Federal Contractor Profile
Luna Innovations Incorporated
$149M obligated·369 awards·7 agencies·17 NAICS
Federal Contracts
Showing contracts 401–448 of 448 total. Sorted by action date, most recent first. Excludes $0 modifications.
| Date | Agency | PIID | NAICS | Description | Amount |
|---|---|---|---|---|---|
| Aug 18, 2016 | Department of DefenseW6QK ACC-APG NATICK | W911QY16P0273 | 541712 | IGF::OT::IGF NOVEL FLAME RESISTANT NONWOVEN FABRICS FOR UNIFORMS | $150K |
| Aug 15, 2016 | Department of DefenseFA8651 AFRL RWK | FA865116P0212 | 541712 | IGF::OT::IGF SBIR PH 1 - SWIFT AND QUIET AIRFIELD ASSESSMENT | $150K |
| Aug 12, 2016 | Department of DefenseW6QK AATD CONTR OFF | W911W616C0034 | 541712 | IGF::OT::IGF SBIR PH I TOPIC NO. A16-004 ENTITLED: ENHANCED MATRICES FOR DURABLE AND DAMAGE TOLERANT COMPOSITES | $100K |
| Aug 3, 2016 | Department of DefenseW6QK ACC-APG DURHAM | W911NF15C0068 | 541712 | IGF::OT::IGF SBIR PH II TITLED: "BIOINSPIRED SYNTHETIC NANOPARTICLES AS UNIVERSAL ANTIVENOM" | $250K |
| Aug 1, 2016 | Department of DefenseW6QK ACC-APG | W91CRB15C0010 | 541712 | IGF::OT::IGF SBIR PHASE 1 - TOPIC NO. A15-029 | $50K |
| Jul 21, 2016 | Department of DefenseNAVSEA HQ | N0002416P4510 | 541712 | STATUS REPORT IGF::OT::IGF | $80K |
| Jul 11, 2016 | Department of DefenseOFFICE OF NAVAL RESEARCH | N0001415C0043 | 541712 | IGF::CT::IGF | $284K |
| Jul 11, 2016 | Department of DefenseOFFICE OF NAVAL RESEARCH | N0001416P1042 | 541712 | SBIRSOL2016.1 IGF::CT::IGF | $80K |
| Jul 7, 2016 | Department of DefenseFA8051 772 ESS PKD | FA805116P0014 | 541712 | IGF::OT::IGF SBIR TOPCE AF161-002 FAST SETTING | $100K |
| Jul 6, 2016 | Department of DefenseNAVSEA HQ | N0002415P4526 | 541712 | IGF::OT::IGF STATUS REPORT | $70K |
| Jul 5, 2016 | Department of DefenseFA8650 USAF AFMC AFRL PZL AFRL/PZL | FA865016M5033 | 541712 | IGF::OT::IGF ADVANCED MONITORING OF AIRCRAFT COATING CONDITION AND CORROSION | $150K |
| Jun 15, 2016 | Department of DefenseMISSILE DEFENSE AGENCY (MDA) | HQ014716C7506 | 541712 | ::IGF::OT::IGF:: SBIR PHASE I RESEARCH AND DEVELOPMENT | $40K |
| Jun 14, 2016 | Department of DefenseNAVAIR WARFARE CTR AIRCRAFT DIV | N6833516C0121 | 541712 | IGF::OT::IGF, RESEARCH AND DEVELOPMENT STTR PHASE II | $375K |
| Jun 13, 2016 | Department of DefenseFA8222 AFSC OL H PZIE | FA822216C0002 | 541712 | IGF::OT::IGF SMALL BUSINESS INNOVATION RESEARCH PHASE II | $51K |
