Federal Contractor Profile
Ata Engineering, INC.
$52M obligated·179 awards·3 agencies·13 NAICS
Federal Contracts
Showing contracts 151–200 of 201 total. Sorted by action date, most recent first. Excludes $0 modifications.
| Date | Agency | PIID | NAICS | Description | Amount |
|---|---|---|---|---|---|
| Sep 18, 2017 | Department of DefenseW6QK AATD CONTR OFF | W911W617C0024 | 541712 | IGF::OT::IGF ATA ENGINEERING INC. SBIR PH II ~ FULLY INTEGRATED AEROELASTIC SIMULATION OF COMPLETE VERTICAL LIFT CONFIGURATIONS | $494K |
| Sep 15, 2017 | National Aeronautics and Space AdministrationNASA SHARED SERVICES CENTER | 80NSSC17P1160 | 511210 | IGF::OT::IGF ATA ENGINEERING SOFTWARE | $4K |
| Sep 14, 2017 | National Aeronautics and Space AdministrationNASA SHARED SERVICES CENTER | 80NSSC17P1576 | 511210 | IGF::OT::IGFADVANCED FEMAP COURSE | $15K |
| Sep 12, 2017 | Department of DefenseNSWC DAHLGREN | N0017817C1307 | 541712 | IGF::OT::IGF STATUS REPORT | $130K |
| Sep 11, 2017 | Department of DefenseFA9550 AFRL AFOSR | FA955017P0017 | 541712 | IGF::OT::IGF SBIR PHASE I 9 MONTHS | $150K |
| Aug 9, 2017 | National Aeronautics and Space AdministrationNASA JOHNSON SPACE CENTER | 80JSC017F0038 | 541712 | IGF::OT::IGFNEW LEGACY TASK ORDER | $15K |
| Jul 31, 2017 | National Aeronautics and Space AdministrationNASA SHARED SERVICES CENTER | 80NSSC17P0696 | 511210 | IGF::OT::IGF SW RENEWAL - FEMAP | $64K |
| Jul 6, 2017 | Department of DefenseFA8650 USAF AFMC AFRL PZL AFRL/PZL | FA865015C2640 | 541712 | IGF::OT::IGF HASI PROGRAM | $993K |
| Jun 12, 2017 | National Aeronautics and Space AdministrationNASA ARMSTRONG FLIGHT RESEARCH CNTR | NND17AA58T | 541330 | IGF::OT::IGF CREW GROUND VIBRATION TEST CONSULTING USING EXTRACTION OF FIXED-BASE MODES FOR THE UPCOMING PASSIVE AEROELASTIC TAILORED (PAT) WING GROUND VIBRATION TEST (GVT). | $33K |
| Jun 8, 2017 | National Aeronautics and Space AdministrationNASA SHARED SERVICES CENTER | NNX17CM19P | 541712 | IGF::OT::IGF MITIGATION OF DYNAMIC COMBUSTION INSTABILITY IS ONE OF THE MOST DIFFICULT ENGINEERING CHALLENGES FACING NASA AND INDUSTRY IN THE DEVELOPMENT OF NEW CONTINUOUS-FLOW COMBUSTION SYSTEMS SUCH AS THE COMBUSTION CHAMBERS IN LIQUID-FUELED ROCKET ENGINES (LRES). COMBUSTION INSTABILITIES ARE SPONTANEOUS, SELF-SUSTAINING OSCILLATIONS THAT TIE THE COMBUSTOR ACOUSTICS TO THE COMBUSTION REACTION ITSELF. THESE OSCILLATIONS CAN LEAD TO A WIDE RANGE OF PROBLEMS FROM OFF-DESIGN PERFORMANCE TO CATASTROPHIC FAILURE. EFFORTS