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Federal Contract Awards

53awards

Analyze awards, watch incumbents and competitors, track new transactions or changes, and use award history to shape recompete and capture strategy.

Awardee
is
DJWWMELNH821
Award ID
Description
Recipient
Total Value
Awarding Agency
Funding Agency
Set Aside
NAICS
PSC
Award Date
Start Date
End Date
80LARC25FA033
INFLATABLE AERODYNAMIC DECELERATOR (IAD) TRACK C - SOLID STATE GAS GENERATOR DEVELOPMENTANASPHERE, INC$3,458,993NATIONAL AERONAUTICS AND SPACE ADMINISTRATIONNATIONAL AERONAUTICS AND SPACE ADMINISTRATION—541715Research and Development in the Physical, Engineering, and Life Sciences (except Nanotechnology and Biotechnology)AR11SPACE R&D SERVICES; SPACE FLIGHT, RESEARCH AND SUPPORTING ACTIVITIES; BASIC RESEARCHSep 24, 2025Sep 24, 2025Jun 30, 2027
80NSSC25C0137
SBIR I MIXED GAS GENERATOR FOR INFLATABLE DECELERATORSANASPHERE, INC$149,497NATIONAL AERONAUTICS AND SPACE ADMINISTRATIONNATIONAL AERONAUTICS AND SPACE ADMINISTRATION—541715Research and Development in the Physical, Engineering, and Life Sciences (except Nanotechnology and Biotechnology)AJ14GENERAL SCIENCE AND TECHNOLOGY R&D SERVICES; GENERAL SCIENCE AND TECHNOLOGY; R&D ADMINISTRATIVE EXPENSESAug 27, 2025Sep 29, 2025Mar 27, 2026
80NSSC25C0105
PHASE II SBIRANASPHERE, INC$849,098NATIONAL AERONAUTICS AND SPACE ADMINISTRATIONNATIONAL AERONAUTICS AND SPACE ADMINISTRATION—541713Research and Development in NanotechnologyAJ14GENERAL SCIENCE AND TECHNOLOGY R&D SERVICES; GENERAL SCIENCE AND TECHNOLOGY; R&D ADMINISTRATIVE EXPENSESJun 12, 2025Jun 12, 2025Jun 11, 2027
80NSSC24PB261
FY24 SBIR PHASE I- SOLID-STATE NONCOMBUSTIBLE GAS GENERATORANASPHERE, INC$149,555NATIONAL AERONAUTICS AND SPACE ADMINISTRATIONNATIONAL AERONAUTICS AND SPACE ADMINISTRATION—541715Research and Development in the Physical, Engineering, and Life Sciences (except Nanotechnology and Biotechnology)AJ14GENERAL SCIENCE AND TECHNOLOGY R&D SERVICES; GENERAL SCIENCE AND TECHNOLOGY; R&D ADMINISTRATIVE EXPENSESAug 7, 2024Aug 7, 2024Aug 7, 2024
80LARC23FA022
INFLATABLE AERODYNAMIC DECELERATOR TRACK C - SOLID STATE GAS GENERATOR DEVELOPMENTANASPHERE, INC$284,150NATIONAL AERONAUTICS AND SPACE ADMINISTRATIONNATIONAL AERONAUTICS AND SPACE ADMINISTRATION—541715Research and Development in the Physical, Engineering, and Life Sciences (except Nanotechnology and Biotechnology)AR11SPACE R&D SERVICES; SPACE FLIGHT, RESEARCH AND SUPPORTING ACTIVITIES; BASIC RESEARCHMay 24, 2023May 24, 2023Sep 1, 2023
80NSSC22CA097
