Federal Contractor Profile
Luna Innovations Incorporated
$149M obligated·369 awards·7 agencies·17 NAICS
Federal Contracts
Showing contracts 351–400 of 448 total. Sorted by action date, most recent first. Excludes $0 modifications.
| Date | Agency | PIID | NAICS | Description | Amount |
|---|---|---|---|---|---|
| Jun 22, 2017 | Department of DefenseFA8650 USAF AFMC AFRL PZL AFRL/PZL | FA865017C5057 | 541712 | IGF::OT::IGF ADVANCED MONITORING OF AIRCRAFT COATING CONDITION AND CORROSION | $742K |
| Jun 21, 2017 | Department of DefenseFA8650 USAF AFMC AFRL PZL AFRL/PZL | FA865017P5035 | 541712 | IGF::OT::IGF LIGHTWEIGHT COMPOSITE PANELS FOR HEMP PROTECTION OF FIXED&MOBILE NC3 SYSTEMS | $150K |
| Jun 16, 2017 | Department of DefenseW6QK ACC-APG NATICK | W911QY17P0129 | 541712 | SBIR PHASE I - LUNA INNOVATIONS INC. IGF::OT::IGF | $100K |
| Jun 15, 2017 | Department of DefenseFA9550 AFRL AFOSR | FA955017C0013 | 541712 | IGF::OT::IGF "(SBIR II) ADDITIVELY MANUFACTURED HYPERSONIC WITH EMBEDDED INSTRUMENTATION" | $563K |
| Jun 14, 2017 | Department of DefenseNSWC DAHLGREN | N0002416P4510 | 541712 | STATUS REPORT IGF::OT::IGF | $70K |
| Jun 13, 2017 | Department of DefenseFA8051 772 ESS PKD | FA805117C0004 | 541712 | IGF::CT::IGF SBIR PHASE II - TOPIC CBD161-001 | $500K |
| Jun 8, 2017 | National Aeronautics and Space AdministrationNASA SHARED SERVICES CENTER | NNX17CK09P | 541712 | IGF::OT::IGF POLYMER MATRIX COMPOSITES ARE INCREASINGLY REPLACING TRADITIONAL METALLIC MATERIALS IN NASA LAUNCH VEHICLES. HOWEVER, THE REPAIR AND SUBSEQUENT INSPECTION METHODS FOR THESE MATERIALS ARE CONSIDERABLY MORE COMPLICATED. TYPICALLY, A COMPOSITE LAMINATE PATCH MUST BE MANUALLY FABRICATED AND BONDED OR CO-CURED TO THE DAMAGED STRUCTURE. TO ENSURE HIGH QUALITY PATCHES WITH SUFFICIENT COMPACTION AND LOW VOID CONTENT, SIGNIFICANT TIME, PREPARATION AND EQUIPMENT IS REQUIRED. CURRENT SURFACE PREPARATIONS REQUIRE TIME CONSUMING LABOR AND CAN BE A RISK FOR FURTHER DAMAGE. THE IDEAL REPAIR METHODOLOGY WOULD ALLOW FOR A RAPID STRUCTURAL REPAIR TO BE PERFORMED ON-SITE IN LOCATIONS WITH MINIMAL ACCESS AND WITHOUT THE NEED FOR EXTENSIVE TOOLING, SURFACE PREP, CURE TIMES AND COMPLICATED INSPECTION TECHNIQUES. ENGINEERS AT LUNA HAVE DEVELOPED A NUMBER OF TECHNOLOGIES THAT HAVE THE POTENTIAL TO ENABLE HIGH PERFORMANCE COMPOSITE REPAIR AND INSPECTION DURING PRE-LAUNCH GROUND PROCESSING. LUNA'S COMPREHENSIVE SYSTEM WILL REALIZE IMPROVEMENTS VIA FACILE SURFACE PREPARATION, REDUCTION OF SPECIALIZED FABRICATION EQUIPMENT, RAPID-ON-DEMAND CURING RESINS AND UTILIZATION OF LUNA'S UNIQUE FIBER OPTIC MEASUREMENT CAPABILITY FOR MONITORING REPAIR STATE. THIS PHASE I | $125K |
