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NASA's Space Shuttle Program: Shuttle Avionics Design Constraints and Considerations - Guide Book Based on KSC Engineering's Shuttle Turnaround Experi
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1132957NASA's Space Shuttle Program: Shuttle Avionics Design Constraints and Considerations - Guide Book Based on KSC Engineering's Shuttle Turnaround Experihttps://www.gandhi.com.mx/nasa-s-space-shuttle-program-shuttle-avionics-design-constraints-and-considerations-guide-book-based-on-ksc-engineering-s-shuttle-turnaround-experience-lessons-learned-1/phttps://gandhi.vtexassets.com/arquivos/ids/1301494/e19e45d5-57e0-4f59-89cb-b631de23c817.jpg?v=638337823964500000131131MXNProgressive ManagementInStock/Ebooks/<p>This unique NASA report provides information and lessons learned from shuttle avionics testing constraints. Objective - Consolidate within one report the operational Constraints and Considerations for launch site testing of the present Shuttle Avionics systems. Constraint - Testing that requires special vehicle configurations and ground support equipment configurations. Consideration - Testing configurations that have driven special infrastructure/ resource requirements, or have high failure rates. Purpose - To provide to the designers of future avionics systems the information required to possibly design out these concerns.</p><p>Contents: GENERAL 1. INSTRUMENTATION COEFFICIENTS 2. TELEMETRY DATA AVAILABILITY 3. AVIONICS COOLING 4. CONNECTOR RETEST 5. CONNECTOR MATED INDICATION 6. PARALLEL SWITCH CONTROL 7. MAN-IN-THE-LOOP 8. AVIONICS LRU ACCESS / MOUNTING 9. AVIONICS LRU FASTENING DEVICES 10. AVIONICS LRU GROUND HANDLING EQUIPMENT 11. AVIONICS BITE / TEST POINTS 12. CRITICAL REDUNDANT POWER VERIFICATION 13. SOFTWARE IN END-ITEM 14. LOCAL OPF OPERATION 15. UNPLANNED WORK 16. VENDOR DRAWINGS 17. HYDRAULICS DPS 1. MEMORY DUMP & COMPARE 2. MASS STORAGE DEVICE CAPABILITY 3. GPC MULTIPLE MEMORY CONFIGURATIONS 4. LAUNCH BUS SPEEDUP 5. MDM RETEST 6. CRT VIDEO OUTPUT GNC 1. INDEPENDENT CONTROL OF ACTUATOR POWER 2. ENGINE COLLISION 3. SSME HYDRAULIC CIRCUITS ISOLATION 4. ENGINE CHANGEOUTS DRIVE CLEARANCE TESTS 5. SRB TVC FLEX BEARING RESTRICTION 6. SRB NOZZLE FLEX BEARING TEMPERATURE 7. EXCESSIVE AEROSURFACE POSITIONING REQUIREMENTS 8. NOSEWHEEL STEERING (NWS) TESTING 9. BRAKES/ANTI-SKID MAINTAINABILITY 10. REACTION CONTROL SYSTEM (RCS) VERNIER DRIVERS 11. RCS DRIVERS-DRIVER POWER ACTIVATION 12. ACCELEROMETER ASSEMBLIES (AA) INACCESSIBLE 13. IMU HEALTH ASSESSMENT 14. STAR TRACKER LENS & LIGHT SHADE INSPECTION 15. STAR TRACKER CONTAMINATION 16. ENTRY AIR DATA SENSORS UNDEPENDABLE 17. DEPLOYABLE ENTRY AIR DATA PROBES TELECOMM 1. HOLLOW RF WAVEGUIDES THAT PENETRATE PRESSURIZED STRUCTURE 2. HAZARDOUS RF SYSTEMS & GROUND ANTENNA COUPLER REQUIREMENTS RMS 1. AUDIBLE TESTING SSME 1. SSME INSTRUMENTATION CALIBRATION COEFFICIENTS GLOSSARY/ACRONYMS</p>...1125859NASA's Space Shuttle Program: Shuttle Avionics Design Constraints and Considerations - Guide Book Based on KSC Engineering's Shuttle Turnaround