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Federal Contractor Profile

Aosense, INC.

$55M obligated·67 awards·5 agencies·7 NAICS

Federal Contracts

Showing award actions 51–100 of 132 funded award actions, most recent first.

Contracts with positive obligations
67
Funded award actions shown
132
Obligations shown
$55M
Awarding agencies
5

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 July 17, 2026. Source: USAspending federal award records.

DateAgencyPIIDNAICSDescriptionAmount
Jul 29, 2019National Aeronautics and Space AdministrationNASA GODDARD SPACE FLIGHT CENTERNNG14CR61C541712IGF::OT::IGF SBIR PHASE III AWARD. PHASE I/II AWARDED UNDER NNX13CG02C COLD ATOM GRAVITY GRADIOMETER FOR GEODESY: THE CONTRACTOR SHALL DESIGN, CONSTRUCT, AND OPTIMIZE A HIGH-PERFORMANCE GRAVITY GRADIOMETER BASED ON LIGHT-PULSE ATOM INTERFEROMETRY. THE CONTRACTOR SHALL BUILD AND TEST A SECOND PROTOTYPE ZERO-DEAD-TIME (ZDT) ABSOLUTE GRAVIMETER. THE INSTRUMENTS IN THIS PHASE III EFFORT TAKES ADVANTAGE OF TECHNOLOGIES DEVELOPED UNDER NASA SBIR PHASE I AND PHASE II PROGRAMS.$134K
May 22, 2019Department of DefenseOFFICE OF NAVAL RESEARCHN0001418C1028541715SENSORS FOR ATOMIC INERTIAL NAVIGATION AND TIMING (SAINT)$5K
May 1, 2019Department of DefenseOFFICE OF NAVAL RESEARCHN0001418C1028541715SENSORS FOR ATOMIC INERTIAL NAVIGATION AND TIMING (SAINT)$255K
Apr 4, 2019Department of DefenseFA9453 AFRL RVKFA945318C0024541715IGF::OT::IGF "COMPACT PERCISION ATOMIC CLOCK"$19K
Feb 14, 2019National Aeronautics and Space AdministrationNASA GODDARD SPACE FLIGHT CENTERNNG14CR61C541712IGF::OT::IGF SBIR PHASE III AWARD. PHASE I/II AWARDED UNDER NNX13CG02C COLD ATOM GRAVITY GRADIOMETER FOR GEODESY: THE CONTRACTOR SHALL DESIGN, CONSTRUCT, AND OPTIMIZE A HIGH-PERFORMANCE GRAVITY GRADIOMETER BASED ON LIGHT-PULSE ATOM INTERFEROMETRY. THE CONTRACTOR SHALL BUILD AND TEST A SECOND PROTOTYPE ZERO-DEAD-TIME (ZDT) ABSOLUTE GRAVIMETER. THE INSTRUMENTS IN THIS PHASE III EFFORT TAKES ADVANTAGE OF TECHNOLOGIES DEVELOPED UNDER NASA SBIR PHASE I AND PHASE II PROGRAMS.$54K
Jan 9, 2019Department of DefenseOFFICE OF NAVAL RESEARCHN0001418C1028541715SENSORS FOR ATOMIC INERTIAL NAVIGATION AND TIMING (SAINT)$1.0M
Oct 24, 2018National Aeronautics and Space AdministrationNASA GODDARD SPACE FLIGHT CENTERNNG14CR61C541712IGF::OT::IGF SBIR PHASE III AWARD. PHASE I/II AWARDED UNDER NNX13CG02C COLD ATOM GRAVITY GRADIOMETER FOR GEODESY: THE CONTRACTOR SHALL DESIGN, CONSTRUCT, AND OPTIMIZE A HIGH-PERFORMANCE GRAVITY GRADIOMETER BASED ON LIGHT-PULSE ATOM INTERFEROMETRY. THE CONTRACTOR SHALL BUILD AND TEST A SECOND PROTOTYPE ZERO-DEAD-TIME (ZDT) ABSOLUTE GRAVIMETER. THE INSTRUMENTS IN THIS PHASE III EFFORT TAKES ADVANTAGE OF TECHNOLOGIES DEVELOPED UNDER NASA SBIR PHASE I AND PHASE II PROGRAMS.$15K
