X-15: the NASA mission reports ; incorporating files from the USAF
Gespeichert in:
| Weitere Verfasser: | |
|---|---|
| Format: | Buch |
| Sprache: | English |
| Veröffentlicht: |
Burlington
Apogee Books
2000
|
| Online-Zugang: | Inhaltsverzeichnis |
| Beschreibung: | 408 S. Ill., graph. Darst. 1 CD-ROM (12 cm) |
| Format: | Systemvoraussetzungen: Minimum requirements: Pentium 90. - 4x CDROM drive. - Windows 95. - Recommended: Web Browser & Internet access |
| ISBN: | 1896522653 |
Internformat
MARC
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| 245 | 1 | 0 | |a X-15 |b the NASA mission reports ; incorporating files from the USAF |c comp. from the archives & ed. by Robert Godwin |
| 264 | 1 | |a Burlington |b Apogee Books |c 2000 | |
| 300 | |a 408 S. |b Ill., graph. Darst. |e 1 CD-ROM (12 cm) | ||
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| 338 | |b nc |2 rdacarrier | ||
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| 700 | 1 | |a Godwin, Robert |4 edt | |
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| 999 | |a oai:aleph.bib-bvb.de:BVB01-018474813 | ||
Datensatz im Suchindex
| _version_ | 1804140495949004800 |
|---|---|
| adam_text | 30 X-15 THE NASA MISSION REPORTS INCORPORATING FILES FROM THE USAF
COMPILED FROM THE ARCHIVES & EDITED BY ROBERT GODWIN SUB GOTTINGEN 216
510 139 NACH DEN BESTIMMUNGEN DES URHEBERRECHTS DART DAS. AUF
BEILIEGENDFEN DISKETTEN/CD-ROMS GESPEICHERTE COMPUTERPROGRAMM NICHT AUF
EINEN ANDEREN DATEN- TRAGER IIBERTRAGON UND INSBESONDERE N I C H T ZU
GEWERBLICHEN ZWECKEN GENUTZT WARDEN. DIE BIBLIOTHEK UBERNIMMT K E I N E
GARANTIE FUR DIE VIRENFREIHEIT DES DATENTRAGERS. X-L 5 THE NFLSR MISSION
REPORTS 1 CONTENTS INTRODUCTION FLIGHT SUMMARY RESS RELEASE SCIENCE
APPLICATIONS BIOGRAPHIES SCOTT CROSSFIELD JOSEPH WALKER ROBERT WHITE
FORREST PETERSEN JOHN MCKAY ROBERT RUSHWORTH NEIL ARMSTRONG JOE ENGLE
MILTON THOMPSON WILLIAM KNIGHT WILLIAM DANA MICHAEL ADAMS DEVELOPMENT OF
THE X-L 5 RESEARCH AIRCRAFT CHRONOLOGY FOREWORD 1 GENESIS II DESIGN
DETAILS IIITHEMOCKUP IV ENGINE EVOLUTION V AUXILIARY POWER UNIT VI
PRESSURIZATION AND ESCAPE VII FLIGHT DATA. SYSTEM VIII MATTERS OF
GENERAL CONCERN GLOSSARY OF ABBREVIATIONS BI-ANNUAL REPORTS TO CONGRESS
1ST BIANNUAL REPORT 2ND BIANNUAL REPORT 3RD BIANNUAL REPORT 4TH BIANNUAL
REPORT 5TH BIANNUAL REPORT 6TH BIANNUAL REPORT 7TH BIANNUAL REPORT 8TH
BIANNUAL REPORT 9TH BIANNUAL REPORT 10TH BIANNUAL REPORT 11 TH BIANNUAL
REPORT 12TH BIANNUAL REPORT 13TH BIANNUAL REPORT 14TH BIANNUAL REPORT 1