| Jun 9, 2016 | National Aeronautics and Space AdministrationNASA SHARED SERVICES CENTER | NNX16CS66P | 541712 | IGF::OT::IGF EXPANDING THE CAPABILITY OF HUMAN EXPLORATION IS A PRIMARY GOAL FOR NASA AND THE IN-SITU RESOURCE UTILIZATION (ISRU) PROGRAM WHICH FOCUSES ON TRANSFORMING AVAILABLE MATERIAL RESOURCES ON EXTRATERRESTRIAL SURFACES INTO USABLE MATERIALS AND PRODUCTS. BY IDENTIFYING, COLLECTING, AND CONVERTING LOCAL RESOURCES INTO PRODUCTS THAT CAN REDUCE MISSION MASS, COST, AND/OR RISK, A SUSTAINABLE MANNED EXPEDITION TO MARS BECOMES CLOSER TO REALITY. BULK OR MODIFIED REGOLITH CAN BE COMBINED WITH A BINDER AS A CONCRETE AGGREGATE TO FORM A CONSTRUCTION MATERIAL THAT CAN BE EXTRUDED INTO BRICKS OR SLABS FOR STRUCTURES, SHELTERS, LANDING PADS, ROADS, AND SHIELDING. WITH THIS GOAL IN MIND, RESEARCHERS AT LUNA HAVE IDENTIFIED A POLYMER CONCRETE FORMULATION BASED ON UREA-FORMALDEHYDE (UF) THAT CAN BE PRESSED INTO HIGH COMPRESSIVE STRENGTH INTERLOCKING BRICKS SUITABLE FOR CONSTRUCTION. LUNA?S BINDER SYSTEM CAN ALSO BE PRODUCED IN-SITU FROM FEED GASES IDENTIFIED BY NASA (N2, H2, CO2) WHILE GENERATING O2 AND WATER. IF SUCCESSFUL, THESE UF POLYMERS ARE ALSO EXPECTED TO HAVE ADDITIONAL USE IN THE PRODUCTION OF PLASTIC PARTS OR COMPONENTS TO SUPPORT MISSION SUSTAINABILITY. | $125K |
| Jun 3, 2016 | Department of DefenseOFFICE OF NAVAL RESEARCH | N0001415C5053 | 541712 | ATMOSPHERIC CORROSION R&D IGF::CT::IGF | $243K |
| Jun 3, 2016 | National Aeronautics and Space AdministrationNASA SHARED SERVICES CENTER | NNX16CJ51P | 541712 | IGF::OT::IGF LUNA IS ADDRESSING NASA'S NEED TO DEVELOP NEW MULTIFUNCTIONAL TEXTILES FOR IMPROVED ENVIRONMENTAL PROTECTION GARMENTS (EPG). PREVIOUS PROTECTIVE SUITS SUCH AS THE APOLLO ERA EPG OR CURRENTLY USED EXTRAVEHICULAR MOBILITY UNIT (EMU) PROVIDE THERMAL AND MICROMETEOROID PROTECTION, BUT ARE INTENDED ONLY FOR SHORT DURATION USE. NASA PLANS FOR A FUTURE MANNED MARS MISSION WILL POTENTIALLY REQUIRE EXTENDED PROTECTION FOR UP TO 500 DAYS. CRITICAL CAPABILITIES FOR THESE TEXTILES INCLUDE IMPROVED I) DUST MITIGATION TO PROTECT FROM POTENTIALLY CORROSIVE OR ABRASIVE PARTICLES IN THE MARTIAN REGOLITH, II) CUT AND PUNCTURE RESISTANCE TO PROTECT THE SUIT BLADDER FROM DAMAGE FROM SHARP EDGES OF TOOLS AND ROCKS, AND III) DURABILITY FOR EXTENDED USE. LUNA WILL DEVELOP A MULTIFUNCTIONAL TEXTILE COMPOSITE THAT WILL ACHIEVE THESE STRINGENT GOALS, WHILE MAINTAINING COMFORT AND MOBILITY. OUR TEAM WILL COMBINE SEVERAL WELL DEVELOPED TECHNOLOGIES INTO A PRACTICAL TEXTILE DESIGN, WHICH WILL PROVIDE EXCELLENT PROTECTION FROM DUST, FIRE, CHEMICAL EXPOSURE, AND CUT/PUNCTURE. THESE WILL BE INTEGRATED TO MINIMIZE WEIGHT AND MAXIMIZE FLEXIBILITY SUCH AS TO NOT PROHIBIT, DEGRADE, OR INTERFERE WITH THE USE OF EQUIPMENT. | $125K |