IMPROVED SOLID-STATE HYDROGEN GAS GENERATORANASPHERE, INC$749,223NATIONAL AERONAUTICS AND SPACE ADMINISTRATIONNATIONAL AERONAUTICS AND SPACE ADMINISTRATION—541715Research and Development in the Physical, Engineering, and Life Sciences (except Nanotechnology and Biotechnology)AJ14GENERAL SCIENCE AND TECHNOLOGY R&D SERVICES; GENERAL SCIENCE AND TECHNOLOGY; R&D ADMINISTRATIVE EXPENSESMay 13, 2022May 13, 2022May 12, 2024
80NSSC22C0015
LOW-COST MIXED-PHASE CLOUD CHARACTERIZATION SENSOR SUITEANASPHERE, INC$25,176NATIONAL AERONAUTICS AND SPACE ADMINISTRATIONNATIONAL AERONAUTICS AND SPACE ADMINISTRATION—541715Research and Development in the Physical, Engineering, and Life Sciences (except Nanotechnology and Biotechnology)AJ14GENERAL SCIENCE AND TECHNOLOGY R&D SERVICES; GENERAL SCIENCE AND TECHNOLOGY; R&D ADMINISTRATIVE EXPENSESFeb 18, 2022Sep 25, 2021Jun 24, 2022
80NSSC21C0102
IMPROVED SOLID-STATE HYDROGEN GAS GENERATORANASPHERE, INC$124,892NATIONAL AERONAUTICS AND SPACE ADMINISTRATIONNATIONAL AERONAUTICS AND SPACE ADMINISTRATION—541715Research and Development in the Physical, Engineering, and Life Sciences (except Nanotechnology and Biotechnology)AJ14GENERAL SCIENCE AND TECHNOLOGY R&D SERVICES; GENERAL SCIENCE AND TECHNOLOGY; R&D ADMINISTRATIVE EXPENSESMay 11, 2021May 19, 2021Nov 19, 2021
80NSSC21C0016
HIGH-CAPACITY, HIGH-SPEED, SOLID-STATE HYDROGEN GAS GENERATORANASPHERE, INC$149,974NATIONAL AERONAUTICS AND SPACE ADMINISTRATIONNATIONAL AERONAUTICS AND SPACE ADMINISTRATION—541715Research and Development in the Physical, Engineering, and Life Sciences (except Nanotechnology and Biotechnology)AR11SPACE R&D SERVICES; SPACE FLIGHT, RESEARCH AND SUPPORTING ACTIVITIES; BASIC RESEARCHDec 17, 2020Dec 17, 2020Apr 14, 2021
W911S220P0225
SMART TETHER FLIGHT MODULE, WITH CUP ANEANASPHERE, INC$38,728DEPT OF THE ARMYDEPT OF THE ARMY—339999All Other Miscellaneous Manufacturing6660METEOROLOGICAL INSTRUMENTS AND APPARATUSJan 17, 2020Jan 17, 2020Feb 18, 2020
75N93019P00942
LITETETHER STARTER KIT AND FLIGHT MODULE QTY 2)ANASPHERE, INC$12,090NATIONAL INSTITUTES OF HEALTHNATIONAL INSTITUTES OF HEALTH—334516Analytical Laboratory Instrument Manufacturing6640LABORATORY EQUIPMENT AND SUPPLIESAug 7, 2019Aug 7, 2019Aug 6, 2020
80NSSC19C0165
SATELLITES PROVIDE VALUABLE DATA FOR CLOUD, PRECIPITATION, AND RADIATIVE TRANSFER RESEARCH. SUPPORTING IN-SITU ATMOSPHERIC MEASUREMENTS OF CLOUD PROPERTIES ARE ESSENTIAL.ANASPHERE, INC$775,155NATIONAL AERONAUTICS AND SPACE ADMINISTRATIONNATIONAL AERONAUTICS AND SPACE ADMINISTRATION—541715Research and Development in the Physical, Engineering, and Life Sciences (except Nanotechnology and Biotechnology)AR11SPACE R&D SERVICES; SPACE FLIGHT, RESEARCH AND SUPPORTING ACTIVITIES; BASIC RESEARCHJul 12, 2019Jul 12, 2019Jun 11, 2022