STH BIANNUAL REPORT 16TH BIANNUAL REPORT 17TH BIANNUAL REPORT 18TH
BIANNUAL REPORT 19TH BIANNUAL REPORT 20TH BIANNUAL REPORT NORTH AMERICAN
PROPOSAL INTRODUCTION DESIGN CONSIDERATIONS GENERAL ARRANGEMENT WEIGHT
SUMMARY RESEARCH SUITABILITY THERMAL PROBLEMS THERMAL SUITABILITY...WING
THERMAL SUITABILITY...FUSELAGE THERMAL SUITABILITY...CABIN AND EQUIPMENT
BAY THERMAL SUITABILITY ... REMOTE EQUIPMENT & ROUTING AIRFRAME SERVICE
SYSTEMS...CABIN AND EQUIPMENT CONDITIONING AIRFRAME SERVICE
SYSTEMS...AUXILIARY POWER UNITS AIRFRAME SERVICE SYSTEMS...ELECTRICAL
AIRFRAME SERVICE SYSTEMS.-.SPACE CONTROLS POWER PLANT...ROCKET
INSTALLATION POWER PLANT..PROPELLANT SYSTEM ALIGHTING GEAR
INSTRUMENTATION PROGRAM SCHEDULE NORTH AMERICAN WIND TUNNELS DESIGN
MISSIONS PERFORMANCE CAPABILITY RECOVERY CAPABILITY GLIDING CAPABILITY
ROUTINE MAINTENANCE GROUND HANDLING PRE-FLIGHT PARENT INSTALLATION
CAPTIVE FLIGHT LAUNCH EMERGENCY PROCEDURES FLIGHT 6 II II 14 16 17 17 18
19 20 21 22 22 24 24 25 1954-1959 28 30 31 42 59 61 76 77 84 87 97 98 99
100 100 102 104 106 106 106 107 107 108 108 109 110 NO III III 112 113
116 116 117 118 118 119 120 120 121 121 122 123 123 124 124 125 125 126
127 127 128 129 129 130 130 131 131 132 132 133 133 134 LANDING POST
FLIGHT DESIGN BRIEF ...TWO PLACE VERSION GENERAL ARRANGEMENT...TWO PLACE
VERSION DESIGN MISSION...TWO PLACE VERSION SUPPORTING DATA LIST 134 135
135 136 136 137 SYSTEM DEVELOPMENT PLAN X-L5 RESEARCH AIRCRAFT A.
INTRODUCTION B. SYSTEM DEVELOPMENT PLAN DD FORM 613 C. GENERAL DESIGN
SPECIFICATION D. SUB SYSTEM DESCRIPTION E. PROPULSION SUB-SYSTEM INTERIM
FLIGHT MANUAL SECTION 1 DESCRIPTION AIRPLANE ENGINE (XLR99) PROPELLANT
SUPPLY SYSTEM (XLR99) ENGINE AND PROPELLANT CONTROL HELIUM SYSTEM
(XLR99) PROPELLANT PRESSURIZATION HELIUM SYSTEM (XLR99) ENGINES (XLRII)
PROPELLANT SUPPLY SYSTEM (XLRI1) ENGINE AND PROPELLANT CONTROL NITROGEN
SYSTEM (XLRI 1) PROPELLANT PRESSURIZATION HELIUM SYSTEM (XLRI 1)
AUXILIARY POWER UNITS ELECTRICAL POWER SUPPLY SYSTEMS HYDRAULIC POWER
SUPPLY SYSTEMS FLIGHT CONTROL SYSTEMS WING FLAP SYSTEM SPEED BRAKE
SYSTEM LAUNCH SYSTEM LANDING GEAR SYSTEM INSTRUMENTS CONVENTIONAL FLIGHT
REFERENCE SYSTEM INERTIA! ALL-ATTITUDE FLIGHT DATA SYSTEM
(GYRO-STABILIZED PLATFORM) INSTRUMENTATION SYSTEM INDICATOR, CAUTION,
AND WARNING LIGHT SYSTEM CANOPY EJECTION SEAT AUXILIARY EQUIPMENT
SECTION 2 NORMAL PROCEDURES PREPARATION FOR FLIGHT PREFLIGHT CHECK
CAPTIVE TAXI AND FLIGHT PRELAUNCH LAUNCH FLIGHT CHARACTERISTICS ENGINE
OPERATION ENGINE BURNOUT SHUTDOWN PROCEDURE ABORTED LAUNCH DESCENT