| Jun 3, 2016 | Department of DefenseFA8650 USAF AFMC AFRL PZL AFRL/PZL | FA865016M5030 | 541712 | IGF::OT::IGF WIRELESS, INTELLIGENT, NON-INVASIVE, LOW-POWER LIFE-CYCLE STATUS MONITORING SYSTEM... | $150K |
| Jun 3, 2016 | Department of DefenseMISSILE DEFENSE AGENCY (MDA) | HQ014716C7720 | 541712 | IGF::OT::IGF SBIR PHASE II RESEARCH&DEVELOPMENT "RAPIDLY DISINTEGRATING COMPOSITES FOR FAST COOK-OFF MITIGATION" | $1000K |
| Jun 2, 2016 | Department of DefenseFA8650 USAF AFMC AFRL PZL AFRL/PZL | FA865016M5063 | 541712 | IGF::OT::IGF NEXT GENERATION CHROMATE-FREE FLEXIBLE AIRCRAFT PRIMERSBIR I | $150K |
| May 31, 2016 | Department of DefenseNAVAIR WARFARE CTR AIRCRAFT DIV | N6833516C0243 | 541712 | PROGRESS REPORT "IGF::OT::IGF" | $80K |
| May 31, 2016 | National Aeronautics and Space AdministrationNASA SHARED SERVICES CENTER | NNX16CP32P | 541712 | IGF::OT::IGF LUNA PROPOSES TO CONTINUE DEVELOPMENT OF ITS MARSUPIAL ROVER SENSING TETHER (MARS TETHER) TECHNOLOGY BY MINIATURIZING THE SENSOR'S INTERROGATION SYSTEM. LUNA IS CURRENTLY ENGAGED IN A PHASE II SBIR WITH NASA JPL (CONTRACT NNX13CP33P) TO DEVELOP A REVOLUTIONARY TECHNOLOGY THAT MONITORS THE DISTRIBUTED TENSION, CURVATURE, AND PATH OF A TETHER THAT CONNECTS A MARSUPIAL ROVER ROBOT TO ITS BASE STATION. THIS SENSING TETHER TURNS A PASSIVE CABLE THAT PROVIDES POWER AND COMMUNICATION INTO A POWERFUL TOOL THAT PROVIDES INFORMATION ABOUT THE HEALTH AND STATE OF BOTH THE ROVER AND THE TETHER, ALERTING THE BASE STATION TO POSSIBLE PINCH POINTS, SNAGGED CABLES, OR HIGH TENSION DUE TO POOR TRACTION OR STEEP SLOPE ENCOUNTERED BY THE ROVER. LUNA PROPOSES TO MINIATURIZE THE INTERROGATION SYSTEM OF THE MARS TETHER TO ENABLE JPL TO REALIZE THE FULL POTENTIAL OF THE ROVER. REDUCING THE SIZE, WEIGHT, AND POWER (SWAP) OF THE TETHER SYSTEM WILL ALLOW THE ROVER TO BE TESTED IN MULTIPLE REALISTIC SCENARIOS. IN ADDITION, MINIATURIZATION IS THE FIRST STEP IN PREPARING THE ENTIRE SENSING TETHER SYSTEM FOR FLIGHT-READINESS FOR MISSIONS TO MARS, ASTEROIDS, AND THE REST OF THE SOLAR SYSTEM | $125K |