| Jun 5, 2017 | National Aeronautics and Space AdministrationNASA SHARED SERVICES CENTER | NNX17CL75P | 541712 | IGF::OT::IGF LUNA IS DEVELOPING A DISTRIBUTED ANEMOMETER THAT CAN DIRECTLY MEASURE FLOW FIELD VELOCITY PROFILES USING HIGH-DEFINITION FIBER OPTIC SENSING (HD-FOS). THE CONCEPT IS INSPIRED BY HOT-FILM ANEMOMETRY, BUT EXTENDS THE CAPABILITY FROM A POINT MEASUREMENT TO A DISTRIBUTED MEASUREMENT. WITH A SPATIAL RESOLUTION OF 1.25 MM, THOUSANDS OF DATA POINTS CAN BE COLLECTED ALONG AN OPTICAL FIBER TO ENABLE 1D, 2D OR 3D FIELD MEASUREMENTS, DEPENDING ON THE ROUTING OF THE SENSOR. THE BENEFITS OF THIS APPROACH COMPARED TO PARTICLE IMAGE VELOCIMETRY (PIV) INCLUDE: NO SEEDING OF THE FLOW IS NECESSARY; THE SENSOR CAN BE USED IN NON-LINE-OF-SIGHT LOCATIONS; VELOCITY AND TEMPERATURE PROFILES CAN SIMULTANEOUSLY BE ACQUIRED; AND THE TECHNOLOGY CAN POTENTIALLY BE IMPLEMENTED IN A FLYING VEHICLE. MEASUREMENTS OF BOUNDARY LAYER VELOCITY AND TEMPERATURE PROFILES, TRANSITION LOCATION, AND SKIN FRICTION CAN BE ATTAINED WITH THIS TECHNIQUE. PHASE I WILL PROVE THE FEASIBILITY OF FLOW VELOCITY MEASUREMENT FROM A DISTRIBUTED FIBER OPTIC SENSOR OVER A RANGE OF TEMPERATURES AND MACH NUMBERS TO QUANTIFY ITS ACCURACY. DURING PHASE II, THE TECHNOLOGY WILL BE MATURED FOR IMPLEMENTATION IN NASA WIND TUNNELS AND COMMERCIAL JET ENGINES. DURING PHASE III, LUNA WILL WORK WITH NASA AND INDUSTRY PARTNERS TO COMMERCIALIZE THE TECHNOLOGY. | $125K |
| Jun 5, 2017 | National Aeronautics and Space AdministrationNASA SHARED SERVICES CENTER | NNX17CG50P | 541712 | IGF::OT::IGF LUNA WILL TEAM WITH DR. JOHN BOWERS OF UCSB TO DEVELOP AN OPTICAL FREQUENCY DOMAIN REFLECTOMETRY (OFDR) SYSTEM-ON-CHIP USING HETEROGENEOUS SILICON PHOTONICS TO ENABLE A MINIMAL WEIGHT STRUCTURAL HEALTH MONITORING SYSTEM. THIS SYSTEM-ON-CHIP WILL BE THE BUILDING BLOCK FOR DISTRIBUTED SENSING INTERROGATION SYSTEMS THAT ARE THE SIZE OF A DECK OF PLAYING CARDS. THIS LIGHTWEIGHT, RUGGED, AND MINIATURE SYSTEM WILL ENABLE OFDR-BASED SHM SENSING APPLICATIONS IN SPACE, WHERE SIZE AND WEIGHT CONSTRAINTS ARE PARAMOUNT. PHASE I WILL PROVE THE FEASIBILITY OF USING THE HETEROGENEOUS SILICON TUNING LASER CHIP DEVELOPED BY UCSB TO DRIVE AN OFDR SENSOR IN THE LABORATORY, CULMINATING WITH A DISTRIBUTED STRAIN MEASUREMENT IN A COMPOSITE PART. DURING PHASE II, LUNA WILL DEVELOP A FULL OFDR SYSTEM-ON-CHIP, DEMONSTRATING THE MINIATURIZATION AND WEIGHT SAVINGS NECESSARY FOR DEEP SPACE SHM APPLICATIONS. OVERCOMING TECHNICAL HURDLES IN LASER TUNING, POLARIZATION CONTROL, AND DELAY LINE LENGTH ARE CRITICAL TO SUCCESSFUL COMMERCIALIZATION OF THE INNOVATION FOR SHM SENSING, AND WILL PROVIDE ADVANCEMENT IN THE STATE-OF-THE-ART OF SILICON PHOTONICS AND STRUCTURAL HEALTH MONITORING. | $125K |
