Award search
Awards for “boeing”
25 awards on this page · sorted by amount · page 167
| Award ID | Recipient | Awarding agency | Amount | Start | End | NAICS | Description |
|---|---|---|---|---|---|---|---|
| 80LARC19F0056 | THE BOEING COMPANY | National Aeronautics and Space Administration | $4.82M | 2019-05-22 | 2021-06-30 | 541712 | PROPULSION AIRFRAME AEROACOUSTICS AND AIRCRAFT SYSTEM NOISE FLIGHT TEST ON THE ECODEMONSTRATOR 2019 BOEING 787 TESTBED AIRCRAFT. THE SCOPE OF THIS TASK ORDER IS TO PERFORM A TEST FLIGHT CAMPAIGN TO ACQUIRE ACOUSTIC FLIGHT DATA FOR THE PURPOSES OF PAA EFFECTS AND AIRCRAFT SYSTEM NOISE OBJECTIVES WITH THE CONTRACTOR PROVIDING FLIGHT SERVICES, AIRCRAFT DATA AND INFORMATION, ACOUSTIC INSTRUMENTATION, AND DATA PROCESSING SERVICES. |
| FA813419F0014 | THE BOEING COMPANY | Department of Defense | $4.81M | 2019-06-04 | 2019-09-17 | 336413 | E-4B ENGINE SUSTAINMENT |
| FA875012C0042 | THE BOEING COMPANY | Department of Defense | $4.81M | 2012-01-30 | 2014-03-30 | 541712 | COMMAND&CONTROL OF CYBER ASSETS FOR MISSION ASSURANCE (C2 CAMA) |
| 0104 | THE BOEING COMPANY | Department of Defense | $4.8M | 2012-11-05 | 2015-06-30 | 336411 | FY12 (F) ANAV KITS |
| 0001 | THE BOEING COMPANY (0674) | Department of Defense | $4.8M | 2006-09-21 | 2009-12-31 | 336413 | — |
| 0089 | THE BOEING COMPANY (0674) | Department of Defense | $4.8M | 2008-01-01 | 2011-09-10 | 336413 | KADENA CY2008 SIMULATOR SERVICE |
| FA860926FB015 | THE BOEING COMPANY | Department of Defense | $4.8M | 2026-01-08 | 2027-01-08 | 336411 | THE UNITED STATES GOVERNMENT (USG) AND THE KC-46 PROGRAM OFFICE SEEKS TO ESTABLISH A DIMINISHING MANUFACTURING SOURCES AND MATERIAL SHORTAGES (DMSMS) CONTRACT TO PREPARE, IDENTIFY, ASSESS, AND ANALYZE ENTERPRISE-WIDE SOLUTIONS. |
| 0013 | THE BOEING COMPANY | Department of Defense | $4.8M | 2011-07-07 | 2015-04-30 | 336413 | TO PROCURE FIRST RELATED PRODUCTS |
| FA813426FB011 | THE BOEING COMPANY | Department of Defense | $4.8M | 2025-12-17 | 2026-03-10 | 488190 | CONTRACTOR LOGISTICS SUPPORT FOR THE C-32/C-40 AIRCRAFT FLEETS |
| H9224124F0014 | BOEING SIKORSKY AIRCRAFT SUPPORT, LLC | Department of Defense | $4.79M | 2024-02-01 | 2025-01-31 | 488190 | DATA MANAGEMENT/ANALYSIS |
| 0097 | THE BOEING COMPANY | Department of Defense | $4.79M | 2008-09-19 | 2012-08-31 | 336411 | ECP 6318 USN NON RECURRING |
| FA852617F0002 | THE BOEING COMPANY | Department of Defense | $4.79M | 2016-10-01 | 2017-09-30 | 336411 | IGF::OT::IGF TOOLING SUSTAINMENT |
| W15QKN24F0081 | THE BOEING COMPANY | Department of Defense | $4.79M | 2023-12-15 | 2025-09-30 | 334515 | NGATS DELIVERY ORDER |
| 0006 | THE BOEING COMPANY | Department of Defense | $4.79M | 2011-06-01 | 2014-06-30 | 332993 | IAF FMS SDB I PHASE 2 TEST ASSETS |
| SC14 | THE BOEING COMPANY | Department of Defense | $4.79M | 2013-08-28 | 2017-09-30 | 336411 | C-17 INITIAL SPARES FOR UK-7 |
