Tactical missile design:
Gespeichert in:
| 1. Verfasser: | |
|---|---|
| Format: | Buch |
| Sprache: | English |
| Veröffentlicht: |
Reston, Va.
American Institute of Aeronautics and Astronautics
2006
|
| Ausgabe: | 2. ed |
| Schriftenreihe: | AIAA education series
|
| Schlagworte: | |
| Online-Zugang: | lizenzfrei Inhaltsverzeichnis |
| Beschreibung: | XIX, 468 S. 1 CD-ROM |
| ISBN: | 1563477823 |
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| 245 | 1 | 0 | |a Tactical missile design |c Eugene L. Fleeman |
| 250 | |a 2. ed | ||
| 264 | 1 | |a Reston, Va. |b American Institute of Aeronautics and Astronautics |c 2006 | |
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Datensatz im Suchindex
| _version_ | 1804143681031110656 |
|---|---|
| adam_text | IMAGE 1
PREFACE
P. XVII
INTRODUCTION/KEY DRIVERS IN THE DESIGN PROCESS
P. 1
INTRODUCTION
P. 1
TACTICAL MISSILE CHARACTERISTICS
P. 1
CONCEPTUAL DESIGN PROCESS
P. 4
EXAMPLES OF STATE-OF-THE-ART MISSILES
P. 7
AERODYNAMIC CONFIGURATION SIZING PARAMETERS
P. 9
EXAMPLE OF ALTERNATIVES IN ESTABLISHING MISSION REQUIREMENTS P. 10
USE OF A BASELINE MISSILE
P. 14
SUMMARY
P. 18
PROBLEMS
P. 18
AERODYNAMIC CONSIDERATIONS IN TACTICAL MISSILE DESIGN
P. 21
INTRODUCTION
P. 21
MISSILE DIAMETER TRADEOFF
P. 21
NOSE FINENESS TRADEOFF
P. 29
BOATTAIL
P. 34
LIFTING BODY VERSUS AXISYMMETRIC BODY
P. 34
STATIC STABILITY
P. 38
BODY AERODYNAMIC CENTER
P. 40
FLARE STABILIZER
P. 41
WINGS VERSUS NO WINGS
P. 43
NORMAL FORCE PREDICTION FOR SURFACES (E.G., WING, TAIL, CANARD) P. 44
AERODYNAMIC CENTER PREDICTION FOR SURFACES (E.G., WING, TAIL, CANARD) P.
47
HINGE MOMENT PREDICTION
P. 48
THIN SURFACE (E.G., WING, TAIL, CANARD) DRAG PREDICTION
P. 49
SURFACE GEOMETRY TRADEOFFS
P. 51
FLIGHT CONTROL ALTERNATIVES
P. 55
MANEUVER ALTERNATIVES
P. 69
ROLL ORIENTATION
P. 72
TRIM
P. 73
TAIL AREA SIZING
P. 74
STABILITY AND CONTROL CONCEPTUAL DESIGN CRITERIA
P. 76
BODY BUILDUP
P. 77
SUMMARY
P. 79
PROBLEMS
P. 79
PROPULSION CONSIDERATIONS IN TACTICAL MISSILE DESIGN
P. 81
INTRODUCTION
P. 81
PROPULSION ALTERNATIVES ASSESSMENT
P. 81
TURBOJET PROPULSION TEMPERATURE TECHNOLOGY LIMIT
P. 86
TURBOJET THRUST PREDICTION
P. 92
TURBOJET SPECIFIC IMPULSE PREDICTION
P. 94
IMAGE 2
RAMJET PROPULSION ALTERNATIVES
P. 95
RAMJET SPECIFIC IMPULSE PREDICTION
P. 97
RAMJET THRUST PREDICTION
P. 98
RAMJET TEMPERATURE TECHNOLOGY LIMIT
P. 100
RAMJET ENGINE/BOOSTER INTEGRATION
P. 105
RAMJET MISSILE DRAG
P. 108
RAMJET INLET OPTIONS
P. 109
SUPERSONIC INLET/AIRFRAME INTEGRATION
P. 112
FUEL ALTERNATIVES
P. 120
DUCTED ROCKET DESIGN CONSIDERATIONS
P. 121
ROCKET MOTOR PERFORMANCE
P. 122
SOLID PROPELLANT GRAIN ALTERNATIVES
P. 128
SOLID ROCKET THRUST MAGNITUDE CONTROL
P. 130
SOLID PROPELLANT ALTERNATIVES
P. 132
MOTOR CASE MATERIAL ALTERNATIVES
P. 134
ROCKET NOZZLE MATERIAL ALTERNATIVES
P. 136
SUMMARY
P. 137
PROBLEMS
P. 137
WEIGHT CONSIDERATIONS IN TACTICAL MISSILE DESIGN
