3.4 SEAMS 136
7.3.5 BALLUTE INSTRUMENTATION 147
7.4 MANUFACTURING CONSIDERATIONS 151
7.4.1 ENVELOPE PARTS 151
7.4.2 ENVELOPE ASSEMBLY 153
8 TRANSPORTATION AND DEPLOYMENT SYSTEM 155
8.1 STATEMENT OF PURPOSE 155
8.2 SYSTEM DESIGN 155
8.3 THEORY OF OPERATION 156
8.3.1 GENERAL PRINCIPLE 156
8.3.2 PROTECTIVE ATMOSPHERE 156
8.4 BALLUTE PACKAGING 158
8.4.1 GENERAL PRINCIPLE 158
8.4.2 PACKAGING EFFICIENCY AND TRAPPED GAS 158
8.5 DEPLOYMENT TESTS 164
IMAGE 3
TABLE OF CONTENTS XI
8.5.1 PARABOLIC FLIGHT DEPLOYMENT TEST 164
8.5.2 REGINA IN SPACE DEPLOYMENT TEST 166
9 INFLATION CONTROL AND GAS STORAGE SYSTEM (IGSS) 169
9.1 SYSTEM DESIGN 169
9.2 THEORY OF OPERATION 173
9.2.1 GENERAL OVERVIEW 173
9.2.2 MATHEMATICAL DESCRIPTION AND SIMULATION 174
10 MISSION AND SPACECRAFT DESIGN FOR BALLUTE APPLICATIONS 179
10.1 PRINCIPAL MISSION AND SPACECRAFT DESIGN GUIDE 179
10.2 THE MIRIAM SPACEFLIGHT TEST 181
10.2.1 GENERAL MISSION AND SPACECRAFT OVERVIEW 181
10.2.2 INSTRUMENTATION AND METHODS TO ACHIEVE THE MISSION GOALS 186
10.2.3 INSTRUMENT POD 187
10.2.4 TRAJECTORY AND AEROTHERMODYNAMIC ANALYSIS 189
10.2.5 BALLUTE 191
10.2.6 DEPLOYMENT AND INFLATION SUBSYSTEMS 194
10.2.7 FLIGHT REPORT AND CONCLUSION 204
10.3 THE ARCHIMEDES MARS BALLOON PROBE 208
10.3.1 SCIENTIFIC MISSION AND PAYLOAD INSTRUMENTS 208
10.3.2 MARS MISSION SYSTEM ELEMENTS 209
10.3.3 MISSION DESIGN 214
10.3.4 CONCLUSION 225
10.4 OTHER APPLICATIONS 226
10.4.1 THE ARCHIMDES-V VENUS BALLUTE PROBE 226
10.4.2 SKY RAFT: RECOVERY FROM EARTH ORBIT 226
11 CONCLUSION AND OUTLOOK 229
BIBLIOGRAPHY 231
|
| any_adam_object | 1 |
| author | Griebel, Hannes |
| author_GND | (DE-588)144006170 |
| author_facet | Griebel, Hannes |
| author_role | aut |
| author_sort | Griebel, Hannes |
| author_variant | h g hg |
| building | Verbundindex |
| bvnumber | BV037408475 |
| ctrlnum | (OCoLC)730033769 (DE-599)DNB1010163671 |
| dewey-full | 629.435430284 |
| dewey-hundreds | 600 - Technology (Applied sciences) |
| dewey-ones | 629 - Other branches of engineering |
| dewey-raw | 629.435430284 |
| dewey-search | 629.435430284 |
| dewey-sort | 3629.435430284 |
| dewey-tens | 620 - Engineering and allied operations |
| discipline | Maschinenbau / Maschinenwesen Verkehr / Transport |
| edition | 1. ed. |
| format | Thesis Book |
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| indexdate | 2024-07-09T23:23:41Z |
| institution | BVB |
| isbn | 9783834814258 3834814253 |
| language | English |
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| physical | XXX, 236 S. zahlr. Ill., graph. Darst. 21 cm |
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| spelling | Griebel, Hannes Verfasser (DE-588)144006170 aut Reaching high altitudes on Mars with an inflatable hypersonic drag balloon (ballute) Hannes Griebel 1. ed. Wiesbaden Vieweg + Teubner 2011 XXX, 236 S. zahlr. Ill., graph. Darst. 21 cm txt rdacontent n rdamedia nc rdacarrier Vieweg + Teubner research Zugl.: München, Univ. der Bundeswehr, Diss., 2010 Ballonsonde (DE-588)4125991-9 gnd rswk-swf Marsflug (DE-588)4476597-6 gnd rswk-swf (DE-588)4113937-9 Hochschulschrift gnd-content Marsflug (DE-588)4476597-6 s Ballonsonde (DE-588)4125991-9 s DE-604 DNB Datenaustausch application/pdf http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&local_base=BVB01&doc_number=022560993&sequence=000001&line_number=0001&func_code=DB_RECORDS&service_type=MEDIA Inhaltsverzeichnis |
| spellingShingle | Griebel, Hannes Reaching high altitudes on Mars with an inflatable hypersonic drag balloon (ballute) Ballonsonde (DE-588)4125991-9 gnd Marsflug (DE-588)4476597-6 gnd |
| subject_GND | (DE-588)4125991-9 (DE-588)4476597-6 (DE-588)4113937-9 |
| title | Reaching high altitudes on Mars with an inflatable hypersonic drag balloon (ballute) |
| title_auth | Reaching high altitudes on Mars with an inflatable hypersonic drag balloon (ballute) |
| title_exact_search | Reaching high altitudes on Mars with an inflatable hypersonic drag balloon (ballute) |
| title_full | Reaching high altitudes on Mars with an inflatable hypersonic drag balloon (ballute) Hannes Griebel |
| title_fullStr | Reaching high altitudes on Mars with an inflatable hypersonic drag balloon (ballute) Hannes Griebel |
| title_full_unstemmed | Reaching high altitudes on Mars with an inflatable hypersonic drag balloon (ballute) Hannes Griebel |
| title_short | Reaching high altitudes on Mars with an inflatable hypersonic drag balloon (ballute) |
| title_sort | reaching high altitudes on mars with an inflatable hypersonic drag balloon ballute |
| topic | Ballonsonde (DE-588)4125991-9 gnd Marsflug (DE-588)4476597-6 gnd |
| topic_facet | Ballonsonde Marsflug Hochschulschrift |
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