80NSSC18P2041
RADIATIVE TRANSFER PROPERTIES OF CLOUDS PLAY AN IMPORTANT ROLE IN THE ENERGY BALANCE OF THE EARTH. NUMEROUS NASA PROGRAMS AND EXPERIMENTS ARE DIRECTED TO MEASURING THESE EFFECTS. IN-SITU MEASUREMENTS ARE CRITICAL FOR SUPPORTING SATELLITE-BORNE INSTRUMENTS. WHILE RESEARCH AIRCRAFT CARRY THE BEST IN-SITU INSTRUMENTS, THE AIRCRAFT AND INSTRUMENTS ARE TOO EXPENSIVE TO PROVIDE SUFFICIENT COVERAGE. ANASPHERE IS DEVELOPING A SUITE OF LOW-COST, BALLOON-BORNE INSTRUMENTS THAT CAN QUANTIFY ALL THREE CONDENSED PHASES OF WATER IN CLOUDS: SUPERCOOLED LIQUID, LIQUID, AND ICE. THE FIRST TWO INSTRUMENTS HAVE BEEN DEVELOPED AND ARE USED AROUND THE WORLD. THIS PROJECT IS DIRECTED TO DEVELOPING THE ICE WATER CONTENT (IWC) SENSOR TO COMPLETE THE TRIO. ADDITION OF AN IWC SENSOR WILL YIELD A SUITE OF INSTRUMENTS THAT CAN BE USED FOR MEASUREMENTS OF ALL CLOUD TYPES INCLUDING MIXED-PHASE CLOUDS. IN PHASE I, AN IWC SENSOR WHICH IS A DERIVATIVE OF THE PRECEDING SUCCESSFUL INSTRUMENTS WILL BE DEVELOPED. THIS WILL ENTAIL THE DEVELOPMENT OF A SUITABLE ICE COLLECTION MEDIUM AND ASSOCIATED CALIBRATION EQUATIONS. SUPPORTING WORK TO BE COMPLETED WILL INCLUDE OPTIMIZING ANASPHERE S ICING WIND TUNNEL FOR PURE ICE PARTICLE CONDITIONS. PHASE I WILL CONCLUDE WITH THE NEW IWC SENSOR BEING OPERATED IN THE ICING WIND TUNNEL.ANASPHERE, INC$124,757NATIONAL AERONAUTICS AND SPACE ADMINISTRATIONNATIONAL AERONAUTICS AND SPACE ADMINISTRATION—541715Research and Development in the Physical, Engineering, and Life Sciences (except Nanotechnology and Biotechnology)AR11SPACE R&D SERVICES; SPACE FLIGHT, RESEARCH AND SUPPORTING ACTIVITIES; BASIC RESEARCHJul 25, 2018Jul 27, 2018Feb 25, 2019
80NSSC18C0032
DEPLOYABLE AERODYNAMIC DECELERATORS ARE AN ENABLING TECHNOLOGY FOR MISSIONS TO PLANETS AND MOONS WITH ATMOSPHERES AS WELL AS FOR RETURNING PAYLOADS TO EARTH. THESE DECELERATORS REQUIRE A GAS SOURCE FOR INFLATION, AND THE OBJECTIVE IS TO PROVIDE AN IMPROVEMENT OVER EXISTING PRESSURIZED GAS INFLATION SYSTEMS. A HYDROGEN GAS GENERATOR SUITABLE FOR THE INFLATION OF HYPERSONIC AERODYNAMIC INFLATABLE DECELERATORS (HIADS) WAS DEVELOPED AND TESTED. KEY AREAS OF PHASE I WORK INCLUDED THE DESIGN OF A HEAT GENERATION AND TRANSFER SYSTEM TO FUNCTION UNDER ZERO-G CONDITIONS, COMPONENT DESIGNS RESISTANT TO DAMAGE FROM THE LAUNCH ENVIRONMENT, DESIGN OF AN ASSOCIATED