FedTALLY

Award search

Awards for “boeing

25 awards on this page · sorted by amount · page 325

Federal prime contract awards for boeing
Award IDRecipientAwarding agencyAmountStartEndNAICSDescription
FA810717F0012THE BOEING COMPANYDepartment of Defense$1.02M
2017-09-202020-06-30336411IGF::OT::IGF B-52 ENGINEERING SERVICES
0021THE BOEING COMPANYDepartment of Defense$1.02M
2006-09-272009-12-31541710200612!000955!5700!FA9451!DET 8 AFRL/PKD !F2960100D0169 !A!N! !Y!0021 ! !20060927!20071231!965427164!965427164!009256819!N!BOEING LTS INC !6200 UPTOWN BLVD !ALBUQUERQUE !NM!87110!02000!001!35!ALBUQUERQUE !BERNALILLO !NEW MEXICO!+000000440000!N!N!000000000000!AC53!RDTE/WEAPONS-ADV TECH DEV !A1A!AIRFRAMES AND SPARES !000 !NOT DISCERNABLE !541990!E! !5!B!S! ! ! !99990909!B! ! !A! !A!N!U!2!001!B! !Z!N!Z! ! !N!C!N! ! ! !Z!Z!A!A!000!A!B!N! ! ! ! ! ! !0001! !
S1110A18F0045THE BOEING COMPANYDepartment of Defense$1.02M
2017-12-062019-08-30336411F/A-18 A-D AND E/F MODIFICATIONS
0006THE BOEING COMPANYDepartment of Defense$1.02M
2011-02-072012-01-31336411FY10 ECP 6318 A2 KITS
CA0503THE BOEING COMPANYDepartment of Transportation$1.02M
2009-10-062011-11-30541690AWARD OF TASK ORDER NO. CA 3503 ENTITLED "NEXTGEN TECHNOLOGY SUPPORT".
N0001414C0170THE BOEING COMPANYDepartment of Defense$1.02M
2014-09-122017-09-11541712LONG RANGE BROAD AGENCY ANNOUNCEMENT (BAA) FOR NAVY AND MARINE CORPS SCIENCE AND TECHNOLOGY
FA810512C0001BOEING AEROSPACE OPERATIONS, INC.Department of Defense$1.02M
2012-04-052013-11-08336413CONTROL COLUMN ACTUATED BRAKE (CCAB) KIT PURCHASE AND INSTALLATION FOR THE REPUBLIC OF SINGAPORE AIR FORCE (RSAF) AND KIT PURCHASE ONLY FOR THE FRENCH AIR FORCE (FAF).
0014THE BOEING COMPANYDepartment of Defense$1.02M
2010-01-202012-08-29541712AVIATR
24FTTHE BOEING COMPANYDepartment of Defense$1.02M
2017-07-282018-10-313364138504595884!PARTS KIT,FUSELAGE
N0001920F0453THE BOEING COMPANYDepartment of Defense$1.02M
2019-12-162021-12-31541330THE PURPOSE OF THIS TASK ORDER IS PROCURE TESTING AND ANALYSIS IN SUPPORT OF INTEGRATION OF ADM-160D MINIATURE AIR LAUNCHED DECOY/JAMMER (MALD-N) ON F/A-18E/F AND EA-18G AIRCRAFT.
FA813420F5405BOEING AEROSPACE OPERATIONS, INC.Department of Defense$1.02M
2020-07-012022-06-04488190CONTRACTOR LOGISTICS SUPPORT FOR THE C-32/C-40 AIRCRAFT FLEET.
