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Home/Contractors/Microlink Devices INC/contracts

Federal Contractor Profile

Microlink Devices INC

$57M obligated·54 awards·2 agencies·2 NAICS
OverviewContractsAgenciesNAICS

Federal Contracts

Showing award actions 51–72 of 72 funded award actions, most recent first.

Contracts with positive obligations
54
Funded award actions shown
72
Obligations shown
$57M
Awarding agencies
2

This table shows award actions with a positive obligation. Zero-dollar and negative-dollar actions, such as administrative changes and deobligations, are not displayed. Multiple award actions may belong to the same contract.

Award data as of June 11, 2026. Source: USAspending federal award records.

DateAgencyPIIDNAICSDescriptionAmount
Sep 20, 2017Department of DefenseFA9453 AFRL RVKFA945317C0421541712IGF::OT::IGF "FLEXIBLE, LIGHTWEIGHT SOLAR CELL WITH 40% EFFICIENCY FABRICATED BY EPITAXIAL LIFTOFF ADN WAFER BONDING"$188K
Sep 19, 2017Department of DefenseNAVAIR WARFARE CTR AIRCRAFT DIVN6833517C0269541712RESEARCH AND DEVELOPMENT SBIR PHASE IIE IGF::OT::IGF$450K
Sep 19, 2017Department of DefenseW6QK ACC-APG NATICKW911QY17P0297541712IGF::OT::IGF SBIR PHASE I R&D EFFORT: LIGHT WEIGHT FLEXIBLE SOLAR CELLS PERFORMANCE ENHANCED WITH NANOSTRUCTURES$100K
Aug 31, 2017Department of DefenseFA9453 AFRL RVKFA945317P0449541712IGF::OT::IGF IMPROVED RADIATION HARDNESS IN MULTIJUNCTION SOLAR CELLS USING WAVELENGTH SPECIFIC PHOTONIC STRUCTURES$150K
Jun 9, 2017National Aeronautics and Space AdministrationNASA SHARED SERVICES CENTERNNX17CC60P541712IGF::OT::IGF BY EPITAXIAL LATERAL OVERGROWTH (ELOG) AND SELECTIVE AREA GROWTH (SAG) IN NANOMETER SCALES, MICROLINK DEVICES WILL DEVELOP THE NEXT GENERATION OF MULTIJUNCTION SOLAR CELLS FOR SPACE APPLICATIONS. THE PROPOSED INNOVATION IS THE FIRST ATTEMPT TO USE ADVANCED SURFACE NANO-ENGINEERING TECHNOLOGIES TO CONTROL THE FORMATION, PROPAGATION AND ANNIHILATION MECHANISM OF EXTENDED DEFECTS INCLUDING DISLOCATIONS IN MULTIJUNCTION SOLAR CELLS. THERE IS SIGNIFICANT GAP BETWEEN THE THEORETICALLY CALCULATED EFFICIENCY OF MULTIJUNCTION SOLAR CELLS AND THE EXPERIMENTAL RESULTS. THAT EFFICIENCY GAP INCREASES WITH THE INCREASE OF NUMBER OF JUNCTIONS/SUBCELLS. MISFIT DISLOCATIONS CREATED DUE TO HIGH LATTICE MISMATCH BETWEEN SUBCELLS PLAY A MAJOR ROLE IN HAMPERING THE EFFICIENCY AND RELIABILITY OF SUCH DEVICES. A SUCCESSFUL IMPLEMENTATION OF NANO-ELOG IN SOLAR CELLS WILL RESULTS IN 3J SOLAR CELLS WITH SIGNIFICANTLY REDUCED DISLOCATION DENSITY, RESULTING IN AN IMPROVED VOC AND ISC AND CONVERSATION EFFICIENCIES OF THE CELLS. THEREFORE, MLD CAN UTILIZE THIS METHOD TO GROW DEVICES WITH INCREASED NUMBER OF JUNCTIONS TO REACH PRACTICAL EFFICIENCIES CLOSE TO 40% (6J) FROM THE CURRENT 30% (IN COMMERCIALLY AVAILABLE 3J CELLS) IN AM0 AND 1SUN CONDITIONS. IT IS IMPORTANT TO EXPLORE, AND CONSEQUENTLY, TAKE ADVANTAGE OF THE LATEST NANO-PATTERNING DEVELOPMENTS FOR NASA'S PHOTOVOLTAIC DEVICES.$125K