FILTRATION AND CONTAINMENT SYSTEM, THE FABRICATION AND TEST OF GENERATORS INCORPORATING THE FOREGOING DESIGNS, AND THE DEVELOPMENT OF THERMAL MODELS OF THE SYSTEM. LIVE TESTS SUCCESSFULLY PROVED THE OPERATION OF ALL OF THE NEW DESIGN FEATURES DEVELOPED IN PHASE I. PHASE II WORK WILL INCLUDE: SCALING UP PHASE I GENERATOR DESIGNS, BUILDING AND TESTING LARGER GENERATOR EXAMPLES WITH THE LARGEST BEING SUITED TO 12-METER HIADS, ENVIRONMENTAL TESTING OF THE GENERATORS, NONDESTRUCTIVE TESTING TO ASSESS THE EFFECTS OF ENVIRONMENTAL TESTING, A ZERO-G DROP TEST, DEVELOPMENT OF HANDLING AND LIFECYCLE PLANS FOR THE GENERATORS, AND THE DELIVERABLE OF A FULLY FUNCTIONAL GENERATOR TO NASA.ANASPHERE, INC$899,334NATIONAL AERONAUTICS AND SPACE ADMINISTRATIONNATIONAL AERONAUTICS AND SPACE ADMINISTRATION—541715Research and Development in the Physical, Engineering, and Life Sciences (except Nanotechnology and Biotechnology)AR11SPACE R&D SERVICES; SPACE FLIGHT, RESEARCH AND SUPPORTING ACTIVITIES; BASIC RESEARCHMay 3, 2018May 3, 2018Sep 30, 2021
N6893617P0689
SMARTTETHER FLIGHT MODULEANASPHERE, INC$19,290DEPT OF THE NAVYDEPT OF THE NAVY—334519Other Measuring and Controlling Device Manufacturing6660METEOROLOGICAL INSTRUMENTS AND APPARATUSAug 23, 2017Aug 23, 2017Sep 30, 2017
NNX17CL36P
IGF::OT::IGF DEPLOYABLE AERODYNAMIC DECELERATORS ARE AN ENABLING TECHNOLOGY FOR MISSIONS TO PLANETS AND MOONS WITH ATMOSPHERES AS WELL AS FOR RETURNING PAYLOADS TO EARTH. THESE DECELERATORS REQUIRE A GAS SOURCE TO INFLATE THEM, AND THE OBJECTIVE IS TO PROVIDE AN IMPROVEMENT OVER EXISTING PRESSURIZED COLD GAS INFLATION SYSTEMS. A SOLID-STATE HYDROGEN GAS GENERATOR IS PROPOSED WHICH IS BASED ON THE THERMAL DECOMPOSITION OF A METAL HYDRIDE IN A CONTROLLED MANNER. ANASPHERE HAS SUCCESSFULLY DEMONSTRATED THIS TECHNOLOGY IN AIR FORCE AND DARPA PROJECTS. VOLUME AND FLOW SPECIFICATIONS FOR THE DARPA GENERATOR WERE WITHIN A FACTOR OF 10 OF WHAT IS REQUIRED FOR A PHASE II DEMONSTRATION. ADVANCES TO BE DEMONSTRATED IN PHASE I RELATE TO ADAPTING THE GENERATOR TECHNOLOGY FOR SPACE OPERATION AND OPTIMIZING THE SYSTEM FROM A MASS PERSPECTIVE. PHASE I WORK WILL INCLUDE THERMAL RESERVOIR DESIGN AND OPTIMIZATION FOR THE SPACE ENVIRONMENT, GAS GENERATION VESSEL DESIGN AND OPTIMIZATION FOR THE SPACE ENVIRONMENT, HEAT TRANSFER OPTIMIZATION, PHYSICAL TESTING OF SUBSCALE ELEMENTS FOLLOWED BY SUBSCALE GENERATOR TESTING, AND FINALLY THE COMPLETION OF SCALED-UP DESIGNS.ANASPHERE, INC$124,314NATIONAL AERONAUTICS AND SPACE ADMINISTRATIONNATIONAL AERONAUTICS AND SPACE ADMINISTRATION—541712AR11SPACE R&D SERVICES; SPACE FLIGHT, RESEARCH AND SUPPORTING ACTIVITIES; BASIC RESEARCHJun 4, 2017Jun 9, 2017Dec 8, 2017