SPRPA119FMQ15THE BOEING COMPANYDepartment of Defense$1.02M
2018-12-212020-08-27336413SLAT BOX SUB ASSEMB
0109THE BOEING COMPANY (0674)Department of Defense$1.02M
2008-10-272009-09-30336411T-38C CCP 109 FY09 DAMAGED EQUIPMENT
0098THE BOEING COMPANY (0674)Department of Defense$1.02M
2008-09-292010-09-30336413MP-08/BIG TAC.INF FILE
0003THE BOEING COMPANYDepartment of Defense$1.02M
2015-05-122016-03-30336413P-8 MISSION SYSTEMS COMPONENTS
FA860925FB007THE BOEING COMPANYDepartment of Defense$1.02M
2025-07-152026-07-15336411JAPAN FMS AIRCRAFT VH405 AND VH406 DEPOT AND DELIVERY CONFIGURATION
S1110A19F0029THE BOEING COMPANYDepartment of Defense$1.02M
2019-03-122021-09-30336411F/A-18 E/F MODIFICATIONS
NNL13AC08TTHE BOEING COMPANYNational Aeronautics and Space Administration$1.02M
2013-08-082016-10-12541712IGF::OT::IGF TASK ORDER - STATEMENT OF WORK (SOW) TASK TITLE: BOEING LCAT ARC JET TEST IN SUPPORT OF FLEXIBLE TPS EVALUATION AND DEVELOPMENT 1.0 INTRODUCTION / BACKGROUND: THE HYPERSONIC INFLATABLE AERODYNAMIC DECELERATOR (HIAD) PROJECT IS A TECHNOLOGY DEVELOPMENT EFFORT INVESTIGATING THE VIABILITY AND SURVIVABILITY OF INFLATABLE AERODYNAMIC DECELERATORS AT FLIGHT RELEVANT ENVIRONMENTS FOR APPLICATION TO FUTURE PLANETARY ENTRY SPACECRAFT. IN ORDER TO EVALUATE A FLEXIBLE THERMAL PROTECTION SYSTEMS (FTPS), WHICH IS THE HEAT SHIELD FOR THE HIAD, THE FTPS MUST BE SUBJECTED TO FLIGHT-RELEVANT HEATING, PRESSURES, AND SHEARING ENVIRONMENTS EXPERIENCED DURING REENTRY, AND SHOW MARGINED PERFORMANCE AND SURVIVAL. IN SUPPORT OF THE HIAD PROJECTS FLEXIBLE SYSTEMS TECHNICAL DEVELOPMENT AREA, THE NASA LANGLEY RESEARCH CENTER (LARC) ENGINEERING GROUP IS MODELING, TESTING, AND VERIFYING MODELING OF FTPS LAYUPS IN FLIGHT RELEVANT REACTIVE FLOW ENVIRONMENTS IN ORDER TO ESTABLISH A MODELING PARADIGM AND A MORE EFFECTIVE MARGIN POLICY FOR INFLATABLE AND RIGID REENTRY SYSTEMS. SPECIFIC NASA PROVIDED SPECIMENS, (MADE UP OF VARIOUS LAYUP COMBINATIONS OF ADVANCED FLEXIBLE MATERIALS) ARE MODELED AND TESTED IN FLIGHT RELEVANT CONDITIONS FOR MODEL VERIFICATION AND MARGIN MATURATION. THIS EFFORT BUILDS UPON TESTING ALREADY CONDUCTED AT THE LCAT UNDER BOEINGS SMAAART CONTRACT NNL10AA05B, TASK ORDER NNL11AD16T, ENTITLED BOEING LCAT ARC-JET TEST IN SUPPORT OF FLEXIBLE TPS EVALUATION AND DEVELOPMENT. UNDER NNL11AD16T, HUNDREDS OF FTPS SAMPLES HAVE BEEN EVALUATED AT SEVERAL CONDITIONS OF DEVELOPMENT INTEREST, ESTABLISHING A BASIS FOR THE CRITICAL ADVANCEMENT OF THE SUCCESSFUL FLIGHT OF THE INFLATABLE REENTRY VEHICLE EXPERIMENT (IRVE)-3 IN JULY 2012 AND ADVANCING THE DEVELOPMENT OF THE NEXT GENERATION OF FTPS. THE TESTING DESCRIBED BY THIS SOW WILL CONTINUE THIS CRUCIAL ADVANCEMENT BY BUILDING UPON THE DATABASE OF RESULTS ALREADY OBTAINED. FURTHER TESTING IS NEEDED TO COMPARE MORE ADVANCED MATERIALS AND LAYUPS WITH PREVIOUSLY TESTED COUPONS AND TO EXTEND THE HEAT FLUX AND PRESSURE TEST RANGE, SIMULATING HARSHER ATMOSPHERIC REENTRY FLIGHT ENVIRONMENTS. 