| DTFAWA10D00019CALL0008 | BOEING AEROSPACE OPERATIONS, INC. | Department of Transportation | $4.79M | 2011-09-28 | 2014-04-01 | 541330 | SE-2020 TAS::69 8107::TAS |
| 0471 | THE BOEING COMPANY | Department of Defense | $4.79M | 2007-06-29 | 2011-01-31 | 336413 | CH-47 SPARE PARTS |
| Z552 | THE BOEING COMPANY | Department of Defense | $4.78M | 2015-08-24 | 2022-09-30 | 336411 | F/A-18 A-D AND E/F MODIFICATIONS |
| 0012 | BOEING AEROSPACE OPERATIONS, INC. | Department of Defense | $4.78M | 2007-05-16 | 2010-03-31 | 336411 | ENGINEERING SERVICES IN SUPPORT OF THE C-17 DEPOT STAND-UP. |
| 0044 | BELL BOEING JOINT PROJECT OFFICE | Department of Defense | $4.78M | 2006-06-08 | 2006-12-08 | 336411 | 200609!438292!1700!N00019!NAVAL AIR SYSTEMS COMMAND !N0001904G0007 !A!N! !N!0044 ! !20060608!20061229!106632750!106632750!106632750!N!BELL BOEING JOINT PROJECT OFFI!47123 BUSE RD BUILDING 227!PATUXENT RIVER !MD!20670!60000!101!42!PHILADELPHIA !PHILADELPHIA !PENN !+000003387034!N!N!000000000000!J016!MAINT & REPAIR OF EQ/AIRCRAFT COMPS & ACCYS !A1A!AIRFRAMES AND SPARES !212 !V22 !336413!E! !4! ! ! ! ! !99990909!B! ! !A! !D!U!Y!1!001!N!1A!A!N!Z! ! !N!C!N! ! ! !A!A!A!A!000!A!B!N! ! ! !Y!1700!N00019!0001! ! |
| 0026 | THE BOEING COMPANY | Department of Defense | $4.78M | 2007-10-12 | 2008-09-30 | 336413 | SERVOCYLINDER, AFT SMCS |
| SPRTA118F0375 | BOEING DISTRIBUTION, INC. | Department of Defense | $4.77M | 2018-05-07 | 2019-11-01 | 336413 | AIRCRAFT COMPRESSOR ROTOR |
| 0066 | THE BOEING COMPANY | Department of Defense | $4.77M | 2009-10-01 | 2013-12-23 | 336411 | POST DELIVERY SUPPORT (PDS) XI |
| RJ27 | THE BOEING COMPANY | Department of Defense | $4.77M | 2008-09-26 | 2010-12-31 | 336411 | LOGISTIC SUPPORT IETM |
| NNL10AB00T | THE BOEING COMPANY | National Aeronautics and Space Administration | $4.76M | 2010-02-18 | 2011-03-30 | 541710 | TAS::80 0125::TAS RECOVERY ACT FUNDS RECOVERY - SMAAATAV TASK TITLE: HWB MULTI BAY TEST ARTICLE DESIGN AND TOOLING 1.0 BACKGROUND: NASA CREATED THE ENVIRONMENTALLY RESPONSIBLE AVIATION (ERA) PROJECT TO EXPLORE AND DOCUMENT THE FEASIBILITY, BENEFITS AND TECHNICAL RISK OF VEHICLE CONCEPTS AND ENABLING TECHNOLOGIES THAT WILL REDUCE THE IMPACT OF AVIATION ON THE ENVIRONMENT. TODAY'S CURRENT GENERATION OF AIRCRAFT HAS BENEFITTED FROM NASA INVESTMENTS IN AERONAUTICAL RESEARCH THAT HAVE IMPROVED FUEL EFFICIENCIES, LOWERED NOISE LEVELS AND LESSENED HARMFUL EMISSIONS. ALTHOUGH SUBSTANTIAL PROGRESS HAS BEEN MADE, MUCH MORE NEEDS TO BE DONE. THE NATION'S AIR TRANSPORTATION SYSTEM WILL EXPAND BY A FACTOR OF TWO OR THREE WITHIN THE NEXT TWO DECADES, POTENTIALLY INCREASING AVIATION'S CONTRIBUTION TO CLIMATE CHANGE. THE ERA PROJECT WORKS TO REDUCE THE ENVIRONMENTAL HARM THAT COULD RESULT FROM SUCH AN EXPANSION. AMONG THE TECHNOLOGIES TO BE EXPLORED IN THE ERA PROJECT ARE THE FOLLOWING: UNCONVENTIONAL AIRCRAFT CONFIGURATIONS THAT HAVE HIGHER