N6893617P0191
RADIO TETHERANASPHERE, INC$8,470DEPT OF THE NAVYDEPT OF THE NAVY—5417126660METEOROLOGICAL INSTRUMENTS AND APPARATUSDec 20, 2016Dec 20, 2016Jan 17, 2017
NND16AA88P
TETHERSONDE SYSTEM - FLIGHT MODULE, GROUND STATION, BLIMP, AND WINCHANASPHERE, INC$24,230NATIONAL AERONAUTICS AND SPACE ADMINISTRATIONNATIONAL AERONAUTICS AND SPACE ADMINISTRATION—334519Other Measuring and Controlling Device Manufacturing6660METEOROLOGICAL INSTRUMENTS AND APPARATUSApr 18, 2016Apr 18, 2016May 17, 2016
AG7D28P150068
IGF::CT::IGF SMARTTETHER V8 FLIGHT MODULE CUP ANEMOMETERANASPHERE, INC$9,750AGRICULTURAL RESEARCH SERVICEAGRICULTURAL RESEARCH SERVICE—334519Other Measuring and Controlling Device Manufacturing6660METEOROLOGICAL INSTRUMENTS AND APPARATUSJul 9, 2015Jul 9, 2015Jul 31, 2015
N6227115M1111
SMARTTETHER FLIGHT MODULE AND ACCESSORIES.ANASPHERE, INC$62,380DEPT OF THE NAVYDEPT OF THE NAVY—5417126660METEOROLOGICAL INSTRUMENTS AND APPARATUSMar 11, 2015Mar 11, 2015Jun 30, 2015
NNC14VF70P
SINGLE WIRE SLWC SENSORS FOR USE WITH RADIOSONDES.ANASPHERE, INC$26,000NATIONAL AERONAUTICS AND SPACE ADMINISTRATIONNATIONAL AERONAUTICS AND SPACE ADMINISTRATION—5417126660METEOROLOGICAL INSTRUMENTS AND APPARATUSJul 23, 2014Jul 23, 2014Oct 28, 2014
NNX14CC16C
IGF::OT::IGF ICING IS ONE OF THE MOST SIGNIFICANT HAZARDS TO AIRCRAFT. A SIZING SUPERCOOLED LIQUID WATER CONTENT (SSLWC) SONDE IS BEING DEVELOPED TO MEET A DIRECTLY RELATED NEED FOR IN-SITU MEASUREMENTS OF BOTH TOTAL SUPERCOOLED LIQUID WATER CONTENT AND DROPLET SIZE DISTRIBUTION. THIS DATA WILL SUPPORT THE DEVELOPMENT OF REMOTE SENSING INSTRUMENTATION TO DETECT ICING CONDITIONS, SUPPORT AIRCRAFT CERTIFICATION ACTIVITIES FOR FLIGHT INTO KNOWN ICING CONDITIONS, AND SUPPORT THE DEVELOPMENT OF NEW ICING-RELATED OPERATIONAL WEATHER FORECAST PRODUCTS. PHASE I DEMONSTRATED THE FEASIBILITY OF THE SSLWC SONDE'S MEASUREMENT TECHNIQUE. THE SONDE AIRFRAME WAS DESIGNED, BUILT, AND TESTED, MATHEMATICAL MODELS RELATING THE SONDE'S RAW DATA TO THE TARGET VARIABLES WERE COMPLETED, A DATA PROCESSING ALGORITHM WAS DEVELOPED AND IMPLEMENTED, AND A PROOF-OFCONCEPT SONDE WAS BUILT. PHASE II WILL INVOLVE REFINING THE SONDE DESIGN, ADAPTING THE MATHEMATICAL ALGORITHMS INTO THEIR FINAL APPLICATION ENVIRONMENTS, CONDUCTING ADDITIONAL STUDIES OF SONDE ELEMENTS IN AN ICING WIND TUNNEL, AND UNDERTAKING TWO FIELD MISSIONS TO OBTAIN INTERCOMPARISON DATA BETWEEN THE SSLWC SONDE AND OTHER ACCEPTED