contract- RECIPIENT AWARD SUMMARY
| AWARD OVERVIEW |
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Agency Name: National Aeronautics and Space Administration |
Project Location:
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Award Number: NND07AA08B |
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Funding Amount:
$0 |
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Ending Date:
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RECIPIENT INFORMATION (AWARD)
| RECIPIENT INFORMATION (AWARD) |
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Recipient Name:
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BOEING COMPANY, THE |
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Recipient Address:
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J S MCDONNELL BLVD |
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Recipient City:
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SAINT LOUIS |
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Recipient State:
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MO |
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Recipient Zip Code:
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631661939 |
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Congressional District:
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No Data Available |
DESCRIPTION OF WORK/SERVICE PERFORMED
MODIFICATION ISSUED TO INCORPORATE ARRA CLUAES, REPORTING AND ADD NEW CLIN.
| Other Awards |
Amount:
$0
Award Description: MODIFICATION ISSUED TO INCORPORATE ARRA CLUAES, REPORTING AND ADD NEW CLIN. |
Amount:
$198,641
Award Description: TAS::80 0125:: RECOVERY ACT FUNDS SUPPORT NASA LANGLEY RESEARCH CENTER IN RESEARCH RELATED TO THE STUDY OF SYSTEM LEVEL CONCEPTS AND SPECIFIC MITIGATION CONCEPTS FOR IMPROVING THE MATERIAL AND STRUCTURAL DURABILITY FOR TRANSPORT FUSELAGE STRUCTURES
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Amount:
$0
Award Description: TAS::80 0125:: RECOVERY ACT FUNDS-CLIN 1 AAD- NRA W/BOEING CO. AGREEMENT #NNL10AA00B,TASK ORDER #NNL10AB34T
THE PURPOSE OF THIS TASK ORDER IS TO SUPPORT NASA LANGLEY RESEARCH CENTER IN RESEARCH RELATED TO THE STUDY OF SYSTEM LEVEL CONCEPTS (CONCEPTS THAT VIEW THE PROCESS AS A WHOLE, INSTEAD OF ADDRESSING ONE PART OF THE PROCESS WITHOUT REGARD TO HOW CHANGING THAT PART WILL IMPACT THE OTHER PARTS OF THE PROCESS) AND SPECIFIC MITIGATION CONCEPTS FOR IMPROVING THE MATERIAL AND STRUCTURAL DURABILITY FOR TRANSPORT FUSELAGE STRUCTURES.
THE GOAL OF THIS EFFORT IS TO DEVELOP SYSTEM-LEVEL CONCEPTS FOR IMPLEMENTING ADVANCED CAPABILITIES TO TRANSPORT FUSELAGE STRUCTURES IN REAL-WORLD OPERATIONAL ENVIRONMENTS. THE CONTRACTOR SHALL IDENTIFY AND ASSESS SYSTEM-LEVEL CONCEPTS THAT GUIDE THE INTEGRATION OF MULTIPLE TECHNOLOGIES AND THEIR ASSOCIATED OPERATIONAL PRACTICES FOR DETECTION, PREDICTION AND MITIGATION/MANAGEMENT; AND DEFINE REQUIREMENTS FOR INDIVIDUAL TECHNOLOGIES AT THE FOUNDATIONAL RESEARCH LEVEL (RESEARCH ON WHICH ALL THE CURRENT AND FUTURE PROCESSES ARE BASED). TO THIS END, THE CONTRACTOR