FedTALLY

Award search

Awards for “boeing

25 awards on this page · sorted by amount · page 243

Federal prime contract awards for boeing
Award IDRecipientAwarding agencyAmountStartEndNAICSDescription
FA920006C0215THE BOEING COMPANYDepartment of Defense$2.04M
2006-07-272009-05-27333319
F3460195C0478THE BOEING COMPANYDepartment of Defense$2.03M
1997-05-092007-12-31336419199708!5700!0380!GD30 !OKLAHOMA CITY ALC/LAD !F3460195C0478 !A!*!P00044 !19970509!19970630!009256819!009256819!009256819!N!81205!BOEING COMPANY, THE INC !7755 E MARGINAL WAY S !SEATTLE !WA!98108!63000!033!53!SEATTLE !KING !WASHINGTON!0001!-000000075201!N!N!000000000000!R414!SYSTEMS ENGINEERING SERVICES !S1 !SERVICES !3CMS!AGM-69 SRAM(SHT RG ATTK MSL) !3724!3!*!*!C!B!N!B!D !U!Y!1!001!N!1G!Z!Y!Z!* !* !N!C!*!A!A!A!A!A!*!* !*!N!A!B!N!*!*!*!*!*!
0026THE BOEING COMPANYDepartment of Defense$2.03M
2006-01-242010-11-02200604!294737!1700!N00019!NAVAL AIR SYSTEMS COMMAND !N0001903G0041 !A!N! !N!0026 ! !20060124!20061231!006265946!006265946!009256819!N!MCDONNELL DOUGLAS CORPORATION,!6200 MCDONNELL BLVD !SAINT LOUIS !MO!63166!12300!049!37!CHERRY POINT MCAS !CRAVEN !N CAROLINA!+000002310229!N!N!000000000000!K015!MODIFICATION OF EQ/AIRCRAFT STRUCTURAL COMPS !A1A!AIRFRAMES AND SPARES !530 !AV-8B REMANUFACTURE !336411!E! !4! ! ! ! ! !99990909!B! ! !A! !D!U!J!1!001!N!1A!C!Y!Z! ! !N!C!N! ! ! !A!A!A!A!000!A!C!N! ! ! !Y!1719!N00019!0001! !
1002THE BOEING COMPANYDepartment of Defense$2.03M
2015-04-092016-01-30336413IGF::OT::IGF NON-RECURRING ENGINEERING DELIVERY ORDER FOR GR9 WING GROUND VIBRATION TEST
0007BELL BOEING JOINT PROJECT OFFICEDepartment of Defense$2.03M
2005-10-202011-03-31336413CV OTPS PRODUCTION
7071THE BOEING COMPANYDepartment of Defense$2.03M
2016-05-192020-10-31336413NAVY AVIATION
0005THE BOEING COMPANYDepartment of Defense$2.03M
2015-08-242016-04-29336413DIGITIZATION OF MASTER TOOLS
0007THE BOEING COMPANYDepartment of Defense$2.03M
2012-03-152015-12-31332993IAF SDB F-16 INTEGRATION
RJ16THE BOEING COMPANYDepartment of Defense$2.02M
2004-08-312010-12-31541330200411!000202!5700!GJ60 !WARNER ROBINS ALC/LFK !F3365701D0026 !A!N! !N!RJ16 ! !20040831!20060831!149879157!006265946!009256819!N!MCDONNELL DOUGLAS CORPORATION !J S MCDONNELL BLVD !SAINT LOUIS !MO!63166!65000!510!29!ST. LOUIS !ST. LOUIS (CITY) !MISSOURI !+000002205530!N!N!000000000000!R414!SYSTEMS ENGINEERING SERVICES !A1A!AIRFRAMES AND SPARES !000 !* !541330!E! !5!B!S! ! !C!20170531!B! ! !N!Z!D!N!U!1!001!N!1G!Z!Y!Z! ! !N!C!N! ! ! !A!A!A!A!000!A!C!N! ! ! ! ! ! !0001! !