| Jun 5, 2017 | National Aeronautics and Space AdministrationNASA SHARED SERVICES CENTER | NNX17CP50P | 541712 | IGF::OT::IGF LUNA PROPOSES TO CONTINUE DEVELOPMENT OF ITS MARSUPIAL ROVER SENSING TETHER (MARS TETHER) TECHNOLOGY BY EXTENDING THE LENGTH OF THE SENSING TECHNOLOGY OUT TO NEARLY A KILOMETER. LUNA'S REVOLUTIONARY TECHNOLOGY MONITORS THE DISTRIBUTED TENSION AND CURVATURE OF A TETHER THAT CONNECTS A MARSUPIAL ROVER TO ITS BASE STATION BY TURNING A PASSIVE CABLE FOR POWER AND COMMUNICATION INTO A POWERFUL TOOL THAT PROVIDES INFORMATION ABOUT THE HEALTH AND STATE OF BOTH THE ROVER AND THE TETHER. THE MARS TETHER CAN ALERT THE BASE STATION TO POSSIBLE PINCH POINTS, SNAGGED CABLES, OR HIGH TENSION DUE TO POOR TRACTION OR STEEP SLOPE. LUNA RECENTLY COMPLETED A PHASE II SBIR WITH NASA JPL THAT INTRODUCED THE FIRST MARS TETHER, IDENTIFYING A SNAG LOCATION ON A 50M TETHER WITH JPL'S AXEL ROVER AND SHOWING OPERATION ON A 100M TETHER. A RELATED PHASE I SBIR DEVELOPED A ROAD MAP FOR MINIATURIZING THE TETHER'S ACQUISITION SYSTEM. IN THIS PHASE I EFFORT, LUNA WILL PROVE THE FEASIBILITY OF EXTENDING THE LENGTH OF THE SENSING CAPABILITIES OF THE MARS TETHER THROUGH A FOCUS ON THE TENSION MEASUREMENT. THIS WILL GREATLY INCREASE THE OPERATING RANGE OF LIGHTWEIGHT, HIGHLY MOBILE ROVERS ENABLING MORE COMPLEX MISSIONS. | $125K |
| May 31, 2017 | Department of DefenseFA8650 USAF AFMC AFRL PZL AFRL/PZL | FA865017P5024 | 541711 | IGF::OT::IGF HIGH SCATTERING HYBRID POLYMER PAINT SYSTEM | $150K |
| May 30, 2017 | Department of DefenseNAVAL AIR WARFARE CENTER | N6893617C0053 | 541712 | IGF::OT::IGF; SBIR PHASE I TOPIC #N171-006 GUIDED ROCKET INDUCTIVE LINK. | $125K |
| May 25, 2017 | Department of DefenseOFFICE OF NAVAL RESEARCH | N0001415C5053 | 541712 | ATMOSPHERIC CORROSION R&D IGF::CT::IGF | $196K |
| May 23, 2017 | Department of DefenseW4PZ USA MED RSCH ACQUIS ACT | W81XWH17C0047 | 541712 | IGF::CT::IGF ARMY SBIR PHASE II(C) AWARD | $500K |
| May 19, 2017 | Department of the InteriorIBC ACQ SERVICES DIVISION (00063) | IND17PC00125 | 541712 | IGF::OT::IGF FLEXIBLE LOW-MODULUS NANOFIBER-BASED TIME NERVE INTERFACES | $505K |