Jun 9, 2017National Aeronautics and Space AdministrationNASA SHARED SERVICES CENTERNNX17CC61P541712IGF::OT::IGF MICROLINK PROPOSES TO DEVELOP AND TEST, A NEW TYPE OF PHOTOVOLTAIC MODULE THAT WILL BE SUITABLE FOR USE IN SMALLSAT AND CUBESAT PLATFORMS REQUIRING MAXIMUM POWER IN A HIGHLY STOWABLE FORMAT. MICROLINK PROPOSES TO ASSEMBLE AND TEST A COMPLETED SERIES ARRAY OF FIVE 20 CM2 CELLS THAT WILL OUTPUT IN EXCESS OF 3.5 W WHILE DEMONSTRATING A PATHWAY FOR PRODUCING SIGNIFICANTLY LARGER ARRAYS CAPABLE OF OUTPUTTING POWERS IN EXCESS OF 100 W. THE TYPICAL AREAL WEIGHT OF CONVENTIONAL GE-BASED SPACE CELLS WITH A 5 MIL THICK RIGID COVERGLASS EXCEEDS 1,000 G/M2. MICROLINK'S PROPOSED FLEXIBLE PHOTOVOLTAIC MODULE WITH ULTRA-THIN ELO SOLAR CELLS AND FLEXIBLE COVERGLASS MATERIAL WILL NOT ONLY BE FLEXIBLE AND COMPARABLE IN EFFICIENCY TO GE-BASED CELLS BUT ALSO HAVE AN AREAL MASS OF LESS THAN 400 G/M2. THIS REPRESENTS GREATER THAN A 60% REDUCTION IN WEIGHT WHICH IS OF PARTICULAR IMPORTANCE FOR SMALLSAT AND CUBESAT APPLICATIONS.$125K
Jun 8, 2017National Aeronautics and Space AdministrationNASA SHARED SERVICES CENTERNNX17CC59P541712IGF::OT::IGF MICROLINK PROPOSES TO DEVELOP A PHOSPHIDE-BASED ELO-IMM FOUR-JUNCTION (4J) SOLAR CELL THAT WILL ENHANCE THE PERFORMANCE AND CAPABILITIES OF SOLAR PHOTOVOLTAIC ARRAYS FOR A VARIETY OF FUTURE NASA MISSIONS. RELATIVE TO STATE-OF-THE-ART INCUMBENT GAINP/GAINAS/GE 3J SPACE SOLAR CELLS, THE PROPOSED PHOSPHIDE-BASED 4J SOLAR CELL HAS SUPERIOR RADIATION TOLERANCE, HIGHER BEGINNING-OF-LIFE (BOL) AND END-OF-LIFE (EOL) EFFICIENCIES, LOWER AREAL MASS DENSITY, HIGHER SPECIFIC POWER, AND LOWER COST. THE IMPROVED RADIATION TOLERANCE IS ENABLED BY ELIMINATING ARSENIDE-BASED SUBCELLS IN FAVOR OF ONLY PHOSPHIDE-BASED SUBCELLS. A REDUCTION IN THE MASS OF THE SOLAR CELL RELATIVE TO INCUMBENT TECHNOLOGY IS ENABLED BY REMOVAL OF THE THICK GAAS SUBSTRATE. COST SAVINGS COMPARED TO INCUMBENT TECHNOLOGY ARE ENABLED BY THE RECOVERY AND REUSE OF THE SUBSTRATE VIA THE ELO PROCESS. THE SUPERIOR RADIATION TOLERANCE CAN ALSO RELAX THE REQUIREMENTS FOR RADIATION SHIELDING, ENABLING FURTHER REDUCTIONS IN ARRAY MASS AND STOWED VOLUME.$125K
May 16, 2017Department of DefenseFA9453 AFRL RVKFA945317C0421541712IGF::OT::IGF "FLEXIBLE, LIGHTWEIGHT SOLAR CELL WITH 40% EFFICIENCY FABRICATED BY EPITAXIAL LIFTOFF ADN WAFER BONDING"$563K