TO PREDICT INSTABILITIES AT DESIGN-TIME IS HINDERED BY THE COMPLEX, MULTI-PHYSICS NATURE OF THE ACOUSTICS AND CHEMISTRY, TYPICALLY REQUIRING MULTIPLE ITERATIONS OF TIME AND RESOURCE INTENSIVE SYSTEM PROTOTYPING. THE PROPOSED PHASE I STTR PROJECT AIMS TO DEVELOP A SIMULATION FRAMEWORK THAT WILL ENABLE ACCURATE, DESIGN-TIME PREDICTION OF INSTABILITIES. THIS FRAMEWORK WILL LEVERAGE THE CAPABILITIES OF LOCI/CHEM FOR MASSIVELY PARALLEL, MULTI-PHYSICS FLOW SIMULATIONS TO GENERATE LOW-ORDER, INDEPENDENT MODELS OF COMBUSTION AND ACOUSTIC RESPONSE TO PERTURBATIONS. BY SOLVING FOR SIMULTANEOUS SOLUTIONS OF THESE LOW-ORDER PERTURBATION MODELS, IT WILL BE POSSIBLE TO NUMERICALLY MAP THE ACOUSTIC MODES OF THE SYSTEM TO THEIR STABILITY CHARACTERISTICS, PROVIDING A MEANS TO PREDICT INSTABILITY. PHASE I WILL DEVELOP CRITICAL ADDITIONS TO LOCI/CHEM'S COMBUSTION MODELING CAPABILITIES, DEVELOP THE APPROPRIATE ACOUSTIC MODELS, DEVELOP A TEST PLAN FOR EXPERIMENTAL VALIDATION OF THE COMBUSTION MODEL, AND CONCLUDE WITH A PROOF-OF-CONCEPT DEMONSTRATION OF THE FULL FRAMEWORK. IN PHASE II, AN EXPERIMENTAL CAMPAIGN WILL BE CARRIED OUT TO VALIDATE THE COMBUSTION MODELING TOOLS DEVELOPED IN PHASE I AND AUGMENT THE SIMULATION FRAMEWORK WITH MULTI-PHASE MODELING APPROPRIATE FOR FULL-SCALE LRE COMBUSTION CHAMBERS. | $125K |
| May 30, 2017 | Department of DefenseFA8650 USAF AFMC AFRL PZL AFRL/PZL | FA865017P5030 | 541711 | IGF::OT::IGF A MULTIPHYSICS FRAMEWORK UTLILIZING NONLINEAR MATERIAL MODELS FOR PREDICITING IMPACT OF | $150K |
| May 19, 2017 | Department of DefenseNAVAIR WARFARE CTR AIRCRAFT DIV | N6833517C0376 | 541712 | PROGRESS REPORT IGF::OT::IGF | $130K |
| May 16, 2017 | Department of DefenseFA8650 USAF AFMC AFRL PZL AFRL/PZL | FA865016C2732 | 541712 | IGF::OT::IGF PREDICITNG NONLINEAR RESPONSE OF COMPOSITE STRUCTURES USED IN HYPERSONIC VEHICLES | $187K |
| Apr 20, 2017 | National Aeronautics and Space AdministrationNASA SHARED SERVICES CENTER | NNX17CC18C | 541712 | IGF::OT::IGF TO ALLOW AVIATION GROWTH TO CONTINUE IN THE FACE OF INCREASINGLY STRINGENT NOISE POLLUTION STANDARDS, NEW AIRCRAFT ENGINES MUST BE DESIGNED WITH NOISE PERFORMANCE AS A PRINCIPAL CONSTRAINT. TECHNOLOGIES TO REALIZE FUTURE PROPULSION NOISE REDUCTION WILL REQUIRE DETAILED EXPERIMENTAL CHARACTERIZATION AND DIAGNOSIS OF THE ACOUSTIC MECHANISMS AND SOURCES WITHIN AN ENGINE SYSTEM OR COMPONENT. ATA ENGINEERING, INC. (ATA) PROPOSES AN SBIR PROJECT TO FURTHER DEVELOP AND VALIDATE METHODS