| Apr 28, 2017 | Department of DefenseW6QK ACC-APG DURHAM | W911NF15C0068 | 541712 | IGF::OT::IGF SBIR PH II TITLED: "BIOINSPIRED SYNTHETIC NANOPARTICLES AS UNIVERSAL ANTIVENOM" | $250K |
| Apr 26, 2017 | National Aeronautics and Space AdministrationNASA SHARED SERVICES CENTER | NNX17CJ06C | 541712 | IGF::OT::IGF LUNA PROPOSES TO CONTINUE DEVELOPMENT OF INTEGRATED HIGH-DEFINITION FIBER OPTIC SENSORS (HD-FOS) AND CARBON NANOTUBE (CNT)-GRAPHENE PIEZORESISTIVE SENSORS FOR INFLATABLE SPACE HABITAT MATERIALS TO ENABLE FULL COVERAGE STRUCTURAL HEALTH MONITORING (SHM) AND IMPACT DETECTION. INFLATABLE HABITATS ARE KEY TO REDUCING THE WEIGHT OF SPACE STRUCTURES, ENABLING FUTURE LONG TERM MISSIONS AND PLANETARY HABITATION. THERE IS A NEED FOR MONITORING THE STRUCTURAL HEALTH OF THESE HABITATS, AS MANY OF THE METHODS USED ON EARTH ARE NOT APPLICABLE TO THE SPACE ENVIRONMENT OR THE MATERIALS USED. TO ACCOMPLISH THIS GOAL, LUNA HAS TEAMED WITH EMBRY-RIDDLE AERONAUTICAL UNIVERSITY (ERAU) WHO IS A LEADER IN THE DEVELOPMENT OF CNT SENSOR TECHNOLOGY. LUNA IS TEAMING WITH AN ESTABLISHED MANUFACTURER TO FABRICATE A SUB-SCALE INFLATABLE STRUCTURE WITH INTEGRATED SHM SENSORS WHICH WILL ENABLE THOROUGH CHARACTERIZATION OF THE APPROACH. DURING PHASE I, THE TEAM SUCCESSFULLY DEMONSTRATED DAMAGE DETECTION IN AN INFLATABLE PROTOTYPE AS WELL AS DYNAMIC IMPACT DETECTION OF SOFT GOODS LAYERS WITH THE TECHNOLOGIES. PHASE II WILL FOCUS ON INCREASING THE TRL OF THE SENSING TECHNOLOGIES AND PREPARING FOR TRANSITION INTO FUTURE NASA MISSIONS. PHASE III WILL FOCUS ON COMMERCIALIZING THE TECHNOLOGY WITH NASA AND NASA AFFILIATES. | $735K |
| Apr 11, 2017 | National Aeronautics and Space AdministrationNASA SHARED SERVICES CENTER | NNX17CC21C | 541712 | IGF::OT::IGF LUNA INNOVATIONS IS PROPOSING TO FURTHER DEVELOP THE RAPID IN-PLACE COMPOSITE ROTOR DAMAGE DETECTION (RIPCORDD) SYSTEM FOR DETERMINING AND TRACKING THE STRUCTURAL HEALTH OF COMPOSITE ROTORCRAFT BLADES AND OTHER COMPOSITE STRUCTURES. THERE IS A NEED FOR ACCURATE, RELIABLE ASSESSMENTS OF THE CONDITION OF COMPOSITE PARTS WHICH MAY HAVE BEEN DAMAGED THROUGH IMPACTS, FATIGUE, OR ABRASION. THIS IS ESPECIALLY TRUE FOR CASES IN WHICH THE DAMAGE MAY NOT BE VISIBLE FROM THE SURFACE. THE RIPCORDD SYSTEM IS DESIGNED SUCH THAT IT WILL ENABLE COMPOSITE ROTOR DAMAGE DETECTION IN SECONDS WITH ABSOLUTELY NO INCREASE IN WEIGHT, POWER CONSUMPTION, OR VOLUME OF THE ROTORCRAFT. THE CORE OF THE RIPCORDD DEVICE IS A UNIQUE, DISTRIBUTED, HIGH-DEFINITION FIBER OPTIC STRAIN SENSOR (HD-FOS) WHICH PROVIDES SPATIALLY DENSE STRAIN MEASUREMENTS (EVERY 1.25-2.5 MM) WITHIN THE COMPOSITE STRUCTURE, COUPLED WITH A GROUND BASED INSTALLATION OF LUNA'S PROVEN OPTICAL FREQUENCY DOMAIN REFLECTOMETRY (OFDR) INSTRUMENTATION. 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. | $750K |