Sep 27, 2018National Aeronautics and Space AdministrationNASA GODDARD SPACE FLIGHT CENTERNNG14CR61C541712IGF::OT::IGF SBIR PHASE III AWARD. PHASE I/II AWARDED UNDER NNX13CG02C COLD ATOM GRAVITY GRADIOMETER FOR GEODESY: THE CONTRACTOR SHALL DESIGN, CONSTRUCT, AND OPTIMIZE A HIGH-PERFORMANCE GRAVITY GRADIOMETER BASED ON LIGHT-PULSE ATOM INTERFEROMETRY. THE CONTRACTOR SHALL BUILD AND TEST A SECOND PROTOTYPE ZERO-DEAD-TIME (ZDT) ABSOLUTE GRAVIMETER. THE INSTRUMENTS IN THIS PHASE III EFFORT TAKES ADVANTAGE OF TECHNOLOGIES DEVELOPED UNDER NASA SBIR PHASE I AND PHASE II PROGRAMS.$9K
Sep 27, 2018National Aeronautics and Space AdministrationNASA SHARED SERVICES CENTERNNX16CG66C541712IGF::OT::IGF AOSENSE WILL BUILD AND TEST AN INTEGRATED ULTRASTABLE LASER MODULE CAPABLE OF REACHING A SHORT-TERM INSTABILITY OF<5E-15 @ 1S. THE FLEXIBLE DESIGN WILL ALLOW THE MODULE TO BE ADAPTED FOR SEVERAL RELEVANT OPTICAL CLOCK WAVELENGTHS WHICH UTILIZE EXTERNAL CAVITY DIODE LASERS. THE FIRST UNIT WILL OPERATE AT 698 NM TO ADDRESS THE SR CLOCK TRANSITION.$500K
Aug 24, 2018National Aeronautics and Space AdministrationNASA SHARED SERVICES CENTER80NSSC18C0158541715ATOM INTERFEROMETRY GRAVITY GRADIOMETER (AIGG) IS ENABLING TECHNOLOGY IN THE FIELD OF ORBITAL GRAVITATIONAL MAPPING OF EARTH AND PLANETARY TARGETS. THESE DEVICES ENABLE MEASUREMENTS WAY BEYOND CLASSICAL DEVICES. SPECIFICALLY CENTRAL PART OF ATOM INTERFEROMETRY RELIES ON TWO PHOTON BRAGG PROCESS. THE ADVANCEMENTS IN PHASE II-X SBIR ALLOWS FABRICATION OF STABILIZED COMPACT LASER AT 852 NM. THIS PHASE II-X LASER WILL BE INTEGRATED INTO A FUNCTIONAL INSTRUMENT (AIGG) TO PERFORM FUNCTIONAL TESTING. THE INTEGRATION OF THIS LASER WILL ENABLE THE AIGG TO ACHIEVE HIGH SPATIAL RESOLUTION, HIGH SENSITIVITIES AND SPECTRAL PURITY REQUIRED FOR THE NEXT GENERATION EARTH AND PLANETARY SCIENCE APPLICATIONS.$250K
Aug 1, 2018Department of DefenseNAVAIR WARFARE CTR AIRCRAFT DIVN6833518C0557541715PROGRESS REPORT$125K
Jul 25, 2018National Aeronautics and Space AdministrationNASA SHARED SERVICES CENTER80NSSC18P2050541715AOSENSE PROPOSES TO DEVELOP LASER AMPLIFIER MODULES FOR COLD-ATOM OPTICAL SYSTEMS. THE DEVICE WOULD DELIVER>1 W OF OPTICAL POWER AT 852 NM BY FIBER WHEN PAIRED WITH AN APPROPRIATE NARROW-LINEWIDTH MASTER LASER OSCILLATOR. A KEY FEATURE IS THE INTEGRATION OF A TAPERED AMPLIFIER WITH AOSENSE-PROPRIETARY COMPACT, HIGH-TRANSMISSION OPTICAL ISOLATORS, YIELDING A FIBER-IN, FIBER-OUT PACKAGE WITH DIMENSIONS OF 50 MM