P. 141
INTRODUCTION
P. 141
BENEFITS OF A LIGHTWEIGHT MISSILE
P. 141
SUBSYSTEM WEIGHT SENSITIVITY TO FLIGHT PERFORMANCE
P. 141
MISSILE WEIGHT PREDICTION
P. 143
CENTER-OF-GRAVITY AND MOMENT-OF-INERTIA PREDICTION
P. 146
STRUCTURE FACTOR OF SAFETY
P. 149
AIRFRAME MANUFACTURING PROCESSES
P. 150
AIRFRAME MATERIAL ALTERNATIVES
P. 153
STRUCTURE/INSULATION TRADES
P. 158
HIGH-TEMPERATURE INSULATION MATERIALS
P. 160
AERODYNAMIC HEATING/THERMAL RESPONSE PREDICTION
P. 162
LOCALIZED AERODYNAMIC HEATING AND THERMAL STRESS
P. 172
STRUCTURE DESIGN
P. 175
SEEKER DOME
P. 186
POWER SUPPLY AND ACTUATORS
P. 190
SUMMARY
P. 193
PROBLEMS
P. 194
FLIGHT PERFORMANCE CONSIDERATIONS IN TACTICAL MISSILE DESIGN P. 197
INTRODUCTION
P. 197
FLIGHT PERFORMANCE ENVELOPE
P. 197
EQUATIONS OF MOTION MODELING
P. 199
DRIVING PARAMETERS FOR FLIGHT PERFORMANCE
P. 201
IMAGE 3
CRUISE FLIGHT PERFORMANCE
P. 202
STEADY-STATE FLIGHT
P. 204
FLIGHT TRAJECTORY SHAPING
P. 205
TURN PERFORMANCE
P. 206
COAST FLIGHT PERFORMANCE
P. 210
BALLISTIC FLIGHT PERFORMANCE
P. 212
BOOST FLIGHT PERFORMANCE
P. 214
INTERCEPT LEAD ANGLE AND VELOCITY
P. 215
COMPARISON WITH PERFORMANCE REQUIREMENTS
P. 216
SUMMARY
P. 217
PROBLEMS
P. 217
MEASURES OF MERIT AND LAUNCH PLATFORM INTEGRATION
P. 219
INTRODUCTION
P. 219
ROBUSTNESS
P. 219
WARHEAD LETHALITY
P. 241
MISS DISTANCE
P. 257
CARRIAGE AND LAUNCH OBSERVABLES
P. 274
OTHER SURVIVABILITY CONSIDERATIONS
P. 277
RELIABILITY
P. 281
COST
P. 283
LAUNCH PLATFORM INTEGRATION
P. 295
SUMMARY
P. 309
PROBLEMS
P. 309
SIZING EXAMPLES
P. 313
INTRODUCTION
P. 313
STANDOFF RANGE REQUIREMENT
P. 313
WING SIZING REQUIREMENT
P. 329
MULTI-PARAMETER HARMONIZATION
P. 332
LOFTED RANGE COMPARISON
P. 335
RAMJET MISSILE RANGE ROBUSTNESS
P. 338
RAMJET PROPULSION/FUEL ALTERNATIVES
P. 350
VELOCITY CONTROL
P. 351
EXAMPLES OF COMPUTER-AIDED CONCEPTUAL DESIGN SIZING TOOLS P. 353
SODA STRAW ROCKET DESIGN, BUILD, AND FLY
P. 358
SUMMARY
P. 375
PROBLEMS
P. 376
DEVELOPMENT PROCESS
P. 379
INTRODUCTION
P. 379
TECHNOLOGY ASSESSMENT/ROADMAP
P. 379
PHASES OF DEVELOPMENT/DESIGN MATURITY
P. 380
TACTICAL MISSILE FOLLOW-ON PROGRAMS
P. 383
IMAGE 4
SUBSYSTEM INTEGRATION
P. 384
EXAMPLE OF TECHNOLOGY DEVELOPMENT
P. 390
EXAMPLES OF STATE-OF-THE-ART ADVANCEMENT
P. 393
NEW TECHNOLOGIES FOR TACTICAL MISSILES
P. 395
SUMMARY
P. 397
PROBLEMS
P. 397
SUMMARY AND LESSONS LEARNED
P. 399
INTRODUCTION
P. 399
EVALUATE ALTERNATIVES AND ITERATE THE SYSTEM-OF-SYSTEMS DESIGN P. 399
EXPLOIT DIVERSE SKILLS
P. 399
UTILIZE CREATIVE SKILLS
P. 401
IDENTIFY AND QUANTIFY THE HIGH-PAYOFF MEASURES OF MERIT
P. 401
START WITH A GOOD BASELINE DESIGN
P. 402
CONDUCT BALANCED, UNBIASED TRADEOFFS
P. 403
EVALUATE MANY ALTERNATIVES
P. 404
SEARCH A BROAD DESIGN SOLUTION SPACE (GLOBAL OPTIMIZATION VERSUS LOCAL
OPTIMIZATION) P. 404
EVALUATE AND REFINE AS OFTEN AS POSSIBLE
P. 405
PROVIDE BALANCED EMPHASIS OF ANALYTICAL VERSUS EXPERIMENTAL P. 406
