FedTALLY

Awards for “honeywell

25 awards on this page · sorted by amount · page 102

Award IDRecipientAwarding agencyAmountStartEndNAICSDescription
80AFRC19C0012HONEYWELL INTERNATIONAL INC.National Aeronautics and Space Administration$868.7K
2019-06-212021-10-31336413EIGHT (8) PANEL MOUNTED BREATHER REGULATORS (VALVE, OXYGEN MASK, AIRCRAFT), PART NUMBER SPC-77301418-0001, DRAFT 2A
SPE4A521F3251HONEYWELL INTERNATIONAL INC.Department of Defense$868.43K
2020-12-142023-02-213364138507851503!TRANSFORMER,POWER
N0038324FV61XHONEYWELL INTERNATIONAL INC.Department of Defense$868.4K
2024-08-072025-10-25336413VALVE ASSEMBLY,ENVI
1320HONEYWELL INTERNATIONAL INC.Department of Defense$868.34K
2016-10-192018-12-173336128503763148!BOOT ASSEMBLY,BALLS
HSCG3810JA70801HONEYWELL INTERNATIONAL INC.Department of Homeland Security$868.26K
2009-11-192010-05-29336411OVERHAUL OF ATF 3-6 ENGINE
SPRPA118FKQ1GHONEYWELL INTERNATIONAL INC.Department of Defense$868.02K
2018-06-132019-05-29336413ATTITUDE HEADING,RE
QP38HONEYWELL INTERNATIONAL INC.Department of Defense$867.17K
2013-04-242014-09-30336413DELIVERY ORDER AGAINST HONEYWELL LONG TERM CONTRACT TO PURCHASE 49 HEAT STACK ASSEMBLY AND 278 DRIVE KEYS.
N0001920F0373HONEYWELL INTERNATIONAL INC.Department of Defense$867.14K
2019-10-252022-02-2833451125 LOT 16 DOMESTIC REFURB EGIS AND 6 PRODUCTION LINE ASSETS FOR BAHRAIN
SPE4A521F9183GRIMES AEROSPACE COMPANYDepartment of Defense$866K
2021-04-202022-07-183364138508150111!LIGHT,LANDING,AIRCR
SPRPA111CY022GRIMES AEROSPACE COMPANYDepartment of Defense$865.28K
2011-02-012011-05-02336413CONTROLLABLE SEARCH
SPRTA116F0325HONEYWELL INTERNATIONAL INC.Department of Defense$865.24K
2016-09-202016-10-31333612BUTTERFLY VALVE
SPRPA121F0KQ1HONEYWELL INTERNATIONAL INC.Department of Defense$865.23K
2021-04-302024-03-203364135841010874423
0438HONEYWELL INTERNATIONAL INC.Department of Defense$865.16K
2013-03-132014-07-31336413IGF::CT::IGF REGULATOR, AIR PRESSURE ON THE F-16; BODY, VALVE ON THE C-5; VALVE, BUTTERFLY ON THE C-130 AND F-15; VALVE, REGULATING ON THE A-10; VALVE ON THE F-15; STARTER ON THE C-130; VALVE, ASSEMBLY ON THE KC-135
UN09HONEYWELL INTERNATIONAL INC.Department of Defense$864.58K
2011-03-252011-12-30333999OTHER AIRCRAFT PART AND AUXILIARY EQUIPMENT MANUFACTURING
XP14HONEYWELL INTERNATIONAL INC.Department of Defense$864.32K
2015-09-282017-08-20334511END ITEM/PLATFORM:UH-60, CH-47, APACHE BLOCK III AND AH64D NSN: 6605-01-513-5946 PART NUMBER: HG9873P02-001
0001HONEYWELL INTERNATIONAL INCDepartment of Defense$863.98K
