Federal Contractor Profile
Faraday Technology, INC.
$27M obligated·71 awards·3 agencies·3 NAICS
Federal Contracts
Showing contracts 51–81 of 81 total. Sorted by action date, most recent first. Excludes $0 modifications.
| Date | Agency | PIID | NAICS | Description | Amount |
|---|---|---|---|---|---|
| Apr 30, 2020 | National Aeronautics and Space AdministrationNASA SHARED SERVICES CENTER | NNX17CJ12C | 541712 | IGF::OT::IGF AMONG THE NUMEROUS TECHNOLOGICAL ADVANCES SOUGHT IN ORDER TO FACILITATE HUMAN SPACE TRAVEL, SOLUTIONS ARE NEEDED FOR TECHNOLOGY THAT SUPPORTS ENERGY-EFFICIENT MAINTENANCE OF CLOSED AIR, WATER, AND WASTE SYSTEMS IN MICROGRAVITY SPACECRAFT HABITATS, LIKE MARS. IN PARTICULAR, A TECHNIQUE FOR THE IN-SITU GENERATION OF CLEANING/SANITIZING SOLUTIONS IS NEEDED TO REDUCE THE DEMAND OF EARTH BASED MATERIALS LIKE CLEANING SUPPLIES TO MEET PERSONAL HYGIENE REQUIREMENT DURING SPACE MISSIONS. THEREFORE, IN THIS PHASE II SBIR PROGRAM, FARADAY WILL CONTINUE THE TECHNOLOGY DEVELOPMENT EFFORTS OF THE PHASE I BY: (1) DEMONSTRATING THE POTENTIAL OF THE DEVICE DESIGN BY TESTING UNDER ZERO GRAVITY; (2) OPTIMIZING THE GDE CATALYTICS, STRUCTURE, AND WETTABILITY, (3) DEMONSTRATING THE POTENTIAL TO USE ONBOARD ISS WATER UTILITIES, (4) DEVELOPING AN ELECTROCHEMICAL PEROXIDE DETECTOR, AND (5) DESIGNING AND BUILDING AN?-SCALE REACTOR TO PRODUCE 1 L/DAY OF 2 W/W% H2O2. THIS EVALUATION WILL ENABLE TRL ENHANCEMENT AND DEMONSTRATE A POTENTIAL PATH FORWARD FOR DEMONSTRATION. THIS TECHNOLOGY HAS THE POTENTIAL TO BE AN ALTERNATIVE METHOD FOR SYNTHESIS OF COMMERCIAL HYDROGEN PEROXIDE OR IN-SITU ONSITE DISINFECTION OF PROCESS WASTE STREAMS AND COULD BE AN INTEGRAL PART OF LONG TERM LIFE SUPPORT ON NASA'S MANNED SPACE MISSIONS. | $289K |
| Apr 29, 2020 | National Aeronautics and Space AdministrationNASA SHARED SERVICES CENTER | 80NSSC20C0070 | 541715 | ENVIRONMENTAL CONTROL AND LIFE SUPPORT FOR SPACECRAFT AND HABITAT | $289K |
| Aug 8, 2019 | National Aeronautics and Space AdministrationNASA SHARED SERVICES CENTER | 80NSSC19C0177 | 541715 | DEVELOP AN APPROACH TO SCALABLY APPLY CARBON NANOTUBE BASED BLACK COATINGS TO LARGE AREA SURFACE AND DEMONSTRATE THE COATING S POTENTIAL TO SUPPRESS SCATTERED LIGHT, WITHSTAND LAUNCH CONDITIONS, AND RESIST RADIATION EFFECTS AND ATOMIC OXYGEN EROSION. | $755K |
| Apr 26, 2019 | Environmental Protection AgencyINFORMATION TECHNOLOGY ACQ DIV (ITA | 68HERD19C0023 | 541715 | FARADAY TECHNOLOGY, INC. SBIR PHASE I | $100K |
| Apr 24, 2019 | Environmental Protection AgencyINFORMATION TECHNOLOGY ACQ DIV (ITA | 68HERD19C0011 | 541715 | FARADAY TECHNOLOGY, INC SBIR PHASE I | $100K |