Apr 12, 2017Department of DefenseNAVAIR WARFARE CTR AIRCRAFT DIVN6833516C0238541712STTR PI R&D. IGF::OT::IGF$70K
Oct 18, 2016Department of DefenseNAVAIR WARFARE CTR AIRCRAFT DIVN6833516C0106541712RESEARCH AND DEVELOPMENT IGF::OT::IGF$380K
Jun 23, 2016National Aeronautics and Space AdministrationNASA SHARED SERVICES CENTERNNX14CC06C541712IGF::OT::IGF MICROLINK DEVICES WILL INCREASE THE EFFICIENCY OF MULTI-JUNCTION SOLAR CELLS BY DESIGNING AND DEMONSTRATING ADVANCED ANTI-REFLECTION COATINGS (ARCS) THAT WILL PROVIDE A BETTER BROADBAND SPECTRAL RESPONSE THAN THAT OF CONVENTIONAL ANTI-REFLECTION COATINGS. ADVANCED COATINGS OF THIS NATURE ARE NEEDED TO REALIZE THE FULL PERFORMANCE OF THE FORTHCOMING GENERATION OF MULTI-JUNCTION SOLAR CELLS, WHICH WILL CONTAIN FOUR OR MORE JUNCTIONS. TWO APPROACHES TO IMPROVING THE PERFORMANCE OF THE ANTIREFLECTION COATINGS WILL BE INVESTIGATED: * DEVELOP MULTILAYER DIELECTRIC ANTIREFLECTION COATINGS INCORPORATING LATIO3 TO ACHIEVE SIGNIFICANTLY IMPROVED OPTICAL COUPLING BETWEEN THE COVERGLASS AND CELL AT THE ULTRAVIOLET AND INFRARED ENDS OF THE SPECTRAL RANGE OF INTEREST; AND * DEVELOP A STRUCTURE AND CORRESPONDING FABRICATION PROCESS TO OXIDIZE THE AL-CONTAINING WINDOW LAYER IN ORDER TO REDUCE THE ABSORPTION OF LIGHT AT THE SHORT-END OF THE SPECTRAL RANGE OF INTEREST, THUS PROVIDING EXTRA USEABLE PHOTONS TO THE CELL. THESE TWO TECHNOLOGIES WILL BE INTEGRATED INTO A HYBRID DESIGN WHICH WILL PROVIDE THE BEST POSSIBLE COUPLING OF LIGHT FROM COVER GLASS TO CELL IN ORDER TO ACHIEVE THE HIGHEST POSSIBLE EFFICIENCY IN NEXTGENERATION DEVICES CONTAINING FOUR OR MORE JUNCTIONS. IT IS EXPECTED THAT THE NEW COATINGS WILL ENABLE A RELATIVE EFFICIENCY INCREASE OF AT LEAST 7%, CORRESPONDING TO A 2.5% ABSOLUTE EFFICIENCY INCREASE. THE RELIABILITY AND RADIATION TOLERANCE OF THESE MATERIALS AND THE SOLAR CELLS INCORPORATING THE NEW DESIGNS WILL BE TESTED.$125K
Jun 23, 2016National Aeronautics and Space AdministrationNASA SHARED SERVICES CENTERNNX14CS57C541712IGF::OT::IGF THE GOAL OF THE PROGRAM IS TO REDUCE THE COST OF SUBSTRATE RECLAIM FOR HIGH-EFFICIENCY SOLAR CELLS FABRICATED BY AN EPITAXIAL LIFT-OFF (ELO) PROCESS, AND TO INCREASE THE NUMBER OF REUSE CYCLES FOR A GIVEN SUBSTRATE. IF SUCCESSFUL, THIS WILL RESULT IN A REDUCTION IN THE COST OF GAAS-BASED MULTI-JUNCTION SOLAR CELLS, IN WHICH THE COST OF THE SUBSTRATE ACCOUNTS FOR APPROXIMATELY 50% OF THE TOTAL COST. THE COST REDUCTION IS ACHIEVED BY INTRODUCING A NEW MULTI-LAYER ETCH-STOP STRUCTURE INTO A INVERTED METAMORPHIC (IMM) TRIPLE-JUNCTION CELL. THE ETCH-STOP STRUCTURE IS GROWN BETWEEN THE ORIGINAL GAAS SUBSTRATE AND THE ELO RELEASE LAYER, THEREBY