X 50 MM X 35 MM OR SMALLER. THIS AMPLIFIER MODULE HAS BROAD APPLICABILITY TO ATOM INTERFEROMETERS AND ATOMIC CLOCKS, BUT IT WOULD BE PARTICULARLY USEFUL FOR HIGH-PERFORMANCE ORBITAL SENSORS LIKE ATOM INTERFEROMETER GRAVITY GRADIOMETERS (AIGGS). SUCH SYSTEMS WILL LIKELY UTILIZE ADVANCED ATOM-OPTIC LASER PULSE SEQUENCES, WHICH REQUIRE MORE LASER POWER TO MITIGATE ATOM LOSSES AND ACHIEVE HIGH SENSITIVITY.$124K
Jul 10, 2018Department of the InteriorIBC ACQ SERVICES DIVISION (00063)140D6318C0017541715IGF::OT::IGF - DARPA-BAA-HR001117S0025 AMBIIENT PROGRAM - RESEARCH AND DEVELOPMENT CONTRACT MICROSYSTEMS TECHNOLOGY OFFICE$1.2M
Jun 27, 2018Department of DefenseFA9453 AFRL RVKFA945318C0024541715IGF::OT::IGF "COMPACT PERCISION ATOMIC CLOCK"$240K
Jun 22, 2018Department of DefenseNAVAL INFORMATION WARFARE SYSTEMSN0003918C0011541715VAPOR WITH PULSED OPTICAL READOUT CLOCK$2.9M
May 24, 2018Department of DefenseOFFICE OF NAVAL RESEARCHN0001418C1028541715SENSORS FOR ATOMIC INERTIAL NAVIGATION AND TIMING (SAINT)$548K
May 8, 2018National Aeronautics and Space AdministrationNASA SHARED SERVICES CENTER80NSSC18C0034541715PRECISION NAVIGATION AND TIMING (PNT) IS A CRITICAL RESOURCE FOR GOVERNMENT AND COMMERCIAL AEROSPACE. GIVEN THE HIGH LAUNCH COST AND SHIFT TOWARD SMALLER PAYLOADS, REDUCING THE SIZE, WEIGHT, AND POWER (SWAP) OF SPACE-BASED NAVIGATION SYSTEMS IS A CRITICAL NEED. ATOM-INTERFEROMETRIC INERTIAL SENSORS HAVE DEMONSTRATED SUPERIOR PERFORMANCE OVER CONVENTIONAL INERTIAL DEVICES OWING TO THE INTRINSIC STABILITY OF ATOMIC SYSTEMS. CENTRAL TO MAKING COLD ATOM SENSORS PRACTICAL IS THEIR ABILITY TO RELIABLY OPERATE FOR EXTENDED PERIODS WITHOUT USER INTERVENTION. CURRENT LASER DIODES, WHICH ARE AT THE HEART OF ATOMIC SENSORS, SUFFER FROM POWER DEGRADATION AND MODE HOPS ON TIMESCALES INCOMPATIBLE WITH LONG TERM DEPLOYMENT. BECAUSE THESE PROPERTIES ARE INHERENT TO THE DIODES, IT IS PRUDENT TO CIRCUMVENT THESE PROBLEMS WITH DIAGNOSTIC PROTOCOLS AIMED AT EARLY DETECTION AND ACTION. DIODES CLOSE TO MODE HOPPING CAN BE TEMPORARILY TAKEN OFFLINE TO TUNE AWAY THE MODE HOP VIA CURRENT AND TEMPERATURE. DIODES WITH DEGRADED POWER CAN BE TAKEN OFFLINE ENTIRELY IN FAVOR OF A HEALTHY DIODE. THIS APPROACH WILL PROVIDE A ROBUST, WAVELENGTH-AGNOSTIC TECHNIQUE TO DELIVER RELIABLE, LONG-LIVED LASER SOURCES AT ATOM SENSOR-RELEVANT WAVELENGTHS. AOSENSE PROPOSES TO DEVELOP A COLD ATOM LASER MODULE (CALM) CAPABLE OF SUPPORTING A BROAD RANGE OF ATOMIC SENSORS. DEVELOPMENT OF THE CALM LASER MODULE WILL RESULT IN A RUGGEDIZED AND RELIABLE LASER SOURCE CAPABLE OF AUTONOMOUSLY DRIVING AN ATOM-BASED SENSOR WITHIN THE SPACE ENVIRONMENT. SUCH AN EFFORT WOULD ENABLE SPACE-BASED APPLICATIONS FOR ATOMIC SENSORS SUCH AS IMUS, CLOCKS, AND MAGNETOMETERS, OPENING UP SIGNIFICANT MARKET OPPORTUNITIES IN THE DEFENSE AND COMMERCIAL SECTORS.$749K