FOR OBTAINING PHASED ARRAY ACOUSTIC DATA FROM COMPLEX DISTRIBUTED NOISE SOURCES USING CONTINUOUSLY MOVING, OR CONTINUOUS-SCAN (CS) MICROPHONES IN CONJUNCTION WITH STATE-OF-THE-ART PHASE-REFERENCING TECHNIQUES. THE BENEFITS OF THE CS METHOD INCLUDE (1) EFFECTIVELY INFINITE SPATIAL RESOLUTION, AS THE SOUND FIELD CROSSSPECTRUM MAY BE DESCRIBED BETWEEN ANY TWO LOCATIONS ALONG THE SCAN TRAJECTORY, (2) PRESERVATION OF PHASE DATA FOR IMPROVED SOURCE AND PROPAGATION MODELING, INCLUDING BEAMFORMING (BF) AND ACOUSTICAL HOLOGRAPHY (AH), (3) SIGNIFICANT REDUCTION OF TEST DATA ACQUISITION TIME (POTENTIALLY TWO TO TEN TIMES FASTER) PER OPERATIONAL POINT, AND CONSEQUENTLY EITHER (4) REDUCED TEST OPERATIONAL COST, OR (5) THE OPPORTUNITY TO SCREEN MORE DESIGN CONCEPTS WITHIN A GIVEN BUDGET. THE PHASE II EFFORT WILL USE SUBSCALE AEROACOUSTIC TESTING TO VALIDATE THE NOVEL CONTINUOUS-SCAN BEAMFORMING (CSBF) MEASUREMENT TECHNIQUES WITH THE AIM OF EVENTUAL IMPLEMENTATION IN NASA ACOUSTIC WIND TUNNEL AND FREE-JET TESTING FACILITIES. ATA WILL ALSO FORMALIZE A CS SOFTWARE TOOLKIT FOR DATA PROCESSING AND VISUALIZATION AND DESIGN A FULL-SCALE ARRAY CONCEPT FOR A CANDIDATE NASA WIND TUNNEL FACILITY. | $755K |
| Apr 10, 2017 | National Aeronautics and Space AdministrationNASA SHARED SERVICES CENTER | NNX17ED65P | 541712 | IGF::OT::IGF ATA SUPPORT FOR BASE DRIVE MODAL EXTRACTION OF E-STA DATA FOLLOW-ON ANALYSIS | $5K |
| Feb 28, 2017 | National Aeronautics and Space AdministrationNASA SHARED SERVICES CENTER | NNX17EC34P | 511210 | IGF::OT::IGF 2 FEMAP (FLOATING) PERPETUAL LICENSES WITH MAINTENANCE&2 4-MONTH MAINTENANCE CONTRACTS | $24K |
| Feb 9, 2017 | Department of DefenseW6QK AATD CONTR OFF | W911W616C0010 | 541712 | IGF::CL,CT::IGF SBIR PHASE I R&D CONTRACT | $50K |
| Nov 29, 2016 | National Aeronautics and Space AdministrationNASA JOHNSON SPACE CENTER | NNJ12JB12B | 541330 | AIRCRAFT AERONAUTICS AND STRUCTURAL ENGINEERING. | $200K |
| Sep 7, 2016 | Department of DefenseNAVAIR WARFARE CTR AIRCRAFT DIV | N6833516C0427 | 541712 | SBIR PI R&D. IGF::OT::IGF | $85K |
| Sep 6, 2016 | National Aeronautics and Space AdministrationNASA ARMSTRONG FLIGHT RESEARCH CNTR | NND16AB33T | 541330 | IGF::OT::IGF X-56A GROUND SUPPORT CONSULTATION | $10K |
| Aug 29, 2016 | Department of DefenseFA8650 USAF AFMC AFRL PZL AFRL/PZL | FA865016C2732 | 541712 | IGF::OT::IGF PREDICITNG NONLINEAR RESPONSE OF COMPOSITE STRUCTURES USED IN HYPERSONIC VEHICLES | $563K |