2008-09-222009-05-14541712OTHER DEFENSE (APPLIED/EXPLORATORY)
NNL08AA23THONEYWELL INTERNATIONAL INCNational Aeronautics and Space Administration$863.59K
2007-12-212010-12-20541710NASA RESEARCH ANNOUNCEMENT (NRA) IN SOLICITATION NNH07ZEA001N. FCSR TASK ORDER TITLE: "VERIFIABLE ADAPTIVE CONTROL: ANALYSIS AND DESIGN". BACKGROUND: THIS EFFORT FALLS UNDER THE NASA INTEGRATED RESILIENT AIRCRAFT CONTROL (IRAC) PROJECT. THE GOAL OF THIS PROJECT IS TO ARRIVE AT A SET OF VALIDATED MULTIDISCIPLINARY INTEGRATED AIRCRAFT CONTROL DESIGN TOOLS AND TECHNIQUES FOR ENABLING SAFE FLIGHT IN THE PRESENCE OF ADVERSE CONDITIONS (E.G., FAULTS, DAMAGE AND/OR UPSETS). THE OBJECTIVE IS TO ADVANCE THE STATE-OF-THE-ART OF ADAPTIVE CONTROLS AS A DESIGN OPTION TO PROVIDE ENHANCED STABILITY AND MANEUVERABILITY MARGINS FOR SAFE LANDING. THE IRAC PROJECT'S TECHNICAL APPROACH IS RELATIVE TO THE FOLLOWING FOUR LEVELS OF RESEARCH DEFINED BY THE AERONAUTICS RESEARCH MISSION DIRECTORATE (ARMD). 1. FOUNDATIONAL RESEARCH (LEVEL 1) FOCUSES ON FUNDAMENTAL THEORY AND METHODS FOR THE CHARACTERIZATION OF ADVERSE CONDITIONS, THEORETICAL ADVANCES IN ADAPTIVE CONTROL, INTELLIGENT PLANNING AND GUIDANCE, AND RELEVANT CONTROL METRICS FOR MEASURING AVAILABLE STABILITY AND CONTROLLABILITY MARGINS. FUNDAMENTAL THEORY AND METHODS WILL BE DEVELOPED IN: (1) PHYSICS-BASED COMPUTATIONAL MODELING OF FLUID, STRUCTURAL, AND ENGINE DYNAMICS TO CHARACTERIZE THE EFFECTS OF ADVERSE CONDITIONS, (2) CONTROL UNDER ADVERSE CONDITIONS, (3) EXPERIMENTAL METHODS FOR TESTING UNDER THESE CONDITIONS, AND THE VALIDATION AND VERIFICATION OF ADAPTIVE AND LEARNING SYSTEMS. 2. DISCIPLINE RESEARCH (LEVEL 2) FOCUSES ON METHODS AND TOOLS THAT ARE REQUIRED FOR THE DEVELOPMENT OF INTEGRATED MODELING, CONTROL, AND RESPONSE PREDICTION METHODOLOGIES FOR ADVERSE EVENTS. THE RESEARCH DISCIPLINES INCLUDE: INTEGRATED DYNAMICS AND FLIGHT CONTROL; INTEGRATED PROPULSION CONTROLS AND DYNAMICS; AIRFRAME & STRUCTURAL DYNAMICS; INTELLIGENT FLIGHT PLANNING AND GUIDANCE; AND VERIFICATION AND VALIDATION METHODS AND TESTBEDS. 3. MULTIDISCIPLINARY RESEARCH (LEVEL 3) FOCUSES ON STABILITY, MANEUVERABILITY, AND SAFE LANDING USING FLIGHT CONTROL TO PREVENT AND/OR MANEUVER SAFELY AFTER AN ADVERSE EVENT. TO ACHIEVE THIS, INTEGRATED ADAPTIVE AIRCRAFT CONTROL FOR STABILITY AND SAFE MANEUVERABILITY, INTEGRATED ADAPTIVE MISSION MANAGEMENT TOOLS FOR SAFE FLIGHT, AND VERIFICATION AND VALIDATION OF THE INTEGRATED SYSTEM ARE IDENTIFIED AS KEY ELEMENTS. 