Apr 23, 2018National Aeronautics and Space AdministrationNASA GODDARD SPACE FLIGHT CENTERNNG14CR61C541712IGF::OT::IGF SBIR PHASE III AWARD. PHASE I/II AWARDED UNDER NNX13CG02C COLD ATOM GRAVITY GRADIOMETER FOR GEODESY: THE CONTRACTOR SHALL DESIGN, CONSTRUCT, AND OPTIMIZE A HIGH-PERFORMANCE GRAVITY GRADIOMETER BASED ON LIGHT-PULSE ATOM INTERFEROMETRY. THE CONTRACTOR SHALL BUILD AND TEST A SECOND PROTOTYPE ZERO-DEAD-TIME (ZDT) ABSOLUTE GRAVIMETER. THE INSTRUMENTS IN THIS PHASE III EFFORT TAKES ADVANTAGE OF TECHNOLOGIES DEVELOPED UNDER NASA SBIR PHASE I AND PHASE II PROGRAMS.$150K
Mar 26, 2018Department of the InteriorIBC ACQ SERVICES DIVISION (00063)140D6318C0017541715IGF::OT::IGF - DARPA-BAA-HR001117S0025 AMBIIENT PROGRAM - RESEARCH AND DEVELOPMENT CONTRACT MICROSYSTEMS TECHNOLOGY OFFICE$242K
Mar 9, 2018National Aeronautics and Space AdministrationNASA GODDARD SPACE FLIGHT CENTERNNG14CR61C541712IGF::OT::IGF SBIR PHASE III AWARD. PHASE I/II AWARDED UNDER NNX13CG02C COLD ATOM GRAVITY GRADIOMETER FOR GEODESY: THE CONTRACTOR SHALL DESIGN, CONSTRUCT, AND OPTIMIZE A HIGH-PERFORMANCE GRAVITY GRADIOMETER BASED ON LIGHT-PULSE ATOM INTERFEROMETRY. THE CONTRACTOR SHALL BUILD AND TEST A SECOND PROTOTYPE ZERO-DEAD-TIME (ZDT) ABSOLUTE GRAVIMETER. THE INSTRUMENTS IN THIS PHASE III EFFORT TAKES ADVANTAGE OF TECHNOLOGIES DEVELOPED UNDER NASA SBIR PHASE I AND PHASE II PROGRAMS.$41K
Feb 28, 2018Department of DefenseFA8650 USAF AFMC AFRL PZL AFRL/PZLFA865013C7327541712IGF::OT::IGF CHIP SCALE COMBINATORAL ATOMIC NAVIGATOR CSCAN$455
Jan 26, 2018National Aeronautics and Space AdministrationNASA GODDARD SPACE FLIGHT CENTERNNG14CR61C541712IGF::OT::IGF SBIR PHASE III AWARD. PHASE I/II AWARDED UNDER NNX13CG02C COLD ATOM GRAVITY GRADIOMETER FOR GEODESY: THE CONTRACTOR SHALL DESIGN, CONSTRUCT, AND OPTIMIZE A HIGH-PERFORMANCE GRAVITY GRADIOMETER BASED ON LIGHT-PULSE ATOM INTERFEROMETRY. THE CONTRACTOR SHALL BUILD AND TEST A SECOND PROTOTYPE ZERO-DEAD-TIME (ZDT) ABSOLUTE GRAVIMETER. THE INSTRUMENTS IN THIS PHASE III EFFORT TAKES ADVANTAGE OF TECHNOLOGIES DEVELOPED UNDER NASA SBIR PHASE I AND PHASE II PROGRAMS.$125K
Jan 25, 2018Department of DefenseFA8650 USAF AFMC AFRL PZL AFRL/PZLFA865013C7327541712IGF::OT::IGF CHIP SCALE COMBINATORAL ATOMIC NAVIGATOR CSCAN$164K