SPE4AX19F3351THE BOEING COMPANYDepartment of Defense$2.02M
2019-05-012020-06-303364138506500090!200092357 FY19 BOEING PREDICT
N0001920F0740BELL BOEING JOINT PROJECT OFFICEDepartment of Defense$2.02M
2020-04-012021-03-15336413FOT&E CV-22 FLIGHT TEST&MODIFICATION
HR001117C0016THE BOEING COMPANYDepartment of Defense$2.02M
2016-11-132020-04-17541712IGF::OT::IGF SIGNAL PROCESSING AT RF (SPAR) - DARPA SEEKS TO TRANSFORM RADIO FREQUENCY (RF) SYSTEMS BY DEVELOPING RF ANALOG SIGNAL PROCESSING AND NONRECIPROCAL TECHNOLOGIES THAT PERFORM UNPRECEDENTED LEVELS OF IN-BAND INTERFERENCE SUPPRESSION. THE SIGNAL PROCESSING AT RF (SPAR) TECHNOLOGY AIMS TO MITIGATE BOTH SELF AND EXTERNALLY GENERATED INTERFERING SIGNALS OF KNOWN AND UNKNOWN CHARACTERISTICS. THE GOAL OF SPAR IS TO DEMONSTRATE NOVEL IN-BAND SIGNAL INTERFERENCE MITIGATION TECHNOLOGIES USING ANALOG SIGNAL PROCESSING TECHNIQUES AS WELL AS NOVEL CHIP-SCALE CIRCULATOR APPROACHES.
N0001919F4057THE BOEING COMPANYDepartment of Defense$2.02M
2019-05-102019-12-31336411SLM ENABLED AT LEMOORE SEAL A/C 3-15
HQ086020C6052THE BOEING COMPANYDepartment of Defense$2.02M
2019-12-202023-12-29541715RESEARCH AND DEVELOPMENT
05UJTHE BOEING COMPANYDepartment of Defense$2.02M
2015-05-082017-08-153364138502086539!HEAD,ROTARY RUDDER
N0001919F0014THE BOEING COMPANYDepartment of Defense$2.02M
2018-10-232020-09-30541512P-8A SYSTEM PRODUCTION CHANGES
0003BELL BOEING JOINT PROJECT OFFICEDepartment of Defense$2.02M
2007-04-172009-02-01541330NON-RECURRING ENGINEERING FOR ECP-0721
NNL09AD50TTHE BOEING COMPANYNational Aeronautics and Space Administration$2.02M
2009-09-292010-08-31541710X48B LOW SPEED FLIGHT CONTROLS VALIDATION
0002ARGON ST, INC.Department of Defense$2.02M
2012-01-102016-08-01541330SPARES FOR AN/SLQ-25A (FMS) CN-P-DAL
80GRC019C0004THE BOEING COMPANYNational Aeronautics and Space Administration$2.02M
2019-05-292023-01-31541715RISK REDUCTION TEST - CONTACT CO FOR FURTHER DESCRIPTION, IF NEEDED.