BEFORE LANDING LANDING AFTER LANDING BEFORE LEAVING AIRPLANE CONDENSED
CHECK LIST SECTION 3 EMERGENCY PROCEDURES ENGINE FAILURE CAPTIVE
OPERATION EMERGENCIES EMERGENCY LAUNCH MAXIMUM GLIDE FORCED LANDING »
FIRE OR EXPLOSION EJECTION EMERGENCY ENTRANCE FUEL SYSTEM FAILURE
TURBOPUMP FAILURE DURING FLIGHT PROPELLANT JETTISONING APU SYSTEM
FAILURE ELECTRICAL POWER SUPPLY SYSTEM FAILURE HYDRAULIC SYSTEM FAILURE
FLIGHT CONTROL HYDRAULIC SYSTEM FAILURE BALLISTIC CONTROL SYSTEM FAILURE
CONDENSED CHECK LIST SECTION 4 AUXILIARY EQUIPMENT AIR CONDITIONING AND
PRESSURIZATION SYSTEM COMMUNICATION AND ASSOCIATED ELECTRONIC EQUIPMENT
LIGHTING EQUIPMENT PILOT S OXYGEN SYSTEM MISCELLANEOUS EQUIPMENT SECTION
5 OPERATING LIMITATIONS INSTRUMENT MARKINGS. ENGINE LIMITATIONS LAUNCH
LIMITATIONS AIRSPEED LIMITATIONS ACCELERATION LIMITATIONS 138 139 141
143 152 156 156 157 167 167 168 168 175 176 176 177 180 183 184 189 189
189 189 190 190 192 194 195 195 196 198 199 199 200 203 204 207 208 208
208 208 209 209 209 209 209 209 210 216 216 216 217 217 217 217 218 218
218 219 219 219 221 223 224 225 225 226 226 229 231 231 232 233 233 233
233 233 233 X-L 5 THE NFLSA MISSION REPORTS PROHIBITED MANEUVERS
CENTER-OF-GRAVITY LIMITATIONS WEIGHT LIMITATIONS SECTION 6 FLIGHT
CHARACTERISTICS MINIMUM CONTROL SPEEDS SPINS AND SPIN RECOVERY FLIGHT
CONTROL EFFECTIVENESS FLIGHT CONFIGURATION CHARACTERISTICS PERFORMANCE
DATA APPENDIX I FLIGHT MANUAL SUPPLEMENT UTILITY FLIGHT MANUAL SECTION I
DESCRIPTION AIRPLANE ENGINE PROPELLANT SUPPLY SYSTEM ENGINE AND
PROPELLANT CONTROL HELIUM SYSTEM PROPELLANT PRESSURIZATION HELIUM SYSTEM
AUXILIARY POWER UNITS ELECTRICAL POWER SUPPLY SYSTEMS HYDRAULIC POWER
SUPPLY SYSTEMS FLIGHT CONTROL SYSTEMS MH-96 ADAPTIVE FLIGHT CONTROL
SYSTEM WING FLAP SYSTEM SPEED BRAKE SYSTEM LAUNCH SYSTEM LANDING GEAR
SYSTEM INSTRUMENTS INERTIAL ALL-ATTITUDE FLIGHT DATA. SYSTEM
(GYRO-STABILIZED PLATFORM) INSTRUMENTATION SYSTEM INDICATOR, CAUTION,
AND WARNING LIGHT SYSTEM CANOPY EJECTION SEAT AUXILIARY EQUIPMENT
SECTION 2 NORMAL PROCEDURES INTRODUCTION PREPARATION FOR FLIGHT
PREFLIGHT CHECK CAPTIVE TAXI AND FLIGHT TAKE-OFF CLIMB TO CRUISE
ALTITUDE PRETAUNCH (45,000 FEET AT .82 MACH) FLIGHT CHARACTERISTICS
ENGINE OPERATION ENGINE BURNOUT SHUTDOWN PROCEDURE DESCENT BEFORE
LANDING LANDING BEFORE LEAVING AIRPLANE SECTION 3 EMERGENCY PROCEDURES
ENGINE FAILURE CAPTIVE OPERATION EMERGENCIES EMERGENCY LAUNCH MAXIMUM
GLIDE FORCED LANDING FIRE OR EXPLOSION EJECTION VENTRAL JETTISON SYSTEM