| Apr 17, 2019 | Department of DefenseFA8650 USAF AFMC AFRL PZL AFRL/PZL | FA865019P5158 | 541715 | SBIR I TOPIC AF191-096; LOW COST ELECTROCHEMICAL MACHINING (ECM) PROCESSES FOR AEROSPACE COMPONENTS | $150K |
| Mar 20, 2019 | Department of DefenseMISSILE DEFENSE AGENCY (MDA) | HQ014719C7065 | 541715 | SBIR/STTR PHASE I RESEARCH&DEVELOPMENT: CARBON NANOTUBE COATINGS ON ELECTROCHEMICAL TEXTURED SURFACES FOR ADVANCED ADSORPTIVE BAFFLES | $105K |
| Jan 30, 2019 | Department of DefenseFA9453 AFRL RVK | FA945319P0573 | 541715 | S3 PRGM - PASSIVE CATHODE DEVICE FOR SPACE PLASMA APPLICATIONS - AF TOPIC 18A-T011 - STTR 1 - BASIC | $150K |
| Jan 9, 2019 | Department of DefenseFA8650 USAF AFMC AFRL PZL AFRL/PZL | FA865019P2024 | 541715 | SBIR PHASE I "ELECTROCHEMICAL APERTURE ENABLING FAST ACTIVATION OF LITHIUM-ION RESERVE BATTERIES" | $150K |
| Dec 27, 2018 | Department of DefenseW6QK ACC-PICA | W15QKN18C0010 | 541715 | PHASE II ENHANCEMENT FOR TOPIC A16-013 | $501K |
| Sep 26, 2018 | National Aeronautics and Space AdministrationNASA SHARED SERVICES CENTER | 80NSSC18C0222 | 541715 | AMONG NUMEROUS TECHNOLOGICAL ADVANCES SOUGHT IN ORDER TO FACILITATE HUMAN SPACE TRAVEL, INNOVATIONS ARE NEEDED THAT SUPPORTS THE MASS- AND ENERGY-EFFICIENT MAINTENANCE OF CLOSED AIR, WATER, AND WASTE SYSTEMS IN SPACECRAFT HABITATS THAT OPERATE ON PLANETARY ENVIRONMENTS SUCH AS MARS AND WITHIN MICROGRAVITY. WASTE-WATER TREATMENT SYSTEM ON BOARD THE ISS IS ONE SUCH SYSTEM THAT HAS LIFETIME/DURABILITY LIMITATIONS AND WOULD BENEFIT FROM IMPROVEMENTS. THEREFORE, IN THIS PHASE II STTR PROGRAM FARADAY WILL CONTINUE THE TECHNOLOGY DEVELOPMENT EFFORTS OF THE PHASE I BY: (1) LEVERAGING EXISTING KNOWLEDGE IN THE COMBINED EXPERTISE OF FARADAY AND UPR FOR DEVICE DESIGN AND TESTING UNDER ZERO GRAVITY CONDITIONS; (2) EXPLORING THE BACTERIA FOR UREA BIOREACTOR AND ELECTROCATALYST FOR AMMONIA REACTOR TAILORED FOR ZERO GRAVITY CONDITIONS OF OUR SUBCONTRACTOR UPR, (3) OPTIMIZING THE ELECTROCATALYTIC EFFICIENCY AND WASTE WATER TREATMENT RATE WITH ON-BOARD WATER SIMULATES, (4) VALIDATING PERFORMANCE UNDER ZERO GRAVITY CONDITIONS; AND (5) DESIGNING AND BUILDING A DEMONSTRATION-SCALE BIO-ELECTROCHEMICAL REACTOR UNIT CAPABLE OF MEETING NASA REQUIRED SPECIFICATIONS . THIS EVALUATION WILL ENABLE TRL ENHANCEMENT AND DEMONSTRATE A POTENTIAL PATH FORWARD FOR PHASE II SCALE-UP AND ASSESSMENT OF THE BIO-ELECTROCHEMICAL SYSTEM IN ZERO-GRAVITY ENVIRONMENTS. THIS TECHNOLOGY HAS THE POTENTIAL TO BE AN INTEGRAL PART OF LONG TERM LIFE SUPPORT ON NASA S MANNED SPACE MISSIONS. | $754K |
| Aug 15, 2018 | Department of DefenseW4GG HQ US ARMY TACOM | W56HZV18C0100 | 541715 | IGF::OT::IGF PHASE I SBIR | $105K |