BECOMING THE EFFECTIVE SUBSTRATE SURFACE AFTER THE ELO PROCESS. THE ETCH-STOP STRUCTURE PREVENTS PITS AND SURFACE DAMAGE THAT OCCUR DURING ELO FROM DAMAGING THE SURFACE OF THE GAAS SUBSTRATE. THE STANDARD METHOD OF RECLAIMING THE GAAS SUBSTRATE AFTER ELO IS TO EMPLOY CHEMO-MECHANICAL POLISHING (CMP) TO REMOVE THE DEFECT-RIDDEN GAAS SURFACE AND CHEMICALLY POLISH THE UNDERLYING GAAS TO YIELD A SURFACE THAT IS SUITABLE FOR EPITAXIAL GROWTH. THE CMP PROCESS WORKS BUT REDUCES THE SUBSTRATE THICKNESS AND CAUSES MINOR WAFER DAMAGE ITSELF, WHICH REQUIRES FURTHER POLISHING. THESE FACTORS ACCUMULATE, IN PRACTICE LIMITING THE NUMBER OF RECLAIM CYCLES TO 5 - 10 FOR A GIVEN SUBSTRATE. WITH THE INCORPORATION OF THE PROPOSED ETCH-STOP STRUCTURE, THE DEFECTS ARE ISOLATED IN THE ETCH-STOP STRUCTURE, WHICH CAN BE DISSOLVED BY SUCCESSIVE SELECTIVE WET CHEMICAL ETCHES TO PRODUCE THE ORIGINAL PRISTINE GAAS SURFACE ON A SUBSTRATE OF THE ORIGINAL THICKNESS. ALL MECHANICAL POLISHING IS ELIMINATED IN THIS PROPOSED WORK, ENSURING A CONSTANT SUBSTRATE THICKNESS THROUGH REPEATED SUBSTRATE RECLAIM CYCLES AND REDUCING THE ESTIMATED COST OF THE RECYCLING PROCESS TO<$1 PER SUBSTRATE. THE PHASE I PROGRAM DEMONSTRATED THAT THIS METHOD FOR SUBSTRATE RECLAIM WORKS; IN PHASE II WE WILL DEVELOP THE RECLAIM INTO AN OPTIMIZED BATCH PROCESS.$125K
May 31, 2016National Aeronautics and Space AdministrationNASA SHARED SERVICES CENTERNNX16CC38P541712IGF::OT::IGF DOUBLE EPITAXIAL LIFT-OFF (D-ELO) IN CONJUNCTION WITH SEMICONDUCTOR BONDING WILL BE LEVERAGED TO PRODUCE 38% EFFICIENT SIX-JUNCTION SOLAR CELLS. THESE SOLAR CELLS WILL ENABLE OPTIMAL PERFORMANCE FOR FUTURE NASA MISSIONS THAT REQUIRE SOLAR CELLS WITH HIGH SPECIFIC POWER, HIGH POWER CONVERSION EFFICIENCY, AND LOWER COST THAN THE INCUMBENT SOLAR CELL TECHNOLOGY. HIGH EFFICIENCY IS ENABLED BY THE USE OF SIX AM0 SPECTRUM-MATCHED SUBCELL JUNCTIONS. A REDUCTION IN MASS COMPARED TO INCUMBENT TECHNOLOGY IS ENABLED BY REMOVAL OF THE THICK SEMICONDUCTOR SUBSTRATES WHILE A COST SAVINGS COMPARED TO INCUMBENT TECHNOLOGY IS ENABLED BY THE RECOVERY AND SUBSEQUENT REUSE OF THE EXPENSIVE SEMICONDUCTOR SUBSTRATES VIA THE D-ELO PROCESS.$125K
May 31, 2016National Aeronautics and Space AdministrationNASA SHARED SERVICES CENTERNNX16CC50P541712IGF::OT::IGF THE PROPOSED INNOVATION WILL DRAMATICALLY IMPROVE THE PERFORMANCE OF TRITIUM-POWERED BETAVOLTAIC BATTERIES THROUGH THE DEVELOPMENT OF AN ULTRA THIN P ON N JUNCTION COMPOSED OF INDIUM GALLIUM PHOSPHIDE COUPLED TO A THIN FILM METAL TRITIDE. THE THIN CELL WILL BE BUILT USING MICROLINK'S SIGNATURE EPITAXIAL LIFT OFF TECHNOLOGY AND STANDARD METALORGANIC CHEMICAL VAPOR DEPOSITION (MOCVD) ALONG WITH CITY LABS' TRITIUM BETAVOLTAIC EXPERTISE. THE PROPOSED BETAVOLTAIC P/N JUNCTION CAN BE STACKED IN A BOX OR ROLLED INTO A CYLINDER AND WILL PROVIDE A COST SAVING OF UP TO 90%, WHILE INCREASING ENERGY DENSITY TO UP TO TWENTY TIMES THAT OF LITHIUM BATTERIES. SUCH AN ADVANCED SEMICONDUCTOR DEVICE WILL PRODUCE MUCH HIGHER POWER OUTPUTS THAN ARE POSSIBLE WITH EXISTING STATE-OF-THE-ART DEVICES AS ILLUSTRATED IN THE FIGURE. IT WILL PROVIDE THE BATTERY A LIFE SPAN IN EXCESS OF 20 YEARS WITH THE BROAD-RANGE TEMPERATURE-INSENSITIVITY BENEFITS NORMALLY ASSOCIATED WITH BETAVOLTAICS. THIS INCREASED POWER/ENERGY DENSITY FOR TRITIUM BETAVOLTAICS WILL OPEN UP PATHWAYS FOR SIGNIFICANT ADVANCES IN POWER SOLUTIONS FOR DIMINUTIVE SIZED, LOW-POWER MICROELECTRONIC DEVICES THAT MAY BE USED IN CUBESAT AND IN-SPACE POWER SYSTEMS. EXAMPLE APPLICATIONS INCLUDE MICROWATT-TO-MILLIWATT AUTONOMOUS 20+ YEAR SENSORS/MICROELECTRONICS FOR USE IN STRUCTURAL MONITORING, MESH NETWORKS, TAGGING AND TRACKING WIRELESS SENSORS, MEDICAL DEVICE IMPLANTS, AND DEEP SPACE POWER WHERE SOLAR IS NOT EASILY AVAILABLE. TRITIUM BETAVOLTAICS ARE CAPABLE OF ADDRESSING THIS POWER NICHE FOR DEVICES REQUIRING RELIABLE, UNINTERRUPTED POWER THROUGH EXTREMES OF TEMPERATURE, LONGEVITY AND DIMINUTIVE FORM FACTORS WHERE TRADITIONAL BATTERIES CANNOT OPERATE.$125K
May 24, 2016National Aeronautics and Space AdministrationNASA SHARED SERVICES CENTERNNX16CL73P541712IGF::OT::IGF MICROLINK DEVICES PROPOSES TO INTEGRATE ITS HIGH-EFFICIENCY, LIGHTWEIGHT, AND FLEXIBLE SOLAR SHEET TECHNOLOGY TO A SMALL UNMANNED AIRCRAFT SYSTEM (UAS) THAT WILL DEMONSTRATE A PATHWAY TO LONG ENDURANCE FLIGHTS FOR SEVERAL WEEKS. THIS WILL BE A BREAKTHROUGH TECHNOLOGY THAT WILL ENHANCE THE PERFORMANCE AND UTILITY OF NASA'S AIRBORNE SCIENCE FLEET UAS. IN PREVIOUS WORK, MICROLINK HAS DEMONSTRATED THAT ITS UNIQUE SOLAR SHEET TECHNOLOGY ENABLES SIGNIFICANT EXTENSION OF FLIGHT FOR SMALL BATTERY-OPERATED UAS PLATFORMS. FURTHER REFINEMENT OF THIS SOLAR TECHNOLOGY AND WORKING IN CLOSE COLLABORATION WITH THE SMALL UAS MANUFACTURER TO OPTIMIZE THE UAS PLATFORM FOR LONG ENDURANCE FLIGHT WILL ALLOW FLIGHT TIMES EVEN GREATER THAN FIRST DEMONSTRATED IN PROTOTYPE EXPERIMENTS. THIS PROJECT WILL LEVERAGE MICROLINKS RECENT ADVANCES IN INVERTED METAMORPHIC (IMM) MULTI-JUNCTION (ELO) SOLAR CELL TECHNOLOGY. THE UNIQUE NATURE OF THE ELO SOLAR CELLS HAS GIVEN RISE TO NEW OPPORTUNITIES FOR SOLAR CELL PACKAGING: THE INHERENT PHYSICAL FLEXIBILITY OF THESE HIGH EFFICIENCY SOLAR CELLS CAN BE EXPLOITED IN THE MANUFACTURE OF A NEW GENERATION OF PHOTOVOLTAIC (PV) BLANKETS THAT ARE LIGHTWEIGHT, FLEXIBLE, AND MODULAR. RECENT