Experi131131https://www.gandhi.com.mx/nasa-s-space-shuttle-program-shuttle-avionics-design-constraints-and-considerations-guide-book-based-on-ksc-engineering-s-shuttle-turnaround-experience-lessons-learned-1/phttps://gandhi.vtexassets.com/arquivos/ids/1301494/e19e45d5-57e0-4f59-89cb-b631de23c817.jpg?v=638337823964500000InStockMXN99999DIEbook20149781310569180_W3siaWQiOiIwOTljZjcyMi01NGNlLTRmN2EtOTJkZS00NDY0YmVkMTljNjYiLCJsaXN0UHJpY2UiOjEzMSwiZGlzY291bnQiOjAsInNlbGxpbmdQcmljZSI6MTMxLCJpbmNsdWRlc1RheCI6dHJ1ZSwicHJpY2VUeXBlIjoiSXBwIiwiY3VycmVuY3kiOiJNWE4iLCJmcm9tIjoiMjAyNC0wNS0xN1QyMjowMDowMFoiLCJyZWdpb24iOiJNWCIsImlzUHJlb3JkZXIiOmZhbHNlfV0=9781310569180_<p>This unique NASA report provides information and lessons learned from shuttle avionics testing constraints. Objective - Consolidate within one report the operational Constraints and Considerations for launch site testing of the present Shuttle Avionics systems. Constraint - Testing that requires special vehicle configurations and ground support equipment configurations. Consideration - Testing configurations that have driven special infrastructure/ resource requirements, or have high failure rates. Purpose - To provide to the designers of future avionics systems the information required to possibly design out these concerns.</p><p>Contents: GENERAL 1. INSTRUMENTATION COEFFICIENTS 2. TELEMETRY DATA AVAILABILITY 3. AVIONICS COOLING 4. CONNECTOR RETEST 5. CONNECTOR MATED INDICATION 6. PARALLEL SWITCH CONTROL 7. MAN-IN-THE-LOOP 8. AVIONICS LRU ACCESS / MOUNTING 9. AVIONICS LRU FASTENING DEVICES 10. AVIONICS LRU GROUND HANDLING EQUIPMENT 11. AVIONICS BITE / TEST POINTS 12. CRITICAL REDUNDANT POWER VERIFICATION 13. SOFTWARE IN END-ITEM 14. LOCAL OPF OPERATION 15. UNPLANNED WORK 16. VENDOR DRAWINGS 17. HYDRAULICS DPS 1. MEMORY DUMP & COMPARE 2. MASS STORAGE DEVICE CAPABILITY 3. GPC MULTIPLE MEMORY CONFIGURATIONS 4. LAUNCH BUS SPEEDUP 5. MDM RETEST 6. CRT VIDEO OUTPUT GNC 1. INDEPENDENT CONTROL OF ACTUATOR POWER 2. ENGINE COLLISION 3. SSME HYDRAULIC CIRCUITS ISOLATION 4. ENGINE CHANGEOUTS DRIVE CLEARANCE TESTS 5. SRB TVC FLEX BEARING RESTRICTION 6. SRB NOZZLE FLEX BEARING TEMPERATURE 7. EXCESSIVE AEROSURFACE POSITIONING REQUIREMENTS 8. NOSEWHEEL STEERING (NWS) TESTING 9. BRAKES/ANTI-SKID MAINTAINABILITY 10. REACTION CONTROL SYSTEM (RCS) VERNIER DRIVERS 11. RCS DRIVERS-DRIVER POWER ACTIVATION 12. ACCELEROMETER ASSEMBLIES (AA) INACCESSIBLE 13. IMU HEALTH ASSESSMENT 14. STAR TRACKER LENS & LIGHT SHADE INSPECTION 15. STAR TRACKER CONTAMINATION 16. ENTRY AIR DATA SENSORS UNDEPENDABLE 17. DEPLOYABLE ENTRY AIR DATA PROBES TELECOMM 1. HOLLOW RF WAVEGUIDES THAT PENETRATE PRESSURIZED STRUCTURE 2. HAZARDOUS RF SYSTEMS & GROUND ANTENNA COUPLER REQUIREMENTS RMS 1. AUDIBLE TESTING SSME 1. SSME INSTRUMENTATION CALIBRATION COEFFICIENTS GLOSSARY/ACRONYMS</p>...9781310569180_Progressive Managementlibro_electonico_1a9871f3-03d2-3369-80be-56ccfe008974_9781310569180;9781310569180_9781310569180Progressive ManagementInglésMéxicohttps://getbook.kobo.com/koboid-prod-public/smashwords-epub-83f547be-c6a0-4f3f-a000-6a11529f4d1d.epub2014-08-13T00:00:00+00:00Progressive Management