| Apr 11, 2017 | Department of DefenseNAVFAC SYSTEMS AND EXP WARFARE CTR | N3943017P1947 | 541712 | IGF::OT::IGF SBIR PHASE I PYRRHOTITE DETECTION IN CONCRETE AGGREGATE | $80K |
| Mar 24, 2017 | Department of DefenseFA8051 772 ESS PKD | FA805116P0014 | 541712 | IGF::OT::IGF SBIR TOPCE AF161-002 FAST SETTING | $50K |
| Mar 24, 2017 | Department of DefenseW4PZ USA MED RSCH ACQUIS ACT | W81XWH16C0010 | 541712 | IGF::OT::IGF SBIR ARMY PHASE II PROPOSAL A2-5968 | $591K |
| Mar 22, 2017 | Department of DefenseFA8222 AFSC OL H PZIE | FA822216C0002 | 541712 | IGF::OT::IGF SMALL BUSINESS INNOVATION RESEARCH PHASE II | $322K |
| Mar 16, 2017 | Department of DefenseNAVAIR WARFARE CTR AIRCRAFT DIV | N6833516C0243 | 541712 | PROGRESS REPORT "IGF::OT::IGF" | $70K |
| Mar 15, 2017 | Department of DefenseOFFICE OF NAVAL RESEARCH | N0001415C5053 | 541712 | ATMOSPHERIC CORROSION R&D IGF::CT::IGF | $50K |
| Mar 8, 2017 | Department of DefenseFA8650 USAF AFMC AFRL PZL AFRL/PZL | FA865014C2529 | 541712 | IGF::OT::IGF EXTREME ENVIRONMENT STRESS AND STRAIN SENSING SYSTEM SBIRII | $244K |
| Feb 21, 2017 | Department of DefenseNAVSEA HQ | N0002414C4016 | 541711 | IGF::OT::IGF BASE | $300K |
| Feb 9, 2017 | Department of DefenseNAVSEA HQ | N0002417C4008 | 541712 | IGF::OT::IGF | $991K |
| Jan 11, 2017 | Department of DefenseDEFENSE THREAT REDUCTION AGENCY | HDTRA117P0002 | 541712 | IGF::OT::IGF C161-003-0027 SBIR PHASE I | $100K |
| Jan 5, 2017 | Department of DefenseW4PZ USA MED RSCH ACQUIS ACT | W81XWH15C0176 | 541712 | IGF::OT::IGF ARMY PHASE ONE SBIR | $50K |
| Dec 13, 2016 | Department of DefenseW4GG HQ US ARMY TACOM | W56HZV16C0021 | 541712 | IGF::OT::IGF PHASE II SBIR AWARD TO LUNA | $513K |
| Dec 9, 2016 | Department of the InteriorIBC ACQ SERVICES DIVISION (00063) | IND16PC00095 | 541712 | IGF::OT::IGF FLEXIBLE LOW-MODULUS NANOFIBER-BASED TIME NERVE INTERFACES | $50K |
| Dec 6, 2016 | Department of DefenseOFFICE OF NAVAL RESEARCH | N0001417P1008 | 541712 | SBIRSOL2016.2 IGF::CT::IGF | $80K |
| Nov 29, 2016 | Department of DefenseW4PZ USA MED RSCH ACQUIS ACT | W81XWH15C0139 | 541712 | IGF::OT::IGF ARMY PHASE I PROPOSAL A151-056-0480 | $50K |
| Oct 12, 2016 | Department of DefenseOFFICE OF NAVAL RESEARCH | N0001416C3076 | 541712 | IGF::CT::IGF | $375K |