Jan 9, 2018National Aeronautics and Space AdministrationNASA GODDARD SPACE FLIGHT CENTERNNG14CR61C541712IGF::OT::IGF SBIR PHASE III AWARD. PHASE I/II AWARDED UNDER NNX13CG02C COLD ATOM GRAVITY GRADIOMETER FOR GEODESY: THE CONTRACTOR SHALL DESIGN, CONSTRUCT, AND OPTIMIZE A HIGH-PERFORMANCE GRAVITY GRADIOMETER BASED ON LIGHT-PULSE ATOM INTERFEROMETRY. THE CONTRACTOR SHALL BUILD AND TEST A SECOND PROTOTYPE ZERO-DEAD-TIME (ZDT) ABSOLUTE GRAVIMETER. THE INSTRUMENTS IN THIS PHASE III EFFORT TAKES ADVANTAGE OF TECHNOLOGIES DEVELOPED UNDER NASA SBIR PHASE I AND PHASE II PROGRAMS.$60K
Dec 11, 2017Department of DefenseOFFICE OF NAVAL RESEARCHN0001415C5022541712IGF::CT::IGF ONRBAA15-001 LONG RANGE BROAD AGENCY ANNOUNCEMENT (BAA) FOR NAVY AND MARINE CORPS SCIENCE AND TECHNOLOGY$389K
Dec 10, 2017Department of the InteriorIBC ACQ SERVICES DIVISION (00063)140D6318C0017541715IGF::OT::IGF - DARPA-BAA-HR001117S0025 AMBIIENT PROGRAM - RESEARCH AND DEVELOPMENT CONTRACT MICROSYSTEMS TECHNOLOGY OFFICE$682K
Dec 6, 2017National Aeronautics and Space AdministrationNASA GODDARD SPACE FLIGHT CENTERNNG14CR61C541712IGF::OT::IGF SBIR PHASE III AWARD. PHASE I/II AWARDED UNDER NNX13CG02C COLD ATOM GRAVITY GRADIOMETER FOR GEODESY: THE CONTRACTOR SHALL DESIGN, CONSTRUCT, AND OPTIMIZE A HIGH-PERFORMANCE GRAVITY GRADIOMETER BASED ON LIGHT-PULSE ATOM INTERFEROMETRY. THE CONTRACTOR SHALL BUILD AND TEST A SECOND PROTOTYPE ZERO-DEAD-TIME (ZDT) ABSOLUTE GRAVIMETER. THE INSTRUMENTS IN THIS PHASE III EFFORT TAKES ADVANTAGE OF TECHNOLOGIES DEVELOPED UNDER NASA SBIR PHASE I AND PHASE II PROGRAMS.$120K
Sep 26, 2017National Aeronautics and Space AdministrationNASA GODDARD SPACE FLIGHT CENTERNNG14CR61C541712IGF::OT::IGF SBIR PHASE III AWARD. PHASE I/II AWARDED UNDER NNX13CG02C COLD ATOM GRAVITY GRADIOMETER FOR GEODESY: THE CONTRACTOR SHALL DESIGN, CONSTRUCT, AND OPTIMIZE A HIGH-PERFORMANCE GRAVITY GRADIOMETER BASED ON LIGHT-PULSE ATOM INTERFEROMETRY. THE CONTRACTOR SHALL BUILD AND TEST A SECOND PROTOTYPE ZERO-DEAD-TIME (ZDT) ABSOLUTE GRAVIMETER. THE INSTRUMENTS IN THIS PHASE III EFFORT TAKES ADVANTAGE OF TECHNOLOGIES DEVELOPED UNDER NASA SBIR PHASE I AND PHASE II PROGRAMS.$90K
Sep 26, 2017Department of DefenseW6QK ACC-RSAW31P4Q17C0109541712IGF::OT::IGF DARPA SBIR PHASE II FOR THE STATEMENT OF WORK ENTITLED, "CALCIUM SLOW BEAM OPTICAL CLOCK (CASBOC)."$750K
Aug 15, 2017Department of DefenseFA8650 USAF AFMC AFRL PZL AFRL/PZLFA865015C7531541712IGF::OT::IGF STOIC - RACK-MOUNT OPTICAL CLOCK (ROC)$1.3M