SHALL CONDUCT A SYSTEMS STUDY OF THE TRANSPORT FUSELAGE STRUCTURE TO ASSESS CURRENT PRACTICES AND FUTURE CONCEPTS FOR FULL LIFE CYCLE AIRWORTHINESS MANAGEMENT OF AIRCRAFT STRUCTURES (INCLUDING DESIGN, CERTIFICATION, MAINTENANCE, AND REPAIR). OF SPECIFIC INTEREST ARE METHODS FOR NEW FUSELAGE DESIGN, AND METHODS AND TECHNOLOGIES FOR INSPECTION AND MAINTENANCE THAT ENABLE THE INTRODUCTION OF ADVANCED MATERIALS AND STRUCTURES WHILE MAINTAINING THE SAME OR HIGHER LEVEL OF SAFETY. THE CONTRACTOR SHALL SUBMIT A FINAL REPORT THAT SUMMARIZES THE CURRENT STATE OF PRACTICE (CURRENT METHODS FOR PERFORMING THE REQUIRED PROCEDURES), LONG-TERM CONCEPTS THAT WILL RESULT IN A SIGNIFICANT IMPROVEMENT IN PRACTICE AND A RECOMMENDED APPROACH FOR A SHORT-TERM DEMONSTRATION OF THE KEY ELEMENTS OF THE LONG-TERM CONCEPT. |
Amount:
$596,245
Award Description: TAS::80 0125::TAS RECOVERY ACT FUNDS
NASA'S AVIATION SAFETY PROGRAM IS CONDUCTING RESEARCH DIRECTED AT IMPROVING THE SAFETY OF CURRENT AND FUTURE AIRCRAFT OPERATING IN THE NATIONAL AIRSPACE SYSTEM. THE RESEARCH FOCUS IS ON THE WAY VEHICLES ARE DESIGNED, BUILT, OPERATED, AND MAINTAINED, AND IS ORGANIZED INTO FOUR PROJECT AREAS: 1) INTEGRATED VEHICLE HEALTH MANAGEMENT, 2) INTEGRATED INTELLIGENT FLIGHT DECK, 3) INTEGRATED RESILIENT AIRCRAFT CONTROL, AND 4) AIRCRAFT AGING AND DURABILITY. THIS RESEARCH STATEMENT OF WORK SPECIFICALLY ADDRESSES THE INTEGRATED VEHICLE HEALTH MANAGEMENT (IVHM) PROJECT WHICH IS CONDUCTING RESEARCH INTO VEHICLE HEALTH MANAGEMENT TECHNOLOGIES THAT WILL DETECT, DIAGNOSE, PREDICT, AND MITIGATE ADVERSE EVENTS THAT OCCUR DURING FLIGHT. ADVERSE EVENTS INCLUDE THOSE THAT ARISE FROM SYSTEM, SUBSYSTEM, OR COMPONENT FAULTS OR FAILURES DUE TO DAMAGE, DEGRADATION, OR ENVIRONMENTAL HAZARDS (SUCH AS TURBULENCE, ELECTROMAGNETIC FIELDS, AND LIGHTNING).
IN PARTICULAR, THIS EFFORT SEEKS TO DEVELOP A VEHICLE-LEVEL REASONING SYSTEM (VLRS) THAT WILL LOOK ACROSS ALL OF THE VEHICLE SUBSYSTEMS (PROPULSION, FLIGHT SYSTEMS, AIRFRAME, AND SOFTWARE) FOR PURPOSES OF DETERMINING WHETHER AN ADVERSE EVENT HAS OCCURRED, DIAGNOSE THE CAUSE, PREDICT THE EFFECT ON THE REMAINING USEFUL LIFE OF THE VEHICLE, AND TAKE APPROPRIATE STEPS TO MITIGATE THE EVENT AS APPROPRIATE. THE VLRS MAY TAKE ADVANTAGE OF COMPONENT, SUBSYSTEM, AND VEHICLE LEVEL MODELS WHICH WOULD REPRESENT CONNECTIVITY AND POTENTIAL CAUSAL CHAINS OF FAILURE. SIMILARLY, PHYSICS-BASED MODELS OF DAMAGE PROPAGATION FOR CERTAIN SUBSYSTEMS (SUCH AS THE AIRFRAME OR ACTUATORS) MAY BE APPROPRIATE FOR INCLUSION IN THE VLRS. VLRS TECHNOLOGIES WILL PRODUCE A SIGNIFICANT AMOUNT OF DATA THAT CAN BE USED TO ENABLE CONDITIONED-BASED MAINTENANCE (CBM) FOR AIRCRAFT. WITH CBM, MAINTENANCE ACTIONS ARE PERFORMED ONLY WHEN THERE IS AN ANTICIPATED NEED, AS OPPOSED TO REGULARLY SCHEDULED MAINTENANCE ACTIONS. IN ORDER TO ANTICIPATE THE NEED FOR MAINTENANCE, A CBM SYSTEM WILL USE INFORMATION AND DATA DERIVED FROM ONBOARD SENSORS AND SUPPORTING INSTRUMENTATION (SUCH AS THOSE UNDER DEVELOPMENT IN NASA'S IVHM PROJECT) AS WELL AS MAINTENANCE LOGS FOR THE VEHICLE.