FAILURE EMERGENCY ENTRANCE FUEL SYSTEM FAILURE TURBOPUMP FAILURE DURING
FLIGHT PROPELTANT JETTISONING APU SYSTEM FAILURE ELECTRICAL POWER SUPPLY
SYSTEM FAILURE HYDRAULIC SYSTEM FAILURE FLIGHT CONTROL HYDRAULIC SYSTEM
FAILURE SECTION 4 AUXILIARY EQUIPMENT AIR CONDITIONING AND
PRESSURIZATION SYSTEM COMMUNICATION AND ASSOCIATED ELECTRONIC EQUIPMENT
PILOT S OXYGEN SYSTEM LIGHTING EQUIPMENT MISCELLANEOUS EQUIPMENT
PHOTOGRAPHIC EQUIPMENT SECTION 5 OPERATING LIMITATIONS INSTRUMENT
MARKINGS ENGINE LIMITATIONS CAPTIVE FLIGHT LIMITATIONS LAUNCH
LIMITATIONS AIRSPEED LIMITATIONS VENTRAL JETTISON LIMITATIONS SPEED
BRAKE OPERATION STABILITY AUGMENTATION SYSTEM LIMITATIONS ACCELERATION
LIMITATIONS WING TIP POD LIMITATIONS ROLL LIMITATIONS 233 233 233 235
235 235 235 236 238 238 240 240 241 252 252 253 253 257 259 260 267 267
267 267 268 268 269 271 271 271 273 276 276 276 276 276 277 278 278 278
280 280 281 282 282 282 282 282 286 286 286 286 287 287 287 288 288 288
288 288 291 291 291 292 292 295 295 299 300 300 301 301 302 302 302 302
302 302 304 304 304 305 305 305 YAW (SIDE-SLIP) LIMITATIONS PROHIBITED
MANEUVERS BALLISTIC CONTROL SYSTEM LIMITATIONS LANDING LIMITATIONS
CENTER-OF-GRAVITY LIMITATIONS WEIGHT LIMITATIONS SECTION 6 FLIGHT
CHARACTERISTICS MINIMUM CONTROL SPEEDS SPINS AND SPIN RECOVERY FLIGHT
CONTROL EFFECTIVENESS FLIGHT CONFIGURATION CHARACTERISTICS APPENDIX 1
X-I5A-2 AIRPLANE SCOPE DESCRIPTION NORMAL PROCEDURES EMERGENCY
PROCEDURES OPERATING LIMITATIONS FLIGHT CHARACTERISTICS X-L5 PILOT
RESCUE MANUAL FOREWORD SEC.A-X-15 AIRPLANE GENERAL DESCRIPTION SEC. B -
PROPELLANTS AND GASES HELIUM PRESSURIZATION AND PNEUMATIC CONTROL SYSTEM
HAZARDS OF PROPELLANTS AND GASES SEC.C-FIRST AID HYDROGEN PEROXIDE
ANHYDROUS AMMONIA LIQUID OXYGEN LIQUID NITROGEN SEC. D - EMERGENCY
ESCAPE SYSTEM EJECTION SEAT SYSTEMS CANOPY SYSTEMS OPERATION OF CANOPY
CANOPY JETTISON SYSTEM CANOPY JETTISON SYSTEM (EMERGENCY) PARACHUTE
ASSEMBLY PILOT S EMERGENCY RADIO BEACON SEC. E - X-15 A/P 22S-2 HIGH
ALTITUDE FULL PRESSURE SUIT SEC. F - B-52 MODIFICATION SEC. G - PILOT
RESCUE PROCEDURE X-L5 PILOT REMOVAL RESCUE SECURING X-L5 AIRPLANE X-L5
PILOT AND B-52 CREW REMOVAL FROM X-I5/B-52 SEC. H - X-I5/B-52 EMERGENCY
CONDITIONS AND PROCEDURES PRIOR TO TAKEOFF IN FLIGHT PRIOR TO LANDING
X-15 EMERGENCY APPENDIX 1 X-L5 RESCUE PLAN APPENDIX 2 STANDARD OPERATING
PROCEDURES FOR X-L5 LANDING AT EDWARDS APPENDIX 3 USE OF A-FRAME
EMERGENCY HOIST X-L5 FLIGHT LOG X-I5THE MOVIE CORRESPONDENCE X-15
ACCIDENT REPORT X-L5 PRESSRELEASE X-L 5 CONTRACTOR ADVERTISEMENTS 305