| Jul 27, 2018 | National Aeronautics and Space AdministrationNASA SHARED SERVICES CENTER | 80NSSC18P2062 | 541715 | SPACE-BORNE INSTRUMENTS, SUCH AS TELESCOPE HOUSINGS AND BAFFLES WHERE STRAY LIGHT REDUCTION IS VITAL REQUIRES THE REDUCTION OF THE STRAY LIGHT FROM OPTICAL PAYLOADS. LOW REFLECTIVE COATINGS (WITH REFLECTIVITY OF ~0.1% OR LESS) IN THE BROAD SPECTRAL RANGE (VISIBLE- NEAR INFRARED) HAVE TO BE DEVELOPED. THESE BLACK COATINGS SHOULD ALSO WITHSTAND AGGRESSIVE SPACE ENVIRONMENTS AND LAUNCH CONDITIONS WITH MARGINAL IMPACT ON THEIR ADHESION AND OPTICAL PERFORMANCE. A PROMISING CANDIDATE WITH AN OUTSTANDING DIFFUSE ABSORPTANCE IS CHEMICALLY VAPOR DEPOSITED LAYERS OF CARBON NANOTUBES. HOWEVER, THESE COATINGS ARE TYPICALLY GROWN BY EXPENSIVE AND THERMALLY BASED TECHNIQUES AND CAN BE DIFFICULT TO APPLY TO 3D STRUCTURES. PHASE I WILL DEMONSTRATE THE FEASIBILITY OF A LOW-COST, EFFICIENT AND SCALABLE MANUFACTURING PROCESS FOR THE DEPOSITION OF DURABLE, LOW REFLECTIVITY CNT BLACK COATINGS BASED ON THE USE OF PULSE AND PULSE REVERSE ELECTROPHORETIC DEPOSITION. THIS TECHNOLOGY WILL ENABLE THE CONFORMAL DEPOSITION OF CNT BLACK COATINGS ON COMPLEX SHAPES AND SHARP EDGES ON COMMONLY USED SPACECRAFT MATERIALS SUCH AS ALUMINUM AND TITANIUM SUBSTRATES. IN PHASE I, FARADAY WILL DEVELOP AN ELECTROPHORETIC BATH FORMULATION AND MANIPULATE THE PULSED ELECTRIC FIELD PARAMETERS TO DEPOSIT DENSE, VERTICALLY ALIGNED MULTI-WALLED CARBON NANOTUBES ONTO TEST SUBSTRATES, AND CHARACTERIZE THE DEPOSITED COATINGS TO SHOW THE POTENTIAL OF ACHIEVING THE DESIRED REFLECTIVITY OF 0.1% OR LESS, MONITOR THE THICKNESS UNIFORMITY AND MORPHOLOGY AND DEMONSTRATE THE POTENTIAL FOR DURABILITY IN SEVERE LAUNCH CONDITIONS. FINALLY, A PRELIMINARY TECHNO-ECONOMIC WILL BE COMPLETED TO SHOW THE POTENTIAL TO REDUCE THE COST OF EXISTING PROCESSES WHILE MAINTAINING REQUIRED OPTICAL PROPERTIES. PHASE II WOULD OPTIMIZE THE DEPOSITION PARAMETERS, ELUCIDATE THEIR EFFECT ON SCATTERED LIGHT SUPPRESSION AND THERMAL-STRUCTURAL PERFORMANCE, PROCESS ALPHA-SCALE COMPONENTS, AND, TO THE EXTENT POSSIBLE, PERFORM A SYSTEM-LEVEL VALIDATION. | $125K |
| Feb 12, 2018 | Department of DefenseFA9453 AFRL RVK | FA945317C0490 | 541712 | IGF::OT::IGF ROBUST IONIC LIQUID ELECTROLYTES FOR REVERSIBLE ELECTROPLATING OF MIRRORS | $187K |
| Nov 16, 2017 | Department of DefenseW6QK ACC-PICA | W15QKN18C0010 | 541715 | PHASE II ENHANCEMENT FOR TOPIC A16-013 | $496K |
| Sep 13, 2017 | Department of DefenseW6QK ACC-PICA | W15QKN17C0079 | 541712 | IGF::OT::IGF THIS IS A PHASE I SBIR CONTRACT FOR TOPIC A17-081. | $99K |