| Aug 25, 2016 | Department of DefenseCOMMANDER | M6785416C6505 | 541712 | IGF::OT::IGF SBIR PHASE II RESEARCH AND DEVELOPMENT | $499K |
| Aug 18, 2016 | Department of DefenseNAVAIR WARFARE CTR AIRCRAFT DIV | N6833512C0330 | 541712 | RESEARCH AND DEVELOPMENT SBIR TOPIC N101-026 | $72K |
| Aug 12, 2016 | National Aeronautics and Space AdministrationNASA JOHNSON SPACE CENTER | NNJ12JB12B | 541330 | AIRCRAFT AERONAUTICS AND STRUCTURAL ENGINEERING. | $13K |
| Aug 10, 2016 | Department of DefenseFA8650 USAF AFMC AFRL PZL AFRL/PZL | FA865016M6738 | 541712 | IGF::OT::IGF SBIR I: MODELING FRAMEWORK FOR AUTOMATED AIRCRAFT ESCAPE INJURY RISK ASSESSMENT | $150K |
| Jul 30, 2016 | National Aeronautics and Space AdministrationNASA GLENN RESEARCH CENTER | NNC16VG95P | 511210 | IGF::OT::IGF PURCHASE OF ONE ADDITIONAL LICENSE AND MAINTENACE FOR SAME | $8K |
| Jul 13, 2016 | National Aeronautics and Space AdministrationNASA GLENN RESEARCH CENTER | NNC16VC75P | 511210 | IGF::OT::IGF MAINTENANCE RENEWAL OF FEMAP SOFTWARE LICENSES | $59K |
| Jul 12, 2016 | Department of DefensePAE STRATEGIC SYSTEMS PROGRAMS | N0003016C0238 | 541712 | IGF::CL::IGF QUARTERLY PROGRESS REPORTS | $750K |
| Jul 8, 2016 | National Aeronautics and Space AdministrationNASA JOHNSON SPACE CENTER | NNJ12JB12B | 541330 | AIRCRAFT AERONAUTICS AND STRUCTURAL ENGINEERING. | $11K |
| Jun 22, 2016 | National Aeronautics and Space AdministrationNASA ARMSTRONG FLIGHT RESEARCH CNTR | NND16AB33T | 541330 | IGF::OT::IGF X-56A GROUND SUPPORT CONSULTATION | $13K |
| Jun 6, 2016 | National Aeronautics and Space AdministrationNASA SHARED SERVICES CENTER | NNX16CC80P | 541712 | IGF::OT::IGF NASA'S AERONAUTICS RESEARCH MISSION DIRECTORATE HAS DECLARED ULTRA-EFFICIENT COMMERCIAL AIR VEHICLES A STRATEGIC AREA FOR DEVELOPMENT IN THE COMING DECADE. WITH NO FORESEEABLE ALTERNATIVES, ADVANCED GAS TURBINE PROPULSION WILL CONTINUE TO POWER FUTURE SUBSONIC TRANSPORT AIRCRAFT. AS A RESULT, ENGINE MANUFACTURERS ARE DEVOTING SIGNIFICANT EFFORT TO INCREASING FUEL EFFICIENCY AND PUSHING ENGINES TOWARD HIGHER FAN BYPASS RATIOS (BPRS). WITH FAN SPEED ALREADY LIMITING ALLOWABLE FAN SIZES, HIGHER BPR REQUIRES NEW, SMALLER ENGINE CORES. HOWEVER, COMPONENT EFFICIENCY TENDS TO DECREASE WITH DECREASING SIZE DUE IN PART TO ENHANCED TIP LEAKAGE AND SECONDARY FLOWS. MANY OF THE EXISTING TECHNOLOGIES DESIGNED TO MITIGATE LOSSES ASSOCIATED WITH THESE FLOW STRUCTURES HAVE ONLY BEEN INVESTIGATED IN CONVENTIONAL MACHINES, UNDER STEADY APPROXIMATIONS, AND/OR