Jul 31, 2017National Aeronautics and Space AdministrationNASA GODDARD SPACE FLIGHT CENTERNNG14CR61C541712IGF::OT::IGF SBIR PHASE III AWARD. PHASE I/II AWARDED UNDER NNX13CG02C COLD ATOM GRAVITY GRADIOMETER FOR GEODESY: THE CONTRACTOR SHALL DESIGN, CONSTRUCT, AND OPTIMIZE A HIGH-PERFORMANCE GRAVITY GRADIOMETER BASED ON LIGHT-PULSE ATOM INTERFEROMETRY. THE CONTRACTOR SHALL BUILD AND TEST A SECOND PROTOTYPE ZERO-DEAD-TIME (ZDT) ABSOLUTE GRAVIMETER. THE INSTRUMENTS IN THIS PHASE III EFFORT TAKES ADVANTAGE OF TECHNOLOGIES DEVELOPED UNDER NASA SBIR PHASE I AND PHASE II PROGRAMS.$209K
Jul 31, 2017Department of DefenseFA9453 AFRL RVKFA945317C0470541712IGF::OT::IGF "TRANSVERSELY-COOLED ATOMIC INERTIAL NAVIGATOR (TRAIN)"$750K
Jul 28, 2017Department of DefenseFA8650 USAF AFMC AFRL PZL AFRL/PZLFA865015C7531541712IGF::OT::IGF STOIC - RACK-MOUNT OPTICAL CLOCK (ROC)$290K
Jul 5, 2017Department of DefenseFA9453 AFRL RVKFA945316C0491541712IGF::OT::IGF SEVERE-ENVIRONMENT COLD-ATOM NAVIGATION TECHNOLOGIES$167K
Jun 30, 2017National Aeronautics and Space AdministrationNASA GODDARD SPACE FLIGHT CENTERNNG14CR61C541712IGF::OT::IGF SBIR PHASE III AWARD. PHASE I/II AWARDED UNDER NNX13CG02C COLD ATOM GRAVITY GRADIOMETER FOR GEODESY: THE CONTRACTOR SHALL DESIGN, CONSTRUCT, AND OPTIMIZE A HIGH-PERFORMANCE GRAVITY GRADIOMETER BASED ON LIGHT-PULSE ATOM INTERFEROMETRY. THE CONTRACTOR SHALL BUILD AND TEST A SECOND PROTOTYPE ZERO-DEAD-TIME (ZDT) ABSOLUTE GRAVIMETER. THE INSTRUMENTS IN THIS PHASE III EFFORT TAKES ADVANTAGE OF TECHNOLOGIES DEVELOPED UNDER NASA SBIR PHASE I AND PHASE II PROGRAMS.$225K
Jun 9, 2017National Aeronautics and Space AdministrationNASA SHARED SERVICES CENTERNNX17CG26P541712IGF::OT::IGF PRECISION NAVIGATION AND TIMING (PNT) IS A CRITICAL RESOURCE FOR GOVERNMENT AND COMMERCIAL AEROSPACE. GIVEN THE HIGH LAUNCH COST AND SHIFT TOWARD SMALLER PAYLOADS, REDUCING THE SIZE, WEIGHT, AND POWER (SWAP) OF SPACE-BASED NAVIGATION SYSTEMS IS A CRITICAL NEED. ATOM-INTERFEROMETRIC INERTIAL SENSORS HAVE DEMONSTRATED SUPERIOR PERFORMANCE OVER CONVENTIONAL INERTIAL DEVICES OWING TO THE INTRINSIC STABILITY OF ATOMIC SYSTEMS. CENTRAL TO MAKING COLD ATOM SENSORS PRACTICAL IS THEIR ABILITY TO RELIABLY OPERATE FOR EXTENDED PERIODS WITHOUT USER INTERVENTION. CURRENT LASER DIODES, WHICH ARE AT THE HEART OF ATOMIC SENSORS, SUFFER FROM POWER DEGRADATION AND MODE HOPS ON TIMESCALES INCOMPATIBLE WITH LONG TERM DEPLOYMENT. BECAUSE THESE PROPERTIES ARE INHERENT TO THE DIODES, IT IS PRUDENT TO CIRCUMVENT THESE PROBLEMS WITH DIAGNOSTIC PROTOCOLS AIMED AT EARLY DETECTION AND ACTION. DIODES CLOSE TO MODE HOPPING CAN BE TEMPORARILY TAKEN OFFLINE TO TUNE AWAY THE MODE HOP VIA CURRENT AND TEMPERATURE. DIODES WITH DEGRADED POWER CAN BE TAKEN OFFLINE ENTIRELY IN FAVOR OF A HEALTHY DIODE. THIS APPROACH WILL PROVIDE A ROBUST, WAVELENGTH-AGNOSTIC TECHNIQUE TO DELIVER RELIABLE, LONG-LIVED LASER SOURCES AT ATOM SENSOR-RELEVANT