| Aug 10, 2017 | Department of DefenseW6QK ACC-PICA | W15QKN16C0070 | 541712 | IGF::OT::IGF MULTIPHYSICS BASED TOOL DESIGN FOR ELECTROCHEMICAL MACHINING, SBIR PHASE I. | $50K |
| Aug 7, 2017 | Department of DefenseFA8650 USAF AFMC AFRL PZL AFRL/PZL | FA865017C5074 | 541712 | IGF::OT::IGF NON DESTRUCTIVE EVAL. OF URETHANE-EPOXY COATING SYSTEMS | $750K |
| Aug 3, 2017 | Department of DefenseFA9453 AFRL RVK | FA945317C0490 | 541712 | IGF::OT::IGF ROBUST IONIC LIQUID ELECTROLYTES FOR REVERSIBLE ELECTROPLATING OF MIRRORS | $563K |
| Jun 8, 2017 | National Aeronautics and Space AdministrationNASA SHARED SERVICES CENTER | NNX17CA30P | 541712 | IGF::OT::IGF AMONG THE NUMEROUS TECHNOLOGICAL ADVANCES SOUGHT IN ORDER TO FACILITATE HUMAN SPACE TRAVEL, SOLUTIONS AND INNOVATIONS ARE NEEDED FOR TECHNIQUES THAT SUPPORTS THE MASS- AND ENERGY EFFICIENT MAINTENANCE OF CLOSED AIR, WATER, AND WASTE SYSTEMS IN SPACECRAFT HABITATS THAT OPERATE WITHIN MICROGRAVITY. AS MISSIONS ARE FORESEEN TO BE EXTENDED WITH LIMITED EARTH RESUPPLY AVAILABLE THERE IS NEED TO DEVELOP DURABLE AND SUSTAINABLE CLOSED LOOP LIVING SYSTEMS. WASTE WATER TREATMENT AND RECOVERY SYSTEM THAT IS MANAGED BY ECLSS ON BOARD THE ISS IS ONE SUCH SYSTEM THAT HAS LIFETIME/DURABILITY LIMITATIONS AND WOULD BENEFIT FROM IMPROVEMENTS TO INCREASE ITS LIFETIME EFFICIENCY. THEREFORE, IN ORDER TO ACHIEVE NASAS GOALS OF EXTENDED MANNED DEEP SPACE MISSIONS, FARADAY TECHNOLOGY INC. AND DR. CARLOS CABRERA OF THE UNIVERSITY OF PUERTO RICO (UPR) PROPOSE TO DEVELOP A TECHNIQUE TO ELIMINATE MANY OF THE CONTAMINANTS THAT COMMONLY FOUL THE WASTE WATER TREATMENT SYSTEM AND PRODUCE A MORE DURABLE CLOSED LOOP PROCESS COMPATIBLE WITH EXISTING ECLSS MAINFRAME TO TREAT AND RECOVER WATER. IN THIS PROGRAM, UPR WILL DEVELOP ENZYME BASED BIO-REACTOR TO EFFICIENTLY CONVERT UREA TO AMMONIA, WHILE FARADAY WILL SCALE AND OPTIMIZE AMMONIA ELECTROLYZER INCORPORATING CUSTOM-FABRICATED GAS DIFFUSION CATHODE AND ANODE. THIS INTEGRATED SYSTEM IS ANTICIPATED TO ENABLE SIGNIFICANT PERFORMANCE ENHANCEMENT BY REDUCING OSMOSIS MEMBRANE FOULING CAUSED BY CONTAMINANTS FROM THE WASTE STREAM AND THEREBY INCREASING THE EFFICIENCY AND DURABILITY OF THE TREATMENT PROCESS. THIS TECHNOLOGY HAS THE POTENTIAL TO BE COMPATIBLE WITH EXISTING ECLSS SYSTEMS AND BE AN INTEGRAL PART OF THE CLOSED LOOP LIVING SYSTEMS REQUIRED FOR LONG TERM LIFE SUPPORT ON NASAS MANNED SPACE MISSIONS. | $125K |