SPE4A526F4380THE BOEING COMPANYDepartment of Defense$2.01M
2026-02-242028-10-313364138511936903!VALVE ASSEMBLY,MANI
SPRRA123F0260THE BOEING COMPANYDepartment of Defense$2.01M
2023-09-152026-07-30334511SPARES
DTFAWA10D00019CALL0020BOEING AEROSPACE OPERATIONS, INC.Department of Transportation$2.01M
2013-09-192016-09-30541330THIS TASK CONSISTS OF 3 PHASES AND EACH PHASE HAS MULTIPLE SUB TASKS. IN PHASE I, THE CONTRACTOR MUST DEVELOP QUANTIFIABLE CRITERIA TO DESCRIBE THE TERM 'STALL DEPARTURE' AND ASSESS A STATE-OF-THE-ART RESEARCH SIMULATION MODEL FOR ITS CAPABILITY TO MODEL THESE CRITERIA. IN PHASE II, THE CONTRACTOR MUST MAP THE STALL DEPARTURE CHARACTERISTICS DOCUMENTED IN DELIVERABLE D1-2 TO SPECIFIC SIMULATION MODEL TABLES AND EQUATIONS AND DEVELOP A COST ESTIMATE OF EXTENDING THE PARAMETERS OF PRIMARY IMPORTANCE TO SIMULATIONS OF OTHER AIRPLANE MODELS. IN PHASE III, THE CONTRACTOR MUST COMPLETE THE OVERALL RESEARCH PROJECT BY DEMONSTRATING THE CAPABILITY TO SUCCESSFULLY EXTEND THE EXISTING ENHANCED UPSET RECOVERY SIMULATION (EURS) MODEL TO A DIFFERENT AIRPLANE SIMULATION. TAS::69 8108::TAS IGF::OT::IGF IGF::OT::IGF
NNL10AD09TTHE BOEING COMPANYNational Aeronautics and Space Administration$2.01M
2010-09-282011-09-27541712TAS::80 0123::TAS RECOVERY ACT FUNDS RECOVERY - SMAAART TASK TITLE: COMPOSITE CRYOTANK TECHNOLOGIES AND DEMONSTRATION DESIGN, ANALYSIS, AND TESTING FOR COMPOSITE LH2 CRYOTANKS 1.0 BACKGROUND NASA IS EXPLORING ADVANCED COMPOSITE MATERIALS AND PROCESSES TO REDUCE THE OVERALL COST AND WEIGHT OF LIQUID HYDROGEN (LH2) CRYOTANKS. COMPOSITES ARE MATERIALS THAT ARE COMBINATIONS OF TWO OR MORE ORGANIC OR INORGANIC COMPONENTS. ONE MATERIAL SERVES AS A "MATRIX," WHICH IS THE MATERIAL THAT HOLDS EVERYTHING TOGETHER, WHILE THE OTHER MATERIAL SERVES AS REINFORCEMENT, IN THE FORM OF FIBERS EMBEDDED IN THE MATRIX. A CRYOTANK IS A CONTAINER THAT CAN STORE VERY COLD LIQUIDS, IN THIS CASE LIQUID HYDROGEN. THE ULTIMATE GOAL OF THIS PROJECT IS TO PROVIDE NEW AND INNOVATIVE CRYOTANK TECHNOLOGIES THAT ENABLE HUMAN SPACE EXPLORATION TO DESTINATIONS BEYOND LOW EARTH ORBIT SUCH AS THE MOON, NEAR-EARTH ASTEROIDS, AND MARS. THE FOCUS OF THIS INITIAL 1-YEAR EFFORT IS TO RESEARCH AND DEVELOP THE COMPOSITE CRYOTANK TECHNOLOGIES REQUIRED FOR A HEAVY LIFT LAUNCH VEHICLE (SIMILAR TO THE SATURN V ROCKET USED TO LAUNCH APOLLO MISSIONS) BETWEEN 8.4 METERS AND 10.0 METERS IN DIAMETER. THIS TECHNOLOGY WILL SERVE MULTIPLE CUSTOMERS INCLUDING NASA, THE DEPARTMENT OF DEFENSE (DOD), AND COMMERCIAL AEROSPACE COMPANIES. FUTURE SPIN-OFF CAPABILITIES MAY INCLUDE LH2 CORE STAGES (1ST AND TYPICALLY LARGEST SECTION OF A ROCKET), IN-SPACE