WAVELENGTHS. AOSENSE PROPOSES TO DEVELOP A COLD ATOM LASER MODULE (CALM) CAPABLE OF SUPPORTING A BROAD RANGE OF ATOMIC SENSORS. PHASE I WILL FOCUS ON ADDRESSING LASER SOURCE RELIABILITY. WE WILL IDENTIFY AND TEST AND CANDIDATE LASER DIODES TO IDENTIFY OPTIMAL SOURCES. IN PARALLEL, AOSENSE WILL DEVELOP PROTOCOLS TO IDENTIFY POTENTIAL DIODE FAILURE AND SEAMLESSLY SWITCH TO A HEALTHY DIODE. DEVELOPMENT OF THE CALM LASER MODULE WILL RESULT IN A RUGGEDIZED AND RELIABLE LASER SOURCE CAPABLE OF AUTONOMOUSLY DRIVING AN ATOM-BASED SENSOR WITHIN THE SPACE ENVIRONMENT. SUCH AN EFFORT WOULD ENABLE SPACE-BASED APPLICATIONS FOR ATOMIC SENSORS SUCH AS IMUS, CLOCKS, AND MAGNETOMETERS, OPENING UP SIGNIFICANT MARKET OPPORTUNITIES IN THE DEFENSE AND COMMERCIAL SECTORS.$125K
May 30, 2017National Aeronautics and Space AdministrationNASA SHARED SERVICES CENTERNNX17CG11C541712IGF::OT::IGF AOSENSE PROPOSES A FREE-SPACE, TWO-WAY OPTICAL TIME TRANSFER SYSTEM COMPATIBLE WITH GLOBAL-SCALE SYNCHRONIZATION OF CURRENT-GENERATION OPTICAL ATOMIC CLOCKS. IN PHASE I, WE HAVE DEMONSTRATED THE REQUISITE PERFORMANCE USING EXISTING HARDWARE COUPLED WITH OFF-THE-SHELF CONTROL ELECTRONICS. BASED ON OUR RESULTS, WE HAVE DESIGNED A FULLY-INTEGRATED MODULE CAPABLE OF DISSEMINATING TIMING SIGNALS WITH SUB-FEMTOSECOND ERROR FROM 1-10,000 S. IN PHASE II, WE WILL PACKAGE THE DEVICE AND DELIVER IT FOR EXTERNAL TESTING. OUR SYSTEM IS EXPECTED TO IMPROVE GROUND-TO-SATELLITE SYNCHRONIZATION A MILLION-FOLD OVER CURRENT RF-BASED TIME TRANSFER SYSTEMS, ENABLING APPLICATIONS INCLUDING CLOCK-BASED GEODESY, VERY LONG BASELINE INTERFEROMETRY, COHERENT LIDAR ARRAYS, AND TESTS OF GENERAL RELATIVITY. THE PHASE I BREADBOARD DEMONSTRATION PERFORMANCE IS CONSISTENT WITH A TIMING JITTER OF 3 FS @ 1S AND INTEGRATES DOWN TO 700 AS AT 30 SECONDS. THE CORRESPONDING FRACTIONAL TIMING INSTABILITY IS 3 X 10^-15 @ 1 SECOND, WHICH FLICKERS AT 2.7 X 10^-17 OUT TO 2000 SECONDS. WE HAVE IDENTIFIED THE SYSTEMATIC EFFECTS THAT LIMIT BOTH SHORT AND LONG TERM STABILITY AND INCORPORATED THE IMPROVEMENTS INTO THE PHASE II DESIGN. WITH THESE IMPROVEMENTS, WE EXPECT A 10X IMPROVEMENT IN BOTH SHORT AND LONG TERMS STABILITY OF THE SYSTEM. IN ADDITION, WE REVIEWED AND FORMALIZED THE LASER DRIVER AND CONTROL ELECTRONICS SPECIFICATIONS. THE INITIAL SCHEMATIC CAPTURE FOR CRITICAL ANALOG SUB SECTIONS WAS COMPLETED AND A SUITABLE FPGA/MICROPROCESSOR COMBINATION WAS CHOSEN TO CONTROL THE SYSTEM AND PROCESS THE TIMING INFORMATION. BASED ON THESE DESIGNS, POWER AND SIZE ESTIMATES WERE USED TO COMPLETE THE MECHANICAL ENCLOSURE MODEL FOR THE TIME-TRANSFER SYSTEM. FOR MAXIMUM FLEXIBILITY IN THE FINAL ARCHITECTURE OF THE OVERALL FREE-SPACE TIME TRANSFER SYSTEM, EACH FREQUENCY COMB SUB-UNIT THAT INCLUDES THE LASER AND CONTROL ELECTRONICS WILL BE HOUSED IN A 1U RACK MOUNT ENCLOSURE.$749K