| Jun 7, 2017 | National Aeronautics and Space AdministrationNASA SHARED SERVICES CENTER | NNX17CC44P | 541712 | IGF::OT::IGF IN ORDER TO IMPROVE HIGH-TEMPERATURE OXIDATION AND CORROSION RESISTANCE OF CRITICAL SUPERALLOY COMPONENTS IN TURBINE ENGINES INNOVATIVE PROCESSING METHODS MUST BE DEVISED TO IMPROVE COATING AND MATERIALS PROPERTIES AT A HIGHER RELIABILITY AND LOWER COSTS. WHETHER OR NOT THERMAL BARRIER COATING ARE APPLIED TO THE ENGINE COMPONENTS, THE RESISTANCE TO OXIDATION AND HOT CORROSION RELIES ON METALLIC COATINGS PROTECTING THE SUPERALLOY SUBSTRATE. THESE METALLIC COATINGS ARE COMMONLY EITHER DIFFUSION ALUMINIDES OR MCRALY OVERLAYS (WHERE M=NI, CO, FE, NI+CO, ETC). COMPARED WITH DIFFUSION COATINGS, MCRALY COATINGS ARE MORE FLEXIBLE IN TERMS OF COMPOSITION SELECTION FOR ACHIEVING A MORE BALANCED COMBINATION OF COATING PROPERTIES AND HAVING A LOWER DUCTILE TO BRITTLE TRANSITION TEMPERATURE, WHICH MAKES THEM MORE RESISTANT TO CRACKING UPON THERMAL CYCLING. SEVERAL TECHNIQUES HAVE BEEN DEVELOPED TO DEPOSIT MCRALY COATINGS INCLUDING PHYSICAL VAPOR DEPOSITION, ELECTROLYTIC CODEPOSITION, ELECTROPHORESIS, AND AUTOCATALYTIC ELECTROLESS DEPOSITION, OF WHICH ELECTROLYTIC CODEPOSITION APPEARS TO BE A PROMISING, LOW COST, NON-LINE OF SIGHT APPROACH. THEREFORE, THE OVERALL OBJECTIVE OF THE PHASE I AND II PROGRAMS IS TO CREATE A SCALABLE COST EFFECTIVE PROCESS TO PRODUCE COATINGS THAT CAN ENHANCE HIGH TEMPERATURE RELIABILITY AND CORROSION/OXIDATION AND EROSION RESISTANCE. THIS PROGRAM WILL BUILD OFF OF DR. YING ZHANG (TENNESSEE TECHNOLOGICAL UNIVERSITY) ELECTROLYTIC CODEPOSITION WORK AND FARADAY TECHNOLOGY'S ALLOY COATING DEVELOPMENT EFFORTS TO CREATE A SCALABLE PROCESS TO ELECTROLYTIC CODEPOSIT MCRALY ONTO ENGINE SHAPED COMPONENTS AND TO INVESTIGATE OTHER POTENTIAL MCRALX ALLOY ELEMENTS THAT COULD FURTHER INCREASE THE COATINGS TEMPERATURE RESISTANCE. IF SUCCESSFUL THIS PROGRAM HAS THE POTENTIAL TO GREATLY IMPROVE THE OXIDATION AND CORROSION RESISTANCE OF METALLIC COATINGS WHILE ALSO IMPROVING THEIR RELIABILITY AT HIGHER OPERATING TEMPERATURES AND REDUCING THEIR MANUFACTURING COSTS. | $125K |
| Jun 5, 2017 | National Aeronautics and Space AdministrationNASA SHARED SERVICES CENTER | NNX17CP39P | 541712 | IGF::OT::IGF THIS PHASE I PROGRAM ADDRESSES THE CHALLENGE OF GAINING THE NECESSARY KNOWLEDGE NEEDED TO SUPPORT CERTIFICATION OF ADDITIVE MANUFACTURING (AM) HARDWARE AND ACHIEVING THE DESIRED SURFACE FINISH AND MECHANICAL PROPERTIES ON HIGH VALUE COMPONENTS PRODUCED BY AM. TO ACHIEVE THIS GOAL FARADAY TECHNOLOGY INC., WILL WORK WITH TEAM MEMBERS AT UES INC., CALRAM INC., KEYSTONE SYNERGISTIC ENTERPRISE INC., AND REM SURFACE ENGINEERING TO DEVELOP THE NECESSARY EMPIRICAL KNOWLEDGE TO PRODUCE A MANUFACTURING DECISION TREE MODEL (MDTM) THAT WILL ENABLE THE PART DESIGNER TO REDUCE THE CYCLE TIME REQUIRED PRODUCE THE DESIRED PART WITH THE REQUIRED SURFACE FINISH. THE MDTM WILL BE DESIGNED TO SELECT THE APPROPRIATE