2.0 SCOPE&OBJECTIVE(S): THE SCOPE OF THIS TASK ORDER IS TO EVALUATE FTPS LAYUPS AND MATERIALS AT COMPARABLE OR HARSHER SIMULATED ATMOSPHERIC REENTRY FLIGHT CONDITIONS AND RIGID DEPLOYABLE TPS LAYUPS AND MATERIALS AT MUCH HARSHER SIMULATED ATMOSPHERIC REENTRY FLIGHT CONDITIONS. FTPS MATERIALS AND SYSTEMS WILL BE TESTED UTILIZING THE LCAT FACILITY FOR 12 WEEKS OF TOTAL TEST TIME AT FOUR SPECIFIC TEST CONDITIONS WHICH SIMULATE RELEVANT TEST ENVIRONMENTS. THE FIRST TWO TEST CONDITIONS, GIVEN IN OBJECTIVES 1 AND 2 BELOW, WERE DEVELOPED UNDER TASK ORDER NNL11AD16T. NEW MATERIALS AND SYSTEMS WILL BE COMPARED AT THESE CONDITIONS. THE REMAINING TWO TEST CONDITIONS ARE NEW TEST REQUIREMENTS OUTLINED IN OBJECTIVES 3 AND 4 BELOW TO EXTEND THE RANGE OF THE CURRENT MATERIALS AND SYSTEMS DATA BASE. THE OBJECTIVES FOR THIS TASK ORDER ARE AS FOLLOWS: OBJECTIVE ONE: EVALUATION OF FTPS LAYUPS AND MATERIALS AT FLIGHT-LIKE CONDITIONS SIMULATING A HEAT FLUX ENTRY CONDITION (SQUARE PULSE OR MISSION PROFILE IN STAGNATION OR SHEAR) OF<50 W/CM2 (HEAT FLUX BETWEEN ~17 AND<50 W/CM2, PRESSURE BETWEEN ~1.7 AND ~10KPA). OBJECTIVE TWO: EVALUATION OF FTPS LAYUPS AND MATERIALS AT FLIGHT-LIKE CONDITIONS SIMULATING A HEAT FLUX ENTRY CONDITION (SQUARE PULSE OR MISSION PROFILE IN STAGNATION OR SHEAR) OF ~50 W/CM2 (HEAT FLUX ~50 W/CM2, PRESSURE ~6KPA). OBJECTIVE THREE: EVALUATION OF FTPS LAYUPS AND MATERIALS AT FLIGHT-LIKE CONDITIONS SIMULATING A HEAT FLUX ENTRY CONDITION (SQUARE PULSE OR MISSION PROFILE IN STAGNATION OR SHEAR) OF ~75 W/CM2 (HEAT FLUX ~75W/CM2, PRESSURE ~10KPA). OBJECTIVE FOUR: EVALUATION OF FTPS LAYUPS AND MATERIALS AT FLIGHT-LIKE CONDITIONS SIMULATING A HEAT FLUX ENTRY CONDITION (SQUARE PULSE IN STAGNATION) OF ~130 W/CM2 (HEAT FLUX ~130 W/CM2, PRESSURE BETWEEN ~6 AND ~12K
0088THE BOEING COMPANYDepartment of Defense$1.02M
2012-09-272014-08-30336413300 CONTROL ASSEMBLY
0004THE BOEING COMPANYDepartment of Defense$1.02M
2010-05-062012-11-14541712VAATE II/III: BOEING
80KSC018F0219THE BOEING COMPANYNational Aeronautics and Space Administration$1.02M
2018-08-242019-01-31336414THE COMMERCIAL CREW PROGRAM (CCP) COMMERCIAL CREW TRANSPORTATION CAPABILITY (CCTCAP) CONTRACT WILL PROVIDE COMPLETION OF THE DESIGN, DEVELOPMENT, TEST, EVALUATION, AND CERTIFICATION OF AN INTEGRATED CREW TRANSPORTATION SYSTEM (CTS) CAPABLE OF TRANSPORTING NASA CREW TO AND FROM THE ISS, IN ACCORDANCE WITH THE DESIGN REFERENCE MISSIONS AND NASA S CERTIFICATION STANDARDS AND REQUIREMENTS. CERTIFICATION OF THE CTS WILL BE DETERMINED BY NASA. NASA PLANS TO ISSUE TASK ORDERS FOR POST CERTIFICATION MISSIONS (PCM) TO AND FROM ISS THAT INCLUDE GROUND, LAUNCH, LIFEBOAT, ON-ORBIT, RETURN AND RECOVERY OPERATIONS. THE MINIMUM