IN SINGLE COMPONENTS OR STAGES. ALSO, THEY OFTEN ADDRESS ONLY A PARTICULAR LOSS MECHANISM IN A GIVEN FLOW STRUCTURE. THE PROPOSED SBIR PROJECT INNOVATES ON EXISTING MITIGATION STRATEGIES FROM A PRACTICAL, HOLISTIC PERSPECTIVE TO GENERATE NOVEL AERODYNAMIC DEVICES TAILORED TO IMPROVE THE EFFICIENCY OF MULTI-STAGE, SMALL-CORE TURBINES WHILE ALSO ACCOUNTING FOR THEIR INHERENTLY UNSTEADY NATURE. THE PROPOSED DEVICES, INCLUDING TIP LEAKAGE CONTROL AND ENDWALL TREATMENTS FOR SECONDARY FLOW CONTROL, WILL BE DESIGNED BY ACCOUNTING FOR EACH LOSS MECHANISM IN THE TARGETED FLOW STRUCTURE AND THE DEVICE'S INFLUENCE ON THE UNSTEADY FLOW FIELD IN THE CURRENT STAGE AND UPSTREAM AND DOWNSTREAM STAGES. SUCCESSFUL DESIGNS WILL ENSURE INCREASES IN COMPONENT EFFICIENCY ALSO INCREASE ENGINE OVERALL EFFICIENCY BY AVOIDING OFFSETTING REDUCTION IN LOSS IN ONE STAGE WITH INCREASED LOSS IN ANOTHER. IN PHASE I, NUMERICAL SIMULATIONS WILL BE USED TO DEVISE AND CHARACTERIZE FEASIBLE LOSS MITIGATION TECHNOLOGIES. THIS FOUNDATIONAL WORK WILL PROVIDE JUSTIFICATION FOR COMPREHENSIVE ANALYSIS AND EXPERIMENTAL EVALUATION OF THE MOST PROMISING CONCEPTS IN PHASE II. | $125K |
| Jun 2, 2016 | National Aeronautics and Space AdministrationNASA SHARED SERVICES CENTER | NNX16CC79P | 541712 | IGF::OT::IGF ATA ENGINEERING, INC., (ATA) PROPOSES AN SBIR PROJECT TO ADVANCE THE TECHNOLOGY READINESS LEVEL (TRL) OF A METHOD FOR MEASURING PHASED ARRAY ACOUSTIC DATA FOR COMPLEX DISTRIBUTED NOISE SOURCES USING CONTINUOUSLY MOVING (REFERRED TO HERE AS CONTINUOUS-SCAN, OR CS) MICROPHONES IN CONJUNCTION WITH STATE-OF-THE-ART PHASE-REFERENCING TECHNIQUES. THE PROPOSED PROJECT AIMS TO DEVELOP TWO NOVEL MODULES TO THE EXISTING SUITE OF TOOLS FOR CS ACOUSTIC MEASUREMENTS: (1) A CONTINUOUS-SCAN BEAMFORMING (CSBF) TOOL FOR ARRAYS LOCATED IN THE MID TO FAR FIELD TO PERFORM SOURCE DIAGNOSTICS IN LOW-SNR WIND TUNNEL ENVIRONMENTS., AND (2) AN AZIMUTHAL MODAL DECOMPOSITION TOOL FOR NEAR-FIELD ARRAYS HAVING PARTIAL AZIMUTHAL COVERAGE, ENABLING ACOUSTICAL HOLOGRAPHY WITHOUT FULL SOURCE ENCLOSURE. THE FIRST MODULE WILL ENABLE SMALL-APERTURE BEAMFORMING (BF) ARRAYS TO ADOPT THE CS METHOD, RESULTING IN REDUCED MAXIMUM SIDELOBE LEVELS AND HIGHER-QUALITY BF IMAGES THAT APPROACH THE THEORETICAL LIMITS ASSOCIATED WITH THE THEORY. THE SECOND MODULE WILL ENABLE CS NEAR-FIELD ARRAYS THAT AVOID THE REQUIREMENT FOR FULL COVERAGE, GREATLY SIMPLIFYING THE ARRAY COVERAGE REQUIREMENTS AND MAKING ACOUSTICAL HOLOGRAPHY SYSTEMS