THIS STATEMENT OF WORK IS THE RESULT OF PROPOSAL 09-IVHM1-09-0009 SUBMITTED BY THE BOEING COMPANY FOR AWARD UNDER THE NASA HEADQUARTERS AERONAUTICS RESEARCH MISSION DIRECTORATE (ARMD) NASA RESEARCH ANNOUNCEMENT (NRA) NNH09ZEA001N ENTITLED, RESEARCH OPPORTUNITIES IN AERONAUTICS 2009, AMENDMENT 1, SUBTOPIC B.4, PROJECT INTEGRATED VEHICLE HEALTH MANAGEMENT (IVHM), TOPIC VEHICLE-LEVEL REASONING SYSTEM / EVALUATION OF MULTIDISCIPLINARY IVHM TECHNOLOGIES, TOOLS, AND TECHNIQUES.
NASA'S AVIATION SAFETY PROGRAM IS CONDUCTING RESEARCH DIRECTED AT IMPROVING THE SAFETY OF CURRENT AND FUTURE AIRCRAFT OPERATING IN THE NATIONAL AIRSPACE SYSTEM. THE RESEARCH FOCUS IS ON THE WAY VEHICLES ARE DESIGNED, BUILT, OPERATED, AND MAINTAINED, AND IS ORGANIZED INTO FOUR PROJECT AREAS: 1) INTEGRATED VEHICLE HEALTH MANAGEMENT, 2) INTEGRATED INTELLIGENT FLIGHT DECK, 3) INTEGRATED RESILIENT AIRCRAFT CONTROL, AND 4) AIRCRAFT AGING AND DURABILITY. THIS RESEARCH STATEMENT OF WORK SPECIFICALLY ADDRESSES THE INTEGRATED VEHICLE HEALTH MANAGEMENT (IVHM) PROJECT WHICH IS CONDUCTING RESEARCH INTO VEHICLE HEALTH MANAGEMENT TECHNOLOGIES THAT WILL DETECT, DIAGNOSE, PREDICT, AND MITIGATE ADVERSE EVENTS THAT OCCUR DURING FLIGHT. ADVERSE EVENTS INCLUDE THOSE THAT ARISE FROM SYSTEM, SUBSYSTEM, OR COMPONENT FAULTS OR FAILURES DUE TO DAMAGE, DEGRADATION, OR ENVIRONMENTAL HAZARDS (SUCH AS TURBULENCE, ELECTROMAGNETIC FIELDS, AND LIGHTNING). |
Amount:
$0
Award Description: TAS::80 0125::TAS
"RECOVERY"- CLIN 00002 TASK ORDER NND10BO13T: THE MODIFICATION IS ISSUED TO INCORPORATE THE REVISION UNDER SECTION 7.0: PERIOD OF PERFORMANCE OF THE SOW. |
Amount:
$592,623
Award Description: TAS::80 0125::TAS
"RECOVERY"- CLIN 00002 TASK ORDER NND10BO13T: BOEING SHALL
PROVIDE NASA WITH BUILDING, TESTING, DOCUMENTATION, AND DELIVER OF A PRODUCTION SUPPORT FLIGHT CONTROL COMPUTER (PSFCC) SHIPSET USING SPARE FLIGHT COMPUTER CARDS FROM NASA'S F-15 AIRCRAFT NASA 837 OBTAINED FROM NASA DRYDEN FLIGHT RESEARCH CENTER (DFRC), IN ACCORDANCE WITH THE STATEMENT OF WORK ENTITLED, " DEVELOPMENT AND DELIVERY OF A SPARE F/A-18 PRODUCTION SUPPORT FLIGHT CONTROL COMPUTER (PSFCC) SHIPSET", DATED FEBRUARY 10, 2010.