PROPULSION SYSTEMS (A PROPULSION SYSTEM IS A MACHINE THAT PRODUCES THRUST TO PUSH AN OBJECT FORWARD), ON-ORBIT PROPELLANT DEPOTS (A CACHE OF PROPELLANT THAT IS PLACED ON AN ORBIT ABOUT THE EARTH OR ANOTHER BODY TO ALLOW SPACECRAFT TO BE FUELLED IN SPACE), AND LIQUID OXYGEN (LOX) CRYOTANKS. OVER THE PAST 15 YEARS, THERE HAVE BEEN A VARIETY OF COMPOSITE CRYOGENIC TANK PROGRAMS AT NASA AND THE AIR FORCE. EACH OF THESE PROJECTS HAS HAD SOME SUCCESS BUT THERE HAVE ALSO BEEN TECHNOLOGY CHALLENGES THAT HAVE MADE NASA RELUCTANT TO INCORPORATE THEM. ONE OF THE GREATEST CHALLENGES THAT NASA FACES WHEN INCORPORATING ANY ADVANCED TECHNOLOGY IS BRIDGING THE MID TECHNICAL READINESS LEVEL (TRL AS DEFINED BY HTTP://ESTO.NASA.GOV/FILES/TRL_DEFINITIONS.PDF) GAP BETWEEN EARLY DEVELOPMENT AND INCORPORATION INTO FLIGHT VEHICLES (ROCKETS). THE INTENT OF THIS CONTRACT EFFORT IS TO PUSH THE TECHNICAL MATURITY OF COMPOSITE TANKS FURTHER BY BUILDING ON THE DEVELOPMENTS OF RECENT PROGRAMS. NASAS MOST RECENT COMPOSITE CRYOTANK WAS DEVELOPED UNDER THE NEXT GENERATION LAUNCH TECHNOLOGY (NGLT) PROJECT. THE COMPOSITE CRYOTANK TECHNOLOGIES AND DEMONSTRATION (CCTD) ALSO HAS THE OPPORTUNITY TO BUILD ON NEW IMPROVEMENTS DEVELOPED BY COMMERCIAL AEROSPACE INTERNAL RESEARCH AND DEVELOPMENT (IR&D) ACTIVITIES AS WELL AS LEVERAGING TECHNOLOGY INVESTMENTS OF INTERNATIONAL AND ACADEMIC PARTNERS, AND OTHER GOVERNMENT AGENCIES. BUILDING ON PAST COMPOSITE CRYOTANK SUCCESSES AND EVALUATING NEW STATE OF THE ART MATERIALS THROUGH EQUIVALENCY TESTING SHOULD ALLOW NASA TO REALIZE CONSIDERABLE MASS AND COST SAVINGS. IN FISCAL YEAR 2011, NASA PLANS TO BEGIN A PROGRAM THAT FOCUSES ON INNOVATIVE IDEAS ENABLING NEW CAPABILITIES OR RADICALLY ALTERING OUR CURRENT APPROACHES TO SPACE SYSTEMS. GAME CHANGING DEVELOPMENT PROJECTS (GCDP) ARE INTENDED TO BE CAPABILITY-ORIENTED AND DIFFER FROM TRADITIONAL RESEARCH AND DEVELOPMENT METHODS THAT ADVANCE DISCIPLINE OR CORE KNOWLEDGE. THE GOAL OF THE PLANNED GCDP IS TO MATURE TECHNOLOGIES IN PREPARATION FOR POTENTIAL SYSTEM LEVEL FLIGHT DEMONSTRATIONS THROUGH SIGNIFICANT GROUND-BASED TESTING AND/OR LABORATORY EXPERIMENTATION. NASA WILL MANAGE THE COMPOSITE CRYOTANK TECHNOLOGIES AND DEMONSTRATION PROJECT WITHIN THESE GUIDELINES. THE CCTD PROJECT WILL BE SPLIT INTO TWO PHASES. THE CURRENT EFFORT DESCRIBED IN THIS SOW IS PHASE 1. THE SUCCESSFUL COMPLETION OF PHASE 1 COULD RESULT IN NASA ISSUING A SEPARATE 2-YEAR CONTRACT FOR PHASE 2 IF FUNDS ARE AVAILABLE. PHASE 2 WILL LIKELY INVOLVE THE CRITICAL DESIGN, ANALYSIS, AND MANUFA
SPE4A526F3611THE BOEING COMPANYDepartment of Defense$2.01M
2026-01-262027-02-283345118511877302!NUT,SELF-LOCKING,PL