MORE PRACTICAL IN TESTING FACILITIES. IN PHASE I, ATA WILL DEMONSTRATE FEASIBILITY OF THE METHODS THROUGH APPLICATION TO EXISTING ACOUSTIC MEASUREMENT DATA SETS. IN PHASE II, THE METHODS WILL BE OPTIMIZED AND RIGOROUSLY VALIDATED THROUGH EXPERIMENTS USING SMALL-SCALE TURBOFAN ENGINE MODELS. ULTIMATELY, WE WILL TRANSITION THESE METHODS TO NASA AND INDUSTRY STAKEHOLDERS FOR ADOPTION IN RELEVANT FACILITIES. | $125K |
| Jun 2, 2016 | National Aeronautics and Space AdministrationNASA SHARED SERVICES CENTER | NNX16CM45P | 541712 | IGF::OT::IGF VEHICLE REENTRY PRESENTS NUMEROUS CHALLENGES THAT MUST BE CAREFULLY ADDRESSED TO ENSURE THE SUCCESS OF CURRENT AND FUTURE SPACE EXPLORATION MISSIONS. AS THEY ENTER THE ATMOSPHERE, THESE VEHICLES ARE SUBJECTED TO EXTREME HYPERSONIC ENVIRONMENTS TYPIFIED BY LARGE STRUCTURAL LOADS, HIGH HEAT FLUXES AND TEMPERATURES, AND AN AGGRESSIVE AEROTHERMAL ENVIRONMENT WHERE NONEQUILIBRIUM DISSOCIATED GASES MAY CAUSE CHEMICAL ABLATION AT THE VEHICLE'S SURFACE. THESE HYPERSONIC FLOWS INVOLVE HIGHLY NONLINEAR FLUID-THERMAL INTERACTIONS SUCH AS VERY STRONG SHOCKS, HIGH AEROHEATING, AND SHOCK BOUNDARY LAYER INTERACTIONS. THE EXTREME ENVIRONMENTS RESULT IN NONLINEAR, COUPLED INTERACTIONS BETWEEN THE VEHICLE'S STRUCTURE AND THE ENVIRONMENT. TRADITIONALLY, DESIGNS OF REENTRY VEHICLES AND THEIR COMPONENTS HAVE BEEN ANALYZED BY DIFFERENT ENGINEERING DISCIPLINES IN AN UNCOUPLED MANNER, LEADING TO A SIMPLIFIED SUPERPOSITION OF DIFFERENT INDEPENDENT ANALYSES. DEPENDING ON THE ASSUMPTIONS, THIS CAN POTENTIALLY LEAD TO OVERCONSERVATISM OR OMISSION OF MULTIPHYSICS PHENOMENA SUCH AS THE DEFORMATION OF STRUCTURAL SKIN PANELS WHICH ALTERS THE LOCAL FLOW FIELD AND RESULTS IN HIGHER AERODYNAMIC AND HEAT LOADING. TO ALLEVIATE THESE PROBLEMS, ATA ENGINEERING PROPOSES TO DEVELOP AN INNOVATIVE APPROACH UTILIZING AN EXISTING MULTIPHYSICS FRAMEWORK THAT ENABLES A MORE COMPLETE SIMULATION OF THE AEROHEATING ENVIRONMENT THROUGHOUT THE FLIGHT TRAJECTORY IN THE CONTINUUM REGIME IS PROPOSED. IN PHASE I, WE WILL DEMONSTRATE FEASIBILITY OF SOLVING THESE PROBLEMS IN ATA'S MULTIPHYSICS SIMULATION ENVIRONMENT BY COUPLING CHAR (A 3D, IMPLICIT CHARRING ABLATOR SOLVER), LOCI/CHEM (A COMPUTATIONAL FLUID DYNAMICS SOLVER FOR HIGHSPEED CHEMICALLY REACTING FLOWS), AND ABAQUS (A COMMERCIAL NONLINEAR STRUCTURAL DYNAMICS PACKAGE) TO CREATE A FULLY COUPLED AEROTHERMOELASTIC CHARRING ABLATIVE SOLVER. PHASE II WILL INVOLVE ENHANCEMENTS TO ENABLE FULL TRAJECTORY SIMULATION AND TOOL VALIDATION WITH EXPERIMENTAL DATA. | $125K |