QUANTITY OF MISSIONS TO BE ORDERED IS TWO (2) AND THE MAXIMUM POTENTIAL QUANTITY OF MISSIONS WHICH MAY BE ORDERED IS SIX (6). IN ADDITION, NASA MAY ISSUE TASK ORDERS FOR SPECIAL STUDIES USED FOR RISK REDUCTION AND OTHER PURPOSES RELATED TO THE CTS. NASA CERTIFICATION UNDER CLIN 001 IS COMPLETE WHEN THE CONTRACTOR S CREW TRANSPORTATION SYSTEM (CTS) HAS MET NASA S REQUIREMENTS FOR SAFELY TRANSPORTING CREW TO AND FROM THE INTERNATIONAL SPACE STATION (ISS) IN ACCORDANCE WITH DOCUMENTS IDENTIFIED IN SECTION C.1, SPECIFICATIONS/STATEMENT OF WORK. SUBCLINS 001A AND 001B, IDENTIFIED IN TABLE B.3, DDTE/CERTIFICATION SUBCLINS, ARE DELIVERY MILESTONES THAT REPRESENT COMPLETION OF REQUIRED WORK NECESSARY TO ACHIEVE NASA CERTIFICATION. DELIVERY PAYMENT FOR THE ISS DESIGN CERTIFICATION REVIEW (DCR) FOR THE CREWED FLIGHT TO THE ISS INCLUDES ALL WORK UNDER THIS CLIN THAT OCCURS FROM THE CONTRACT EFFECTIVE DATE THROUGH THE ISS DCR COMPLETION. THE DELIVERY PAYMENT FOR THE CERTIFICATION REVIEW (CR) WILL INCLUDE ALL WORK THAT OCCURS FROMTHE ISS DCR DELIVERY DATE THROUGH THE END OF THE DDTE/CERTIFICATION CLIN 001. IN ACCORDANCE WITH CLAUSE C.1, SPECIFICATION/STATEMENT OF WORK, THE TASK ORDERING PROCEDURES AND OTHER TERMS AND CONDITIONS IN THE CONTRACT, THE CONTRACTING OFFICER MAY ISSUE POST CERTIFICATION MISSION (PCM) TASK ORDERS. THE CONTRACTOR SHALL USE THE MISSION PRICING RATES SHOWN IN TABLE B.4.1, POST CERTIFICATION MISSION PRICES. THE PER MISSION PRICES ARE FOR A SINGLE ORDER AT THE PRICE STATED PER THE CALENDAR YEAR (CY) BASED ON THE NUMBER OF MISSIONS ORDERED. CTS FULL MISSION CAPABILITY PRICES SHALL BE BASED ON (1) FULFILLMENT OF THE DESIGN REFERENCE MISSION TO THE ISS FOUND IN CCT-DRM-1110, CREW TRANSPORTATION SYSTEM DESIGN REFERENCE MISSIONS, ATTACHMENT J-03, CONTRACT PERFORMANCE WORK STATEMENT, AND OTHER TERMS AND CONDITIONS IN THE CONTRACT AND (2) ALL INHERENT CTS CAPABILITIES THAT ARE WITHIN THE PROPOSED MISSION PRICES. IN ACCORDANCE WITH ATTACHMENT J-03, CONTRACT PERFORMANCE WORK STATEMENT, THE TASK ORDERING PROCEDURES AND OTHER TERMS AND CONDITIONS IN THE CONTRACT, THE CONTRACTOR SHALL PERFORM SPECIAL STUDIES, TEST AND ANALYSES, AS INITIATED BY WRITTEN DIRECTION FROM THE CONTRACTING OFFICER.
FA865614C0113THE BOEING COMPANYDepartment of Defense$1.02M
2014-07-172015-11-20541712IGF::OT::IGF INTEGRATED PRECISION ORDINANCE SYSTEM
0067THE BOEING COMPANYDepartment of Defense$1.02M
2014-05-222014-08-044881905C CHECK
0012THE BOEING COMPANYDepartment of Defense$1.02M
2014-01-232016-01-22336411IGF::OT::IGF FY14 MATERIAL IMPROVEMENT PROJECTS (MIP) INSTALLATION LABOR FOR MLG DOOR LINK CORROSION AND AFT FILLET PANEL DRAINAGE PROJECTS AND MATERIAL FOR MLG DOOR LINK CORROSION PROJECT FOR FY14 AND FY15
FA810718F0014THE BOEING COMPANYDepartment of Defense$1.02M
2018-04-202019-04-19336411B-52 ENGINEERING SERVICE