LIFT TO DRAG RATIO, REDUCED DRAG AND REDUCED COMMUNITY NOISE; DRAG REDUCTION THROUGH LAMINAR FLOW; ADVANCED COMPOSITE STRUCTURAL CONCEPTS FOR WEIGHT REDUCTION; LOW NOX COMBUSTORS; AND PROPULSION AND AIRFRAME INTEGRATION FOR NOISE REDUCTION AND FUEL-BURN IMPROVEMENTS. THE ERA PROJECT WILL FOCUS ON ENVIRONMENTAL ISSUES ASSOCIATED WITH AIRCRAFT, INCLUDING FUEL BURN, EMISSIONS, AND NOISE. THE PROJECT WILL EXPLORE AND DOCUMENT THE FEASIBILITY, BENEFITS AND TECHNICAL RISK OF VEHICLE CONCEPTS AND ENABLING TECHNOLOGIES IDENTIFIED TO HAVE THE POTENTIAL TO MITIGATE THE IMPACT OF AVIATION ON THE ENVIRONMENT. THIS RESEARCH DIRECTLY SUPPORTS THE NATIONAL AERONAUTICS RESEARCH AND DEVELOPMENT POLICY TO DEVELOP APPROPRIATE ENVIRONMENTAL PROTECTION MEASURES TO ENSURE CONTINUED GROWTH IN AIR TRANSPORTATION. THE PRIMARY STRUCTURAL CONCEPT BEING DEVELOPED UNDER THE ERA PROGRAM IN THE AIRFRAME TECHNOLOGY ELEMENT IS THE PULTRUDED ROD STITCHED EFFICIENT UNITIZED STRUCTURE (PRSEUS) DESIGN. THE PRSEUS DESIGN APPROACH IS PART OF THE ERA EFFORT TO ADDRESS FUEL BURN (C02 EMISSIONS) BY REDUCING THE WEIGHT OF ADVANCED STRUCTURES. REDUCING FUEL BURN REDUCES THE NEED TO USE RESOURCES AND REDUCES POLLUTION TO THE ENVIRONMENT. THE APPROACH MOVES FROM SAFE-LIFE TO FAIL-SAFE DESIGN WITH A LIGHTWEIGHT COMPOSITE STRUCTURE. PRSEUS REPRESENTS A NEW CONCEPT IN COMPOSITE DESIGN THEORY AND MANUFACTURING METHODS. IT IS A CONSCIOUS PROGRESSION AWAY FROM CONVENTIONAL LAMINATED AND BONDED ASSEMBLIES TOWARD LARGER ONE-PIECE PANEL DESIGNS WITH SEAMLESS TRANSITIONS AND DAMAGE-ARREST INTERFACES SUCH AS STITCH ROWS AND TEAR STRAPS. IT FOCUSES ON A NEW STRUCTURAL CONCEPT THAT INTEGRATES SKIN, STRINGERS, AND FRAME ELEMENTS INTO A SINGLE LARGE PANEL IN WHICH ALL ELEMENTS ARE SIMULTANEOUSLY CURED (OR CO-CURED) IN ONE HIGH-TEMPERATURE CURE CYCLE. THE RESULTING STRUCTURE IS A NOVEL SOLUTION FOR ADDRESSING THE DEMANDING FUSELAGE LOADING REQUIREMENTS INHERENT IN A PRESSURIZED SHAPED VEHICLE LIKE THE HYBRID WING OR BLENDED WING BODY (HWB/BWB) CONCEPT. THE PRSEUS CONCEPT BUILDS UPON, EXTENDS, AND TAILORS THESE STRUCTURAL TECHNOLOGIES IN ORDER TO MEET THE DEMANDING CHALLENGES ASSOCIATED WITH VEHICLES WITH SHAPES AND LOAD PATHS DIFFERENT FROM TODAY S TRADITIONAL WING AND CIRCULAR FUSELAGE STRUCTURES. HAVING DEMONSTRATED THE UNIQUE CAPABILITY OF THE HYBRID WING BODY (HWB) PULTRUDED ROD STITCHED EFFICIENT UNITIZED STRUCTURE (PRSEUS) STRUCTURAL CONCEPT TO ECONOMICALLY PRODUCE LARGE INTEGRATED STRUCTURAL PANELS, THE PRIMARY AIRFRAME DESIGN CHALLENGE NOW BECOMES THE VALIDATION OF THE STRUCTURAL PERFORMANCE IN THE COMBINED LOADING ENVIRONMENT OF THE HWB PRESSURE SHELL. THE SKIN PANELS IN THE CENTER SECTION PRESSURE SHELL MUST SIMULTANEOUSLY SUPPORT THE INTERIOR CABIN PRESSURE (NZ) AND IN-PLANE LOADS IN BOTH DIRECTIONS (NX AND NY). TO MEET THIS REQUIREMENT, STIFFENING ELEMENTS MUST HAVE CONTINUOUS LOAD PATHS WIT |