| May 18, 2016 | National Aeronautics and Space AdministrationNASA GLENN RESEARCH CENTER | NNC16VC89P | 511210 | SW RENEWAL - ATA PRESSMAP, ATTUNE, IMAT IGF::OT::IGF | $10K |
| May 10, 2016 | National Aeronautics and Space AdministrationNASA JOHNSON SPACE CENTER | NNJ12JB12B | 541330 | AIRCRAFT AERONAUTICS AND STRUCTURAL ENGINEERING. | $62K |
| May 4, 2016 | National Aeronautics and Space AdministrationNASA GLENN RESEARCH CENTER | NNC16QA19P | 541712 | IGF::OT::IGF MODAL EXTRACTION DURING BASE DRIVE EXCITATION FOR EUROPEAN SERVICE MODULE STRUCTURAL TEST ARTICLE (E-STA) TESTING BACKGROUND: GRC NEEDS A METHOD FOR EXTRACTING FIXED BASE MODES WHILE A STRUCTURE IS MOUNTED ON A SHAKE TABLE. THE CONTRACTOR HAS DEVELOPED A METHOD FOR EXTRACTING FIXED BASE MODES FROM A TEST ARTICLE ON A SHAKER TABLE. THE KEY TO THE METHOD IS TO USE RESULTANT ACCELERATIONS OF THE TABLE (SUCH AS RIGID BODY ACCELERATIONS) AS REFERENCES WHEN CALCULATING FREQUENCY RESPONSE FUNCTIONS (FRFS). WHEN THIS IS DONE, THE MODES EXTRACTED FROM THE RESULTING FRFS CORRESPOND TO FIXED BASE MODES. NASA GLENN REQUIRES TECHNICAL SUPPORT DURING A MODAL SURVEY PERFORMED ON THE MECHANICAL VIBRATION FACILITY (MVF) 3-DOF SHAKER. THE MODAL SURVEY WILL BE A COMMISSIONING TEST USING A REPRESENTATIVE TEST ARTICLE TO VERIFY THE MVF 3-DOF SHAKE TABLE. SCOPE OF WORK: THE CONTRACTOR SHALL PROVIDE OFF-SITE AND ON-SITE SUPPORT TO HELP NASA GLENN WITH EXTRACTING MODAL PARAMETERS OF THE E-STA TEST ARTICLE. THE CONTRACTOR SHALL PROVIDE OFF-SITE AND ON-SITE SUPPORT TO HELP GRC WITH EXTRACTING MODAL PARAMETERS OF THE E-STA TEST ARTICLE. THE SUPPORT DURATION SHALL BE FOR A TOTAL OF TWO WEEKS. THE FIRST WEEK SHALL INVOLVE REVIEWING PRETEST ANALYSIS AND CONVERTING PRETEST ANALYSIS RESULTS INTO A SUITABLE FORMAT. THE SECOND WEEK OF SUPPORT SHALL BE ON-SITE SUPPORT TO HELP GRC IMPLEMENT THE TECHNIQUE USED TO GENERATE FIXED BASE FRFS. SUPPORT SHALL ALSO INVOLVE EXTRACTING STRUCTURAL MODES AND PROVIDING EXPERTISE TO HELP TESTING MOVE FORWARD IN AN EFFICIENT MANNER. GOVERNMENT-FURNISHED INFORMATION (TO BE PROVIDED BY NASA GRC) 1. PRE-TEST ANALYSIS RESULTS. 2. TIME-HISTORY TEST DATA IN A SUITABLE FORMAT SUCH AS UNIVERSAL FILE FORMAT, COMMA-SEPARATED VARIABLE FORMAT, OR I-DEAS ASSOCIATED DATA FILE FORMAT. 3. LOCATIONS AND DIRECTIONS OF ACCELEROMETER MEASUREMENTS (IN AN EXCEL SPREADSHEET WITH NODAL ID NUMBERS AND COORDINATE LOCATIONS). 4. ACCESS TO GRC MVF. DELIVERABLES TO GOVERNMENT 1. CONSULTATION DURING PRE-TEST ANALYSIS EFFORT. 2. ON-SITE SUPPORT AT GRC AND/OR PLUM BROOK STATION TO TRANSFER TECHNOLOGY AND IMPLEMENT TESTING METHODOLOGY. | $31K |