| May 31, 2016 | National Aeronautics and Space AdministrationNASA SHARED SERVICES CENTER | NNX16CC51P | 541712 | IGF::OT::IGF LUNA INNOVATIONS IS PROPOSING TO DEVELOP THE RAPID IN-PLACE COMPOSITE ROTOR DAMAGE DETECTION (RIPCORDD) FOR DETERMINING AND TRACKING THE STRUCTURAL HEALTH OF COMPOSITE ROTORCRAFT BLADES. THERE IS A NEED FOR ACCURATE, RELIABLE ASSESSMENTS OF ROTOR CONDITION, PARTICULARLY FOR DAMAGE WHICH MAY NOT BE VISIBLE FROM THE SURFACE. THE RIPCORDD SYSTEM IS DESIGNED SUCH THAT IT WILL RESULT IN ABSOLUTELY NO INCREASE IN WEIGHT, POWER CONSUMPTION, OR VOLUME OF THE ROTORCRAFT. THE CORE OF THE RIPCORDD DEVICE IS A UNIQUE, DISTRIBUTED, FIBER OPTIC STRAIN SENSOR WHICH PROVIDES SPATIALLY DENSE STRAIN MEASUREMENTS (EVERY 1.25-5 MM) WITHIN THE COMPOSITE STRUCTURE OF THE BLADE, COUPLED WITH A GROUND BASED INSTALLATION OF LUNA'S PROVEN INSTRUMENTATION. DURING PHASE I LUNA (WITH GUIDANCE FROM A ROTORCRAFT OEM PARTNER) WILL DEMONSTRATE THE ABILITY TO DETECT AND CHARACTERIZE DAMAGE WHICH OCCURS IN SAMPLE COMPOSITE STRUCTURES. DURING PHASE II LUNA WILL MATURE THE TECHNOLOGY TO TRL6 BY TESTING THE SYSTEM IN A COMPLETE ROTOR. COMMERCIALIZATION WILL FOCUS ON TRANSITIONING THE TECHNOLOGY FIRST TO OEM MANUFACTURERS FOR NON-DESTRUCTIVE INSPECTION APPLICATIONS, FOLLOWED BY DEPLOYMENT TO ROTORCRAFT END USERS FOR LIFETIME MONITORING AND DIAGNOSTICS. | $125K |
| May 31, 2016 | National Aeronautics and Space AdministrationNASA SHARED SERVICES CENTER | NNX16CJ43P | 541712 | IGF::OT::IGF LUNA WILL PARTNER WITH DR. DAEWON KIM AND DR. SIRISH NAMILAE OF EMBRY RIDDLE AERONAUTICAL UNIVERSITY TO DEVELOP A MULTIFUNCTIONAL STRUCTURAL HEALTH MONITORING SOLUTION FOR LIGHTWEIGHT COMPOSITES USED IN LONG DURATION SPACE HABITATS. A COMBINATION OF FIBER OPTIC SENSORS, FOR STRAIN AND TEMPERATURE MONITORING, AND PIEZO RESISTIVE SENSORS, FOR IMPACT DETECTION, WILL BE UTILIZED TO PROVIDE A FLEXIBLE AND LIGHTWEIGHT HEALTH MONITORING SOLUTION. LUNA'S HIGH DEFINITION FIBER OPTIC MEASUREMENT SYSTEM UTILIZES LOW COST OPTICAL FIBER TO REPORT STRAIN OR TEMPERATURE POINTS EVERY 1.25 MM TO 5 MM ALONG THE SENSING FIBER. FIBER CAN BE EMBEDDED IN THE COMPOSITE MATERIALS TO DETECT CHANGES IN THE STRUCTURE AND PREDICT EARLY ONSET OF FAILURE, PRIOR TO VISIBLE DAMAGE. THE PIEZO RESISTIVE SENSORS WILL BE MOUNTED ON FLEXIBLE SOFT GOODS MATERIALS. DURING PHASE 1, LUNA WILL FABRICATE A SMALL-SCALE EXPANDABLE COMPOSITE TEST ARTICLE AND DEMONSTRATE THE ABILITY TO SENSE STRAIN USING EMBEDDED OPTICAL FIBER AND DETECT IMPACT EVENTS USING SURFACE MOUNTED PIEZO RESISTIVE SENSORS. DURING PHASE II, LUNA WILL DEMONSTRATE A SOLUTION THAT FUSES DATA FROM BOTH SENSING TECHNIQUES INTO ONE PLATFORM FOR A COHESIVE SHM SOLUTION. PHASE III WILL FOCUS ON TRANSITIONING THE TECHNOLOGY TO NASA AND NASA AFFILIATES SUCH AS BIGELOW AEROSPACE. | $125K |