WORK HAS DEVELOPED A SOLAR CELL DEVICE AND SOLAR SHEET ENCAPSULATION PROCESS THAT IS ALMOST 50% THE WEIGHT OF EARLIER SOLAR CELLS AND SHEETS FIRST USED ON THE SMALL UAS DEMONSTRATIONS WHILE STILL MAINTAINING THE HIGH-EFFICIENCY OF EARLIER DEVICES. THE RESULT RESULTING MODULAR HIGH-EFFICIENCY SOLAR SHEETS ARE AN IDEAL CANDIDATE AND SOLUTION FOR MAXIMUM POWER GENERATION IN A LIMITED AREA AND WITHIN WEIGHT CONSTRAINTS SUCH AS AIR VEHICLE APPLICATIONS.$125K
May 11, 2016Department of DefenseNAVAIR WARFARE CTR AIRCRAFT DIVN6833516C0238541712STTR PI R&D. IGF::OT::IGF$80K
Apr 28, 2016National Aeronautics and Space AdministrationNASA SHARED SERVICES CENTERNNX16CC16C541712IGF::OT::IGF IN THIS PHASE II PROGRAM WE PROPOSE TO DEVELOP A MANUFACTURABLE PRODUCTION PROCESS TO INTRODUCE BACKSIDE CONTACTS TO MICROLINK DEVICES? LARGE-AREA, MULTIJUNCTION EPITAXIAL LIFT-OFF (ELO) SOLAR CELLS. WE WILL ALSO DEVELOP NEW ASSEMBLY PROCESSES TO FABRICATE FLEXIBLE KAPTON SHEETS WITH BACKSIDE CONTACT ELO SOLAR CELLS. THIS ENABLES AN IMPORTANT PATH FOR COST REDUCTION USING FULLY AUTOMATED LAYDOWN AND INTERCONNECT OF SOLAR PANELS. THE NEW BACKSIDE CONTACT ELO SOLAR CELL TECHNOLOGY HAS POTENTIAL BENEFITS FOR FUTURE NASA SOLAR ELECTRIC PROPULSION (SEP) PROGRAMS USING VERY LARGE SOLAR CELL ARRAYS. BACKSIDE CONTACTS ARE USED IN THE HIGHEST EFFICIENCY SILICON SOLAR CELLS MANUFACTURED BY SUNPOWER (>24% EFFICIENCY IN PRODUCTION) BUT HAVE NEVER BEEN SUCCESSFULLY APPLIED COMMERCIALLY TO MULTIJUNCTION SOLAR CELLS. BENEFITS FOR LARGE-AREA SPACE SOLAR CELL INCLUDE: HIGHER DEVICE EFFICIENCY BY REDUCING TOPSIDE GRID SHADOW AND RESISTIVE LOSSES, NEW APPROACHES FOR PANEL ASSEMBLY BY PLACING CONTACTS ON BACKSIDE OF SOLAR CELL, AND REDUCED ARCING IN HIGH-VOLTAGE ARRAYS BY ELIMINATING TOPSIDE INTERCONNECTS. THE PROPOSED TECHNOLOGY BUILDS ON MICROLINK DEVICES? LOW-COST, LIGHTWEIGHT ELO SOLAR CELL TECHNOLOGY AND PREVIOUS EXPERIENCE WITH BACKSIDE CONTACT SOLAR CELLS FOR CPV APPLICATIONS.$750K
Apr 27, 2016Department of DefenseCOMMANDERM6785416C6509541712IGF::OT::IGF SBIR PHASE I RESEARCH AND DEVELOPMENT$80K
Apr 12, 2016Department of DefenseFA9453 AFRL RVKFA945315C0404541712IGF::OT::IGF STTR 2 - QUANTUM AND NANOSTRUCTURE LIFT OFF SOLAR CELLS$370K
Mar 15, 2016Department of DefenseW6QK ACC-APG ADELPHIW911QX15C0003541712IGF::OT::IGF PHASE II A13-020 MICROLINK$500K
Mar 1, 2016Department of DefenseNAVAIR WARFARE CTR AIRCRAFT DIVN6833516C0106541712RESEARCH AND DEVELOPMENT IGF::OT::IGF$375K
Feb 23, 2016Department of DefenseFA9453 AFRL RVKFA945315C0404541712IGF::OT::IGF STTR 2 - QUANTUM AND NANOSTRUCTURE LIFT OFF SOLAR CELLS$555K

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