APPROACHES TO SUCH MEASUREMENTS. AT THE END OF PHASE II, THE SSLWC SONDE WILL BE PROVEN TO THE POINT THAT IT CAN BE MARKETED WITH CONFIDENCE FOR THE APPLICATION AREAS OUTLINED ABOVE.ANASPHERE, INC$749,917NATIONAL AERONAUTICS AND SPACE ADMINISTRATIONNATIONAL AERONAUTICS AND SPACE ADMINISTRATION—541712AR11SPACE R&D SERVICES; SPACE FLIGHT, RESEARCH AND SUPPORTING ACTIVITIES; BASIC RESEARCHApr 18, 2014Apr 18, 2014Apr 17, 2016
W911QX14P0009
EIGHT (8) SMARTTETHER FLIGHT MODULES, ONE (1) GROUND STATION, AND THREE (3) CONTROLLERSANASPHERE, INC$47,300DEPT OF THE ARMYDEPT OF THE ARMY—5417126660METEOROLOGICAL INSTRUMENTS AND APPARATUSOct 17, 2013Oct 17, 2013Nov 22, 2013
NNX13CC18P
IGF::OT::IGF ICING IS A SIGNIFICANT AVIATION HAZARD, AND ICING CONDITIONS CONTINUE TO BE DIFFICULT TO PRECISELY FORECAST OR LOCATE IN REAL TIME. AN IN-SITU SENSOR, WHICH CAN BE FLOWN COUPLED WITH A RADIOSONDE, IS NEEDED WHICH CAN BOTH MEASURE SUPERCOOLED LIQUID WATER CONTENT IN CLOUDS AS WELL AS CHARACTERIZE THE DROPLET SIZES. THIS SENSOR WILL SUPPORT THE CALIBRATION AND VALIDATION OF REMOTE-SENSING METHODS USED TO DETECT ICING CONDITIONS, AND CAN ALSO BE USED ON ITS OWN TO SUPPORT OPERATIONAL METEOROLOGY APPLICATIONS. ANASPHERE, INC. PROPOSES TO DEVELOP A SIZING SUPERCOOLED LIQUID WATER CONTENT (SSLWC) SONDE WHICH WILL MEET THIS NEED. IT WILL BE BASED ON PROVEN VIBRATING-WIRE TECHNOLOGY WHICH HAS BEEN USED FOR TOTAL WATER CONTENT MEASUREMENTS, BUT WITH AN ALTOGETHER DIFFERENT PHYSICAL IMPLEMENTATION THAT WILL ENABLE DROPLET SIZING. PHASE I WILL INVOLVE THE AERODYNAMIC DESIGN OF THE SSLWC SONDE, ICING TUNNEL TESTS DEMONSTRATING KEY ELEMENTS OF ITS FUNCTION, AND A LIVE FLIGHT TEST TO GATHER INFORMATION ON THE SONDE'S AERODYNAMIC CHARACTERISTICS. PHASE II WILL INVOLVE FURTHER TUNNEL TESTS, LABORATORY CALIBRATION DEVELOPMENT, DESIGN FOR MANUFACTURABILITY, AND FLIGHT TESTS IN ICING CONDITIONS.ANASPHERE, INC$124,979NATIONAL AERONAUTICS AND SPACE ADMINISTRATIONNATIONAL AERONAUTICS AND SPACE ADMINISTRATION—541712AR11SPACE R&D SERVICES; SPACE FLIGHT, RESEARCH AND SUPPORTING ACTIVITIES; BASIC RESEARCHMay 15, 2013May 23, 2013Nov 23, 2013
NNG13HD41P
SMARTTETHER FLIGHT MODULE (1 EACH) DUAL FREQUENCY OPTION (1 EACH) SMARTTETHER GROUND STATION (1 EACH) 15-FT BLIMP (1 EACH)ANASPHERE, INC$8,735NATIONAL AERONAUTICS AND SPACE ADMINISTRATIONNATIONAL AERONAUTICS AND SPACE ADMINISTRATION—334519Other Measuring and Controlling Device Manufacturing6640LABORATORY EQUIPMENT AND SUPPLIESFeb 14, 2013Feb 14, 2013Feb 26, 2013
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