305 305 305 308 308 310 310 310 310 311 312 312 312 314 316 316 317 323
323 323 325 327 327 328 328 328 329 329 329 330 331 331 332 333 333 333
334 335 337 337 337 338 340 340 340 341 341 341 347 348 349 384 392 393
395
|
| any_adam_object | 1 |
| author2 | Godwin, Robert |
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| author_facet | Godwin, Robert |
| building | Verbundindex |
| bvnumber | BV024500040 |
| ctrlnum | (OCoLC)249446560 (DE-599)BVBBV024500040 |
| dewey-full | 629.13338 |
| dewey-hundreds | 600 - Technology (Applied sciences) |
| dewey-ones | 629 - Other branches of engineering |
| dewey-raw | 629.13338 |
| dewey-search | 629.13338 |
| dewey-sort | 3629.13338 |
| dewey-tens | 620 - Engineering and allied operations |
| discipline | Verkehr / Transport |
| format | Book |
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| isbn | 1896522653 |
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| spelling | X-15 the NASA mission reports ; incorporating files from the USAF comp. from the archives & ed. by Robert Godwin Burlington Apogee Books 2000 408 S. Ill., graph. Darst. 1 CD-ROM (12 cm) txt rdacontent n rdamedia nc rdacarrier Systemvoraussetzungen: Minimum requirements: Pentium 90. - 4x CDROM drive. - Windows 95. - Recommended: Web Browser & Internet access Godwin, Robert edt GBV Datenaustausch application/pdf http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&local_base=BVB01&doc_number=018474813&sequence=000001&line_number=0001&func_code=DB_RECORDS&service_type=MEDIA Inhaltsverzeichnis |
| spellingShingle | X-15 the NASA mission reports ; incorporating files from the USAF |
| title | X-15 the NASA mission reports ; incorporating files from the USAF |
| title_auth | X-15 the NASA mission reports ; incorporating files from the USAF |
| title_exact_search | X-15 the NASA mission reports ; incorporating files from the USAF |
| title_full | X-15 the NASA mission reports ; incorporating files from the USAF comp. from the archives & ed. by Robert Godwin |
| title_fullStr | X-15 the NASA mission reports ; incorporating files from the USAF comp. from the archives & ed. by Robert Godwin |
| title_full_unstemmed | X-15 the NASA mission reports ; incorporating files from the USAF comp. from the archives & ed. by Robert Godwin |
| title_short | X-15 |
| title_sort | x 15 the nasa mission reports incorporating files from the usaf |
| title_sub | the NASA mission reports ; incorporating files from the USAF |
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