| Apr 8, 2016 | Department of DefenseW6QK AATD CONTR OFF | W911W616C0010 | 541712 | IGF::CL,CT::IGF SBIR PHASE I R&D CONTRACT | $100K |
| Apr 5, 2016 | National Aeronautics and Space AdministrationNASA JOHNSON SPACE CENTER | NNJ12JB12B | 541330 | AIRCRAFT AERONAUTICS AND STRUCTURAL ENGINEERING. | $38K |
| Mar 24, 2016 | National Aeronautics and Space AdministrationGLENN RESEARCH CENTER | NNC16VD46P | 511210 | IGF::OT::IGF SOFTWARE NEW PURCHASE FEMAP NX NASTRAN | $21K |
| Mar 2, 2016 | Department of DefenseNAVSEA HQ | N0002416C4006 | 541712 | BASE IGF::OT::IGF | $413K |
| Feb 18, 2016 | Department of DefenseFA8650 USAF AFMC AFRL PZL AFRL/PZL | FA865015C2573 | 541712 | IGF::OT::IGF ATA SBIR II FOLLOW-ON | $155K |
| Feb 18, 2016 | Department of DefenseFA8650 USAF AFMC AFRL PZL AFRL/PZL | FA865016C2634 | 541712 | IGF::OT::IGF INNOVATIVE METHOD FOR STARIN SENSOR CALIBRATION OF JSF FLEET AIRCRAFT | $1.5M |
| Feb 11, 2016 | National Aeronautics and Space AdministrationJOHNSON SPACE CENTER | NNJ12JB12B | 541330 | AIRCRAFT AERONAUTICS AND STRUCTURAL ENGINEERING. | $4K |
| Feb 9, 2016 | National Aeronautics and Space AdministrationGLENN RESEARCH CENTER | NNC15QA16P | 541712 | IGF::OT::IGF MODAL EXTRACTION DURING BASE DRIVE EXCITATION AND ACOUSTIC PRE-TEST ANALYSIS | $14K |
| Jan 14, 2016 | National Aeronautics and Space AdministrationNASA SHARED SERVICES CENTER | NNX16TC07P | 511210 | IGF::OT::IGF INTERNAL TRAINING PURCHASES COURSE TITLE: IMAT AND ATTUNE | $22K |
| Jan 6, 2016 | National Aeronautics and Space AdministrationGLENN RESEARCH CENTER | NNC16VA45P | 511210 | IGF::OT::IGF SOFTWARE RENEWAL - IMAT+SIGNAL PERPETUAL LICENSE | $7K |
| Jan 6, 2016 | Department of DefenseFA8650 USAF AFMC AFRL PZL AFRL/PZL | FA865015C2573 | 541712 | IGF::OT::IGF ATA SBIR II FOLLOW-ON | $75K |
| Dec 18, 2015 | National Aeronautics and Space AdministrationJOHNSON SPACE CENTER | NNJ12JB12B | 541330 | AIRCRAFT AERONAUTICS AND STRUCTURAL ENGINEERING. | $66K |
| Dec 17, 2015 | Department of DefenseNAVSEA HQ | N0002416C4006 | 541712 | BASE IGF::OT::IGF | $500K |
| Dec 9, 2015 | National Aeronautics and Space AdministrationJOHNSON SPACE CENTER | NNJ12JB12B | 541330 | AIRCRAFT AERONAUTICS AND STRUCTURAL ENGINEERING. | $13K |
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