USE A DESIGN, BUILD, AND FLY PROCESS FOR FEEDBACK THAT LEADS TO BROADER
KNOWLEDGE P. 406
EVALUATE TECHNOLOGY RISK
P. 407
MAINTAIN REAL-TIME DOCUMENTATION
P. 408
DEVELOP GOOD DOCUMENTATION
P. 408
UTILIZE GROUP SKILLS
P. 410
BALANCE THE TRADEOFF OF IMPORTANCE VERSUS PRIORITY
P. 411
ITERATE THE CONFIGURATION DESIGN
P. 412
CONFIGURATION SIZING CONCEPTUAL DESIGN GUIDELINES
P. 412
WRAP-UP
P. 415
HOMEWORK PROBLEMS/CLASSROOM EXERCISES
P. 417
EXAMPLE OF REQUEST FOR PROPOSAL
P. 427
NOMENCLATURE
P. 437
ACRONYMS
P. 447
CONVERSION FACTORS
P. 451
EXAMPLE OF A SYLLABUS
P. 453
REFERENCES
P. 455
BIBLIOGRAPHY
P. 457
INDEX
P. 461
SUPPORTING MATERIALS
P. 469
TABLE OF CONTENTS PROVIDED BY BLACKWELL S BOOK SERVICES AND R.R. BOWKER.
USED WITH PERMISSION.
|
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| author | Fleeman, Eugene L. |
| author_facet | Fleeman, Eugene L. |
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| author_sort | Fleeman, Eugene L. |
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| dewey-ones | 623 - Military and nautical engineering |
| dewey-raw | 623.4/519 |
| dewey-search | 623.4/519 |
| dewey-sort | 3623.4 3519 |
| dewey-tens | 620 - Engineering and allied operations |
| discipline | Militärwissenschaft Verkehr / Transport |
| edition | 2. ed |
| format | Book |
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| isbn | 1563477823 |
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| spelling | Fleeman, Eugene L. Verfasser aut Tactical missile design Eugene L. Fleeman 2. ed Reston, Va. American Institute of Aeronautics and Astronautics 2006 XIX, 468 S. 1 CD-ROM txt rdacontent n rdamedia nc rdacarrier AIAA education series Tactical missilesxDesign and construction Lenkflugkörper (DE-588)4035334-5 gnd rswk-swf Lenkflugkörper (DE-588)4035334-5 s DE-604 http://www.loc.gov/catdir/toc/ecip0610/2006009611.html lizenzfrei Inhaltsverzeichnis GBV Datenaustausch application/pdf http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&local_base=BVB01&doc_number=020872330&sequence=000001&line_number=0001&func_code=DB_RECORDS&service_type=MEDIA Inhaltsverzeichnis |
| spellingShingle | Fleeman, Eugene L. Tactical missile design Tactical missilesxDesign and construction Lenkflugkörper (DE-588)4035334-5 gnd |
| subject_GND | (DE-588)4035334-5 |
| title | Tactical missile design |
| title_auth | Tactical missile design |
| title_exact_search | Tactical missile design |
| title_full | Tactical missile design Eugene L. Fleeman |
| title_fullStr | Tactical missile design Eugene L. Fleeman |
| title_full_unstemmed | Tactical missile design Eugene L. Fleeman |
| title_short | Tactical missile design |
| title_sort | tactical missile design |
| topic | Tactical missilesxDesign and construction Lenkflugkörper (DE-588)4035334-5 gnd |
| topic_facet | Tactical missilesxDesign and construction Lenkflugkörper |
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