4. SYSTEM LEVEL RESEARCH (LEVEL 4) ACTIVITIES FOCUS ON THE DEVELOPMENT OF MULTIDISCIPLINARY INTEGRATED METHODS, TOOLS, AND TECHNOLOGIES FOR ACHIEVING CONTROL RESILIENCE UNDER ADVERSE CONDITIONS AND THE VALIDATION OF INTEGRATED IRAC TECHNOLOGIES USING SIMULATION AND VEHICLE TEST BEDS, AND TECHNOLOGY REQUIREMENTS DEFINITIONS BASED ON ACCIDENT/INCIDENT ANALYSES, COMPREHENSIVE INTEGRATED TECHNOLOGY EVALUATIONS, AND PARTNERING. THIS RESEARCH EFFORT FALLS PRIMARILY UNDER FOUNDATIONAL RESEARCH AT LEVEL 1 WITH SOME LEVEL 2 WORK AND IS AN INTEGRAL RESEARCH COMPONENT OF THE OVERALL PROJECT CONTENT. IT HAS BEEN DEFINED TO CONTRIBUTE TO PRIMARY TECHNOLOGY NEEDS, ADVANCING THE STATE-OF-THE-ART IN ADAPTIVE CONTROL FOR PILOTED AIRCRAFT, AND IS ASSOCIATED WITH THE PROJECT'S APPLICATION FOCUS ON MULTIDISCIPLINARY INTEGRATED AIRCRAFT CONTROL DESIGN SYNTHESIS. THIS EFFORT ALSO INCLUDES THE DEVELOPMENT OF ADAPTIVE CONTROL METRICS AND ASSOCIATED TOOLS FOR EVALUATING ADAPTIVE CONTROL SYSTEMS. SCOPE: THIS EFFORT IS FOR THE DESIGN AND ANALYSIS OF NEW TECHNIQUES AND ALGORITHMS FOR ADAPTIVE FLIGHT CONTROL. BASED ON THE ROBUSTNESS STABILITY AND PERFORMANCE METRICS FOR ADAPTIVE SYSTEMS DEVELOPED UNDER THIS PROGRAM, THE CONTRACTOR SHALL PERFORM RIGOROUS EVALUATIONS OF ADVANCED ADAPTIVE FLIGHT CONTROL LAWS DESIGNED TO MITIGATE OFF-NOMINAL CONDITIONS AND DOCUMENT THE RESULTS IN ANNUAL TECHNICAL REPORTS. OBJECTIVES: THE OBJECTIVE OF THIS EFFORT IS TO DEVELOP SYNTHESIS AND ANALYSIS TOOLS WHICH CAN BE EFFECTIVELY USED TO DESIGN AND VERIFY ADAPTIVE CONTROL LAWS. IN ORDER TO MEET THIS GOAL, THE CONTRACTOR SHALL PERFORM RESEARCH ON THE FOLLOWING FUNDAMENTAL T
SPE4A526F0422HONEYWELL INTERNATIONAL INC.Department of Defense$862.81K
2025-12-102027-12-073364138511699218!TUBE AND BUSHING AS
SPE4A519F667LHONEYWELL INTERNATIONAL INC.Department of Defense$862.25K
2019-05-092022-12-203325108506517550!PANEL,INTERIOR LINI
0011HONEYWELL INTERNATIONAL INC.Department of Defense$862.05K
2007-09-272009-09-30336413FY 2009 - DELIVERY PRICING
SPRHA419F0016HONEYWELL INTERNATIONAL INC.Department of Defense$861.83K
2019-02-062020-03-31334511F-16 MULTIFUNCTION DISPLAY
N0038322FXP02HONEYWELL INTERNATIONAL INC.Department of Defense$861.42K
2022-05-182023-05-01336413MACHINE,AIR CYCLE
SPE4AX26F073JHONEYWELL INTERNATIONAL INC.Department of Defense$861.3K
2026-04-272028-03-293336118512069716!ROTOR,TURBINE,NONAI
SPE4A519F887PGRIMES AEROSPACE COMPANYDepartment of Defense$860.51K
2019-06-272020-09-163364138506635080!LENS AND RETAINER A
N0038318FFQ0WHONEYWELL INTERNATIONAL INC.Department of Defense$859.97K
2018-01-242024-01-13336413VALVE,REGULATING,FL