Mar 7, 2017Department of Homeland SecurityDOM NUCLEAR DETECT OFF ACQ DIVHSHQDN16C00002541712IGF::OT::IGF IGF::OT::IGF NEW SBIR PHASE II CONTRACT$297K
Mar 3, 2017Department of DefenseOFFICE OF NAVAL RESEARCHN0001415C5022541712IGF::CT::IGF ONRBAA15-001 LONG RANGE BROAD AGENCY ANNOUNCEMENT (BAA) FOR NAVY AND MARINE CORPS SCIENCE AND TECHNOLOGY$771K
Feb 17, 2017Department of the InteriorIBC ACQ SERVICES DIVISION (00063)IND15PC00053541712IGF::OT::IGF PORTABLE COLD ATOM FREQUENCY STANDARD FOR FIELD APPLICATION. SMALL BUSINESS INNOVATION RESEARCH 14.1 PHASE II.$499K
Feb 8, 2017Department of DefenseFA8650 USAF AFMC AFRL PZL AFRL/PZLFA865015C7531541712IGF::OT::IGF STOIC - RACK-MOUNT OPTICAL CLOCK (ROC)$517K
Dec 7, 2016Department of DefenseOFFICE OF NAVAL RESEARCHN0001415C5022541712IGF::CT::IGF ONRBAA15-001 LONG RANGE BROAD AGENCY ANNOUNCEMENT (BAA) FOR NAVY AND MARINE CORPS SCIENCE AND TECHNOLOGY$220K
Nov 29, 2016Department of DefenseFA8650 USAF AFMC AFRL PZL AFRL/PZLFA865013C7327541712IGF::OT::IGF CHIP SCALE COMBINATORAL ATOMIC NAVIGATOR CSCAN$180K
Nov 15, 2016Department of DefenseFA8650 USAF AFMC AFRL PZL AFRL/PZLFA865015C7531541712IGF::OT::IGF STOIC - RACK-MOUNT OPTICAL CLOCK (ROC)$475K
Nov 10, 2016Department of DefenseDEF ADVANCED RESEARCH PROJECTS AGCYHR001109C0116541712COMPLETE THE TASKINGS FOR THE HIGH DYNAMIC RANGE ATOMIC SENSORS (HIDRA) PROGRAM.$645K
Nov 4, 2016Department of CommerceDEPT OF COMMERCE NISTDOCSB134117SU0021541712LASER DIODE CONTROLLER$5K
Sep 29, 2016National Aeronautics and Space AdministrationNASA SHARED SERVICES CENTERNNX16CG66C541712IGF::OT::IGF AOSENSE WILL BUILD AND TEST AN INTEGRATED ULTRASTABLE LASER MODULE CAPABLE OF REACHING A SHORT-TERM INSTABILITY OF<5E-15 @ 1S. THE FLEXIBLE DESIGN WILL ALLOW THE MODULE TO BE ADAPTED FOR SEVERAL RELEVANT OPTICAL CLOCK WAVELENGTHS WHICH UTILIZE EXTERNAL CAVITY DIODE LASERS. THE FIRST UNIT WILL OPERATE AT 698 NM TO ADDRESS THE SR CLOCK TRANSITION.$750K
Sep 23, 2016National Aeronautics and Space AdministrationNASA GODDARD SPACE FLIGHT CENTERNNG16VK17P541712IGF::OT::IGF CONTRACTOR SHALL PROVIDE ANALYTICAL SERVICES.$35K
Sep 13, 2016Department of CommerceDEPT OF COMMERCE NISTDOCSB134116SU0824334516EXTERNAL CAVITY DIODE LASER$14K
Sep 1, 2016Department of DefenseOFFICE OF NAVAL RESEARCHN0001413C0266541712RECONFIGURABLE OPTICAL LATTICES FOR ULTRACOLD ATOMS (N2-4429)$244K

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