"RECOVERY CLIN 00002 REPORTING REQUIREMENTS |
Amount:
$0
Award Description: TAS::80 0125::TAS ENGINEERING AND TECHNICAL SUPPORT FOR THE DFRC RESEARCH AIRCRAFT AND OPERATIONS AIRCRAFT. NASA DFRC HAS SEVERAL TEST AIRCRAFT MANUFACTURED BY BOEING, INCLUDING TWO F-18S AND TWO F-15S. THESE AIRCRAFT ARE MODIFIED WITH RESEARCH INSTRUMENTATION SYSTEM, AND OTHER CAPABILITIES FOR FLYING RESEARCH PROJECTS |
Amount:
$0
Award Description: TAS::80 0125::TAS ENGINEERING AND TECHNICAL SUPPORT FOR THE DFRC RESEARCH AIRCRAFT AND OPERATIONS AIRCRAFT. NASA DFRC HAS SEVERAL TEST AIRCRAFT MANUFACTURED BY BOEING, INCLUDING TWO F-18S AND TWO F-15S. THESE AIRCRAFT ARE MODIFIED WITH RESEARCH INSTRUMENTATION SYSTEM, AND OTHER CAPABILITIES FOR FLYING RESEARCH PROJECTS |
Amount:
$0
Award Description: TAS::80 0125::TAS
"RECOVERY"- CLIN 00002 TASK ORDER NND10BO13T: BOEING SHALL
PROVIDE NASA WITH BUILDING, TESTING, DOCUMENTATION, AND DELIVER OF A PRODUCTION SUPPORT FLIGHT CONTROL COMPUTER (PSFCC) SHIPSET USING SPARE FLIGHT COMPUTER CARDS FROM NASA'S F-15 AIRCRAFT NASA 837 OBTAINED FROM NASA DRYDEN FLIGHT RESEARCH CENTER (DFRC), IN ACCORDANCE WITH THE STATEMENT OF WORK ENTITLED, " DEVELOPMENT AND DELIVERY OF A SPARE F/A-18 PRODUCTION SUPPORT FLIGHT CONTROL COMPUTER (PSFCC) SHIPSET", DATED FEBRUARY 10, 2010.
"RECOVERY CLIN 00002 REPORTING REQUIREMENTS
MODIFICATION TO REVISE THE DELIVERABLE DUE DATE UNDER SECTION 7:4. |
Amount:
$0
Award Description: TAS::80 0125::TAS
"RECOVERY"- CLIN 00002 TASK ORDER NND10BO13T: BOEING SHALL
PROVIDE NASA WITH BUILDING, TESTING, DOCUMENTATION, AND DELIVER OF A PRODUCTION SUPPORT FLIGHT CONTROL COMPUTER (PSFCC) SHIPSET USING SPARE FLIGHT COMPUTER CARDS FROM NASA'S F-15 AIRCRAFT NASA 837 OBTAINED FROM NASA DRYDEN FLIGHT RESEARCH CENTER (DFRC), IN ACCORDANCE WITH THE STATEMENT OF WORK ENTITLED, " DEVELOPMENT AND DELIVERY OF A SPARE F/A-18 PRODUCTION SUPPORT FLIGHT CONTROL COMPUTER (PSFCC) SHIPSET", DATED FEBRUARY 10, 2010.
"RECOVERY CLIN 00002 REPORTING REQUIREMENTS |
Amount:
$0
Award Description: TAS::80 0125::TAS
"RECOVERY"- CLIN 00002 TASK ORDER NND10BO13T: BOEING SHALL
PROVIDE NASA WITH BUILDING, TESTING, DOCUMENTATION, AND DELIVER OF A PRODUCTION SUPPORT FLIGHT CONTROL COMPUTER (PSFCC) SHIPSET USING SPARE FLIGHT COMPUTER CARDS FROM NASA'S F-15 AIRCRAFT NASA 837 OBTAINED FROM NASA DRYDEN FLIGHT RESEARCH CENTER (DFRC), IN ACCORDANCE WITH THE STATEMENT OF WORK ENTITLED, " DEVELOPMENT AND DELIVERY OF A SPARE F/A-18 PRODUCTION SUPPORT FLIGHT CONTROL COMPUTER (PSFCC) SHIPSET", DATED FEBRUARY 10, 2010.
"RECOVERY CLIN 00002 REPORTING REQUIREMENTS |
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