| May 26, 2016 | National Aeronautics and Space AdministrationNASA SHARED SERVICES CENTER | NNX16CA26P | 541712 | IGF::OT::IGF NASA'S ORION SPACECRAFT WILL SERVE AS THE EXPLORATION VEHICLE THAT WILL CARRY A CREW TO SPACE, PROVIDE EMERGENCY ABORT CAPABILITY, SUSTAIN THE CREW DURING THE SPACE TRAVEL, AND PROVIDE SAFE RE-ENTRY FROM DEEP SPACE RETURN VELOCITIES. PLANETARY AEROCAPTURE AND ENTRY REQUIRES THAT THE CREW VEHICLE BE EQUIPPED WITH A THERMAL PROTECTION SYSTEM (TPS) COMPRISED OF LIGHTWEIGHT, HIGH PERFORMANCE ABLATOR MATERIALS. MATERIALS CURRENT UNDER DEVELOPMENT INCLUDE FELT OR WOVEN MATERIAL PRECURSORS IMPREGNATED WITH POLYMERS (I.E. PICA) AND/OR ADDITIVES TO IMPROVE ABLATION AND INSULATIVE PERFORMANCE, ALONG WITH THE BLOCK FORM OF AVCOAT ABLATOR. THERE IS A NEED FOR ADVANCEMENTS IN POLYMERS FOR USE IN BONDING AND/OR GAP FILLS FOR TILES OF ADVANCED TPS FOR EXTREME ENTRY CONDITIONS. THE IDEAL BINDER WOULD BE A FLEXIBLE, LOW GLASS TRANSITION TEMPERATURE POLYMER WITH A HIGH DECOMPOSITION TEMPERATURE/CHAR YIELD (COMPARABLE TO PHENOLIC) AND A HIGH (>1%) STRAIN-TO-FAILURE THAT IS COMPATIBLE WITH CURED EPOXY, PHENOLIC, AND/OR CYANATE ESTER. ENGINEERS AT LUNA HAVE DEVELOPED A NOVEL COPOLYMER ELASTOMER THAT HAS A VERY LOW GLASS TRANSITION (<- 100 DEGREES F) AND A DECOMPOSITION TEMPERATURE ON PAR WITH TYPICAL PHENOLIC ABLATIVES. THIS RESIN CAN BE HIGHLY FILLED TO TUNE ABLATIVE PROPERTIES AND IS COMPATIBLE WITH GLASS AND CARBON FABRIC SUBSTRATES. | $125K |
| May 6, 2016 | Department of DefenseW4LD USA HECSA | W912HQ16P0007 | 541712 | IGF::OT::IGF SERDP PROJECT WP-2603 ENTITLED HYBRID ULTRA-LOW VOC AND NON-HAP RAIN EROSION COATINGS. | $150K |
| May 5, 2016 | Department of DefenseNAVSEA HQ | N0002415C4025 | 541712 | BASE IGF::OT::IGF | $150K |
| Apr 29, 2016 | Department of DefenseNAVSEA HQ | N0002415C4005 | 541712 | BASE IGF::OT::IGF | $557K |
| Apr 25, 2016 | Department of DefenseW4LD USA HECSA | W912HQ09C0033 | 541712 | WP-1673 | $50K |
| Apr 13, 2016 | Department of DefenseNAVSEA HQ | N0002416C4042 | 541712 | BASE IGF::OT::IGF | $500K |
| Apr 1, 2016 | Department of the InteriorIBC ACQ SERVICES DIVISION (00063) | IND16PC00095 | 541712 | IGF::OT::IGF FLEXIBLE LOW-MODULUS NANOFIBER-BASED TIME NERVE INTERFACES | $100K |