BUILD PATHWAY TO FORM THE DESIRED COMPONENT AND IMPROVE THE AS-BUILT SURFACE FINISH ON THE REQUIRED AREAS WHILE ALSO DETERMINING THE NECESSARY SECONDARY STEPS TO ACHIEVE THE DESIRED SURFACE FINISH ON ALL REQUIRED SURFACES. WITH THIS TEAMS COMBINED EXPERTISE RANGE FROM AM PART BUILDING [ARCAM (E-BEAM), SLM (LASER), WIRE FED (E-BEAM)], SECONDARY AM PART FINISHING [ELECTROCHEMICAL AND ISOTROPIC], AND POST PROCESS AM MATERIAL EVALUATION (TENSILE AND MICROSTRUCTURAL CHARACTERIZATION) WE WILL BE ABLE TO DIAGNOSE THE BEST MANUFACTURING CYCLE TO REDUCE TIME AND COST WHILE ENSURING THE FUNCTIONALITY OF THE PRODUCED MATERIAL IS MAINTAINED THROUGH EACH PROCESSING STEP. IT IS ENVISIONED THAT THE OUTCOME OF THIS PHASE I/II PROGRAM WOULD BE A WORKING MDTM THAT HAS THE POTENTIAL TO DIAGNOSE THE BEST MANUFACTURING PATHWAY TO PRODUCE A WIDE RANGE OF HIGH-VALUE COMPONENTS WITH VARIOUS SHAPES AND CONTOURS. | $125K |
| May 1, 2017 | National Aeronautics and Space AdministrationNASA SHARED SERVICES CENTER | NNX17CJ12C | 541712 | IGF::OT::IGF AMONG THE NUMEROUS TECHNOLOGICAL ADVANCES SOUGHT IN ORDER TO FACILITATE HUMAN SPACE TRAVEL, SOLUTIONS ARE NEEDED FOR TECHNOLOGY THAT SUPPORTS ENERGY-EFFICIENT MAINTENANCE OF CLOSED AIR, WATER, AND WASTE SYSTEMS IN MICROGRAVITY SPACECRAFT HABITATS, LIKE MARS. IN PARTICULAR, A TECHNIQUE FOR THE IN-SITU GENERATION OF CLEANING/SANITIZING SOLUTIONS IS NEEDED TO REDUCE THE DEMAND OF EARTH BASED MATERIALS LIKE CLEANING SUPPLIES TO MEET PERSONAL HYGIENE REQUIREMENT DURING SPACE MISSIONS. THEREFORE, IN THIS PHASE II SBIR PROGRAM, FARADAY WILL CONTINUE THE TECHNOLOGY DEVELOPMENT EFFORTS OF THE PHASE I BY: (1) DEMONSTRATING THE POTENTIAL OF THE DEVICE DESIGN BY TESTING UNDER ZERO GRAVITY; (2) OPTIMIZING THE GDE CATALYTICS, STRUCTURE, AND WETTABILITY, (3) DEMONSTRATING THE POTENTIAL TO USE ONBOARD ISS WATER UTILITIES, (4) DEVELOPING AN ELECTROCHEMICAL PEROXIDE DETECTOR, AND (5) DESIGNING AND BUILDING AN?-SCALE REACTOR TO PRODUCE 1 L/DAY OF 2 W/W% H2O2. THIS EVALUATION WILL ENABLE TRL ENHANCEMENT AND DEMONSTRATE A POTENTIAL PATH FORWARD FOR DEMONSTRATION. THIS TECHNOLOGY HAS THE POTENTIAL TO BE AN ALTERNATIVE METHOD FOR SYNTHESIS OF COMMERCIAL HYDROGEN PEROXIDE OR IN-SITU ONSITE DISINFECTION OF PROCESS WASTE STREAMS AND COULD BE AN INTEGRAL PART OF LONG TERM LIFE SUPPORT ON NASA'S MANNED SPACE MISSIONS. | $750K |
| Mar 20, 2017 | Department of DefenseFA8222 AFSC OL H PZIE | FA822216C0006 | 541712 | IGF::OT::IGF SMALL BUSINESS INNOVATIVE RESEARCH (SBIR) PHASE II INTEGRATED ELECTROLYTIC CHROME STRIPPING | $374K |
| Oct 28, 2016 | Environmental Protection AgencyRTP PROC OPS DIVISION (RTPPOD) | EPD17006 | 541712 | IGF::OT::IGF 2015-2016 SBIR PHASE I AWARD - FARADAY TECHNOLOGY, INC | $100K |
