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Faraday Technology, INC.

$27M obligated·71 awards·3 agencies·3 NAICS

Federal Contracts

Showing contracts 5181 of 81 total. Sorted by action date, most recent first. Excludes $0 modifications.

DateAgencyPIIDNAICSDescriptionAmount
Apr 30, 2020National Aeronautics and Space AdministrationNASA SHARED SERVICES CENTERNNX17CJ12C541712IGF::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, 2020National Aeronautics and Space AdministrationNASA SHARED SERVICES CENTER80NSSC20C0070541715ENVIRONMENTAL CONTROL AND LIFE SUPPORT FOR SPACECRAFT AND HABITAT$289K
Aug 8, 2019National Aeronautics and Space AdministrationNASA SHARED SERVICES CENTER80NSSC19C0177541715DEVELOP 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, 2019Environmental Protection AgencyINFORMATION TECHNOLOGY ACQ DIV (ITA68HERD19C0023541715FARADAY TECHNOLOGY, INC. SBIR PHASE I$100K
Apr 24, 2019Environmental Protection AgencyINFORMATION TECHNOLOGY ACQ DIV (ITA68HERD19C0011541715FARADAY TECHNOLOGY, INC SBIR PHASE I$100K
Apr 17, 2019Department of DefenseFA8650 USAF AFMC AFRL PZL AFRL/PZLFA865019P5158541715SBIR I TOPIC AF191-096; LOW COST ELECTROCHEMICAL MACHINING (ECM) PROCESSES FOR AEROSPACE COMPONENTS$150K
Mar 20, 2019Department of DefenseMISSILE DEFENSE AGENCY (MDA)HQ014719C7065541715SBIR/STTR PHASE I RESEARCH&DEVELOPMENT: CARBON NANOTUBE COATINGS ON ELECTROCHEMICAL TEXTURED SURFACES FOR ADVANCED ADSORPTIVE BAFFLES$105K
Jan 30, 2019Department of DefenseFA9453 AFRL RVKFA945319P0573541715S3 PRGM - PASSIVE CATHODE DEVICE FOR SPACE PLASMA APPLICATIONS - AF TOPIC 18A-T011 - STTR 1 - BASIC$150K
Jan 9, 2019Department of DefenseFA8650 USAF AFMC AFRL PZL AFRL/PZLFA865019P2024541715SBIR PHASE I "ELECTROCHEMICAL APERTURE ENABLING FAST ACTIVATION OF LITHIUM-ION RESERVE BATTERIES"$150K
Dec 27, 2018Department of DefenseW6QK ACC-PICAW15QKN18C0010541715PHASE II ENHANCEMENT FOR TOPIC A16-013$501K
Sep 26, 2018National Aeronautics and Space AdministrationNASA SHARED SERVICES CENTER80NSSC18C0222541715AMONG 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, 2018Department of DefenseW4GG HQ US ARMY TACOMW56HZV18C0100541715IGF::OT::IGF PHASE I SBIR$105K
Jul 27, 2018National Aeronautics and Space AdministrationNASA SHARED SERVICES CENTER80NSSC18P2062541715SPACE-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, 2018Department of DefenseFA9453 AFRL RVKFA945317C0490541712IGF::OT::IGF ROBUST IONIC LIQUID ELECTROLYTES FOR REVERSIBLE ELECTROPLATING OF MIRRORS$187K
Nov 16, 2017Department of DefenseW6QK ACC-PICAW15QKN18C0010541715PHASE II ENHANCEMENT FOR TOPIC A16-013$496K
Sep 13, 2017Department of DefenseW6QK ACC-PICAW15QKN17C0079541712IGF::OT::IGF THIS IS A PHASE I SBIR CONTRACT FOR TOPIC A17-081.$99K
Aug 10, 2017Department of DefenseW6QK ACC-PICAW15QKN16C0070541712IGF::OT::IGF MULTIPHYSICS BASED TOOL DESIGN FOR ELECTROCHEMICAL MACHINING, SBIR PHASE I.$50K
Aug 7, 2017Department of DefenseFA8650 USAF AFMC AFRL PZL AFRL/PZLFA865017C5074541712IGF::OT::IGF NON DESTRUCTIVE EVAL. OF URETHANE-EPOXY COATING SYSTEMS$750K
Aug 3, 2017Department of DefenseFA9453 AFRL RVKFA945317C0490541712IGF::OT::IGF ROBUST IONIC LIQUID ELECTROLYTES FOR REVERSIBLE ELECTROPLATING OF MIRRORS$563K
Jun 8, 2017National Aeronautics and Space AdministrationNASA SHARED SERVICES CENTERNNX17CA30P541712IGF::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, 2017National Aeronautics and Space AdministrationNASA SHARED SERVICES CENTERNNX17CC44P541712IGF::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, 2017National Aeronautics and Space AdministrationNASA SHARED SERVICES CENTERNNX17CP39P541712IGF::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, 2017National Aeronautics and Space AdministrationNASA SHARED SERVICES CENTERNNX17CJ12C541712IGF::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, 2017Department of DefenseFA8222 AFSC OL H PZIEFA822216C0006541712IGF::OT::IGF SMALL BUSINESS INNOVATIVE RESEARCH (SBIR) PHASE II INTEGRATED ELECTROLYTIC CHROME STRIPPING$374K
Oct 28, 2016Environmental Protection AgencyRTP PROC OPS DIVISION (RTPPOD)EPD17006541712IGF::OT::IGF 2015-2016 SBIR PHASE I AWARD - FARADAY TECHNOLOGY, INC$100K
Sep 23, 2016Department of DefenseFA8501 OPL CONTRACTING AFSC/PZIOFA850116P0047541712IGF::OT::IGF PLATING OF ZN-NI ON ALUMINUM AND STEEL$150K
Aug 1, 2016Department of DefenseW6QK ACC-PICAW15QKN16C0070541712IGF::OT::IGF MULTIPHYSICS BASED TOOL DESIGN FOR ELECTROCHEMICAL MACHINING, SBIR PHASE I.$100K
Jun 28, 2016Department of DefenseFA8650 USAF AFMC AFRL PZL AFRL/PZLFA865016M5065541711IGF::OT::IGF PHASE I SBIR "NON DESTRUCTIVE EVALUATION OF URETHANE-EPOXY COATING SYSTEMS USING THE SCANNING KELVIN PROBE"$150K
Jun 6, 2016National Aeronautics and Space AdministrationNASA SHARED SERVICES CENTERNNX16CA43P541712IGF::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, 2016Department of DefenseFA9453 AFRL RVKFA945316M0466541712IGF::OT::IGF ROBUST IONIC LIQUID ELECTROLYTES FOR REVERSIBLE ELECTROPLATING OF MIRRORS$150K
Mar 15, 2016Department of DefenseFA8222 AFSC OL H PZIEFA822216C0006541712IGF::OT::IGF SMALL BUSINESS INNOVATIVE RESEARCH (SBIR) PHASE II INTEGRATED ELECTROLYTIC CHROME STRIPPING$374K

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