| Mar 30, 2016 | Department of DefenseFA8501 OPL CONTRACTING AFSC/PZIO | FA850116C0002 | 541711 | IGF::OT::IGF SBIR PHASE II TOPIC AF141-205 | $749K |
| Mar 17, 2016 | Department of DefenseNAVAL AIR WARFARE CENTER AIR DIV | N0042116P0215 | 541712 | ENVIRONMENTAL NODE SENSOR | $67K |
| Mar 14, 2016 | Department of DefenseW4PZ USA MED RSCH ACQUIS ACT | W81XWH16C0010 | 541712 | IGF::OT::IGF SBIR ARMY PHASE II PROPOSAL A2-5968 | $409K |
| Feb 29, 2016 | Department of DefenseW6QK ACC-ORLANDO | W900KK13C0034 | 541712 | BASE AWARD - TRAC PHASE 1 | $341K |
| Feb 26, 2016 | Department of DefenseW4PZ USA MED RSCH ACQUIS ACT | W81XWH16C0014 | 541711 | DHP SBIR PHASE II #A2-6104. IGF::OT::IGF | $995K |
| Feb 22, 2016 | Department of DefenseNAVSEA HQ | N0002415C4025 | 541712 | BASE IGF::OT::IGF | $150K |
| Feb 3, 2016 | Department of DefenseNAVSEA HQ | N0002414C4016 | 541711 | IGF::OT::IGF BASE | $242K |
| Jan 28, 2016 | Department of DefenseOFFICE OF NAVAL RESEARCH | N0001415C0043 | 541712 | IGF::CT::IGF | $25K |
| Jan 28, 2016 | Department of DefenseW6QK ACC-ORLANDO | W900KK13C0034 | 541712 | BASE AWARD - TRAC PHASE 1 | $459K |
| Jan 25, 2016 | Department of DefenseW6QK ACC-APG DURHAM | W911NF16P0005 | 541712 | IGF::OT::IGF - SBIR PHASE I - LATERAL CANTHOTOMY AND CANTHOLYSIS TRAINING SYSTEM | $150K |
| Jan 5, 2016 | Department of DefenseFA8222 AFSC OL H PZIE | FA822216C0002 | 541712 | IGF::OT::IGF SMALL BUSINESS INNOVATION RESEARCH PHASE II | $371K |
| Dec 28, 2015 | Department of DefenseW4GG HQ US ARMY TACOM | W56HZV16C0021 | 541712 | IGF::OT::IGF PHASE II SBIR AWARD TO LUNA | $463K |
| Dec 17, 2015 | Department of DefenseMISSILE DEFENSE AGENCY (MDA) | HQ014716C7506 | 541712 | ::IGF::OT::IGF:: SBIR PHASE I RESEARCH AND DEVELOPMENT | $100K |
| Dec 15, 2015 | Department of DefenseW6QK ACC-APG ADELPHI | W911QX16C0001 | 541712 | IGF::OT::IGF DURABLE COLOR MATCHING COATINGS FOR VEHICLE TIRES | $499K |
| Dec 1, 2015 | Department of DefenseFA9550 AFRL AFOSR | FA955016C0005 | 541712 | IGF::OT::IGF SBIR PHASE I "HIGH REFRACTIVE INDEX HYBRID POLYSULFANE THERMOSETS FOR IR APPLICATIONS," DATED 25 FEB 2015 | $150K |
| Nov 12, 2015 | Department of DefenseNAVAIR WARFARE CTR AIRCRAFT DIV | N6833516C0086 | 541712 | DELIVERABLES (FFP), SBIR PHASE III C TYPE CONTRACT, IGF::OT::IGF | $51K |
| Oct 29, 2015 | Department of DefenseW4PZ USA MED RSCH ACQUIS ACT | W81XWH15C0010 | 921190 | IGF::OT::IGF ARMY PHASE I PROPOSAL A141-048-0391 | $50K |
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