| Sep 23, 2016 | Department of DefenseFA8501 OPL CONTRACTING AFSC/PZIO | FA850116P0047 | 541712 | IGF::OT::IGF PLATING OF ZN-NI ON ALUMINUM AND STEEL | $150K |
| Aug 1, 2016 | Department of DefenseW6QK ACC-PICA | W15QKN16C0070 | 541712 | IGF::OT::IGF MULTIPHYSICS BASED TOOL DESIGN FOR ELECTROCHEMICAL MACHINING, SBIR PHASE I. | $100K |
| Jun 28, 2016 | Department of DefenseFA8650 USAF AFMC AFRL PZL AFRL/PZL | FA865016M5065 | 541711 | IGF::OT::IGF PHASE I SBIR "NON DESTRUCTIVE EVALUATION OF URETHANE-EPOXY COATING SYSTEMS USING THE SCANNING KELVIN PROBE" | $150K |
| Jun 6, 2016 | National Aeronautics and Space AdministrationNASA SHARED SERVICES CENTER | NNX16CA43P | 541712 | IGF::OT::IGF IN THIS PHASE I SBIR PROGRAM, FARADAY WILL DEVELOP A CUSTOM BENCH-SCALE ELECTROCHEMICAL CELL INCORPORATING STATE OF THE ART ELECTROCATALYSTS IN A GAS-DIFFUSION ELECTRODE (GDE) SYSTEM TO SERVE AS PROOF-OF-CONCEPT OF THE SUITABILITY OF AN ELECTROCHEMICAL SYSTEM FOR IN SITU HYDROGEN PEROXIDE GENERATION, TO SERVE AS A DISINFECTANT SOLUTION FOR CREW CONTACT SURFACES IN SPACE VEHICLES. HYDROGEN PEROXIDE IS AN APPEALING DISINFECTANT DUE TO ITS LOW TOXICITY AND INNOCUOUS DECOMPOSITION PRODUCTS (I.E., WATER AND OXYGEN). FARADAY WILL CONSTRUCT A BENCH-SCALE ELECTROREACTOR TO INCORPORATE A CUSTOMFABRICATED GAS DIFFUSION CATHODE AND A COMMERCIAL MIXED-METAL OXIDE ANODE, WHICH WILL THEN BE USED IN HYDROGEN PEROXIDE GENERATION TESTS. ADVENTITIOUS HYDROGEN PEROXIDE CONSUMPTION AT THE ANODE WILL BE AVOIDED BY INCLUSION OF A SELECTIVE MEMBRANE BETWEEN THE ANODE AND CATHODE COMPARTMENTS. THE PERFORMANCE OF THIS ELECTROCHEMICAL GENERATION SYSTEM WILL BE ENHANCED THROUGH APPLICATION OF THE FARADAYIC PROCESS, WHICH INVOLVES PRECISE TUNING OF PULSED ELECTRICAL POTENTIALS APPLIED TO THE CATALYTIC ELECTRODES. THE SYSTEM WILL BE CHARACTERIZED BY THE PEROXIDE GENERATION RATE, THE MAXIMUM ACHIEVABLE PEROXIDE CONCENTRATION, AND THE MICROBIAL DISINFECTION CAPABILITY DEMONSTRATED BY THE SOLUTIONS GENERATED. THESE EFFORTS WILL PROVIDE A PLATFORM FOR SCALE-UP AND OPTIMIZATION EFFORTS IN PHASE II AND TRANSITION TO COMMERCIALIZATION IN PHASE III. | $125K |
| May 18, 2016 | Department of DefenseFA9453 AFRL RVK | FA945316M0466 | 541712 | IGF::OT::IGF ROBUST IONIC LIQUID ELECTROLYTES FOR REVERSIBLE ELECTROPLATING OF MIRRORS | $150K |
| Mar 15, 2016 | Department of DefenseFA8222 AFSC OL H PZIE | FA822216C0006 | 541712 | IGF::OT::IGF SMALL BUSINESS INNOVATIVE RESEARCH (SBIR) PHASE II INTEGRATED ELECTROLYTIC CHROME STRIPPING | $374K |
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