| Oct 6, 2016 | Department of DefenseW6QK ACC-APG ADELPHI | W911QX16C0001 | 541712 | IGF::OT::IGF DURABLE COLOR MATCHING COATINGS FOR VEHICLE TIRES | $499K |
| Oct 5, 2016 | Department of DefenseNAVSEA HQ | N0002416C4042 | 541712 | BASE IGF::OT::IGF | $472K |
| Sep 21, 2016 | Department of DefenseW6QK ACC-APG | W911SR16C0014 | 541712 | IGF::OT::IGF PHASE II SBIR | $578K |
| Sep 21, 2016 | Department of DefenseW6QK ACC-APG DURHAM | W911NF16C0113 | 541712 | IGF::OT::IGF | $465K |
| Sep 20, 2016 | Department of DefenseW6QK ACC-APG ADELPHI | W911QX15C0024 | 541712 | IGF::OT::IGF SBIR II IDENTIFICATION OF MATERIAL DAMAGE PRECURSORS USING NOVEL NDE HARDWARE | $500K |
| Sep 19, 2016 | Department of DefenseW6QK ACC-APG | W911SR16C0050 | 541712 | IGF::OT::IGF SBIR PHASE I - LUNA INNOVATIONS INC. | $100K |
| Sep 19, 2016 | Department of DefenseNAVAIR WARFARE CTR AIRCRAFT DIV | N6833516C0121 | 541712 | IGF::OT::IGF, RESEARCH AND DEVELOPMENT STTR PHASE II | $375K |
| Sep 14, 2016 | Department of Health and Human ServicesNIH NCI | HHSN261201600007C | 541712 | IGF::OT::IGF SBIR TOPIC 347 PHASE I | $225K |
| Sep 13, 2016 | Department of DefenseFA8501 OPL CONTRACTING AFSC/PZIO | FA850114C0017 | 541712 | IGF::OT::IGF SIBR PHASE II; TOPIC: AF112 | $250K |
| Sep 9, 2016 | Department of DefenseNAVSEA HQ | N0002415C4025 | 541712 | BASE IGF::OT::IGF | $500K |
| Sep 7, 2016 | Department of DefenseW4GG HQ US ARMY TACOM | W56HZV16C0148 | 541712 | IGF::OT::IGF PHASE I SBIR CONTRACT FOR HIGH FREQUENCY PISTON SURFACE TEMPERATURE MEASUREMENT SYSTEM. | $105K |
| Sep 2, 2016 | Department of DefenseNAVAL AIR WARFARE CENTER AIR DIV | N0042116P0729 | 541712 | LS2A-485 (WIRED) SENSOR NODE | $98K |
| Sep 1, 2016 | Department of DefenseFA8571 MAINT CONTRACTING AFSC PZIM | FA850116C0002 | 541711 | IGF::OT::IGF SBIR PHASE II TOPIC AF141-205 | $94K |
| Aug 26, 2016 | Department of DefenseW4PZ USA MED RSCH ACQUIS ACT | W81XWH16C0107 | 541712 | IGF::OT::IGF ARMY PHASE I PROPOSAL A161-051-0701 | $100K |
| Aug 23, 2016 | Department of DefenseW4PZ USA MED RSCH ACQUIS ACT | W81XWH16C0120 | 541712 | IGF::OT::IGF. ARMY PHASE I PROPOSAL A161-059-0427 ENTITLED, "PERIPHERAL NERVE TARGETING LIPOSOME-LOADED TUNECOAT(TM) DRESSING FOR TREATMENT OF PERIPHERAL NEUROPATHY." | $100K |
| Aug 22, 2016 | Department of Health and Human ServicesNATIONAL INSTITUTES OF HEALTH NIAID | HHSN272201600034C | 541990 | IGF::OT::IGF - "INNOVATIVE ORAL FORMULATIONS FOR ANTI-TB DRUGS" | $225K |
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