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The Award database is continually updated throughout the year. As a result, data for FY24 is not expected to be complete until March, 2025.

Download all SBIR.gov award data either with award abstracts (290MB) or without award abstracts (65MB). A data dictionary and additional information is located on the Data Resource Page. Files are refreshed monthly.

The SBIR.gov award data files now contain the required fields to calculate award timeliness for individual awards or for an agency or branch. Additional information on calculating award timeliness is available on the Data Resource Page.

Displaying 1 - 10 of 17 results
 
  • Record 1 TO 17

  1. ADIABATIC WANKEL TYPE ROTARY ENGINES

    SBC: ADIABATICS INC            Topic: N/A

    N/A

    SBIR Phase I 1984 National Aeronautics and Space Administration

  2. THIS PROJECT INVOLVES A NEW APPROACH FOR A LOW POWER FOURIER TRANSFORM PROCESSOR.

    SBC: ANALYSIS AND MEASUREMENT SERVICE CORPORATION            Topic: N/A

    THIS PROJECT INVOLVES A NEW APPROACH FOR A LOW POWER FOURIER TRANSFORM PROCESSOR. AN ALGORITHM WHICH REQUIRES NO MULTIPLICATIONS IN THE FOURIER TRANSFORMATION HAS BEEN DEVELOPED. IT IS TO BE IMPLEMENTED AND TESTED IN THIS PROGRAM. THE ALGORITHM IS WELL SUITED FOR REAL-TIME SPECTRAL ANALYSIS AT FREQUENCIES OF INTEREST IN THE 0 TO 10 HZ RANGE REQUIRED FOR PROCESSING MAGNEMOMETER DATA. THE WORK ALSO ...

    SBIR Phase I 1984 National Aeronautics and Space Administration

  3. THE LARGE FORMAT CAMERA: NOVEL ANALYSES OF SENSOR APPLICATIONS

    SBC: Autometric Inc.            Topic: N/A

    N/A

    SBIR Phase I 1984 National Aeronautics and Space Administration

  4. TAPE

    SBC: CORDEC CORP.            Topic: N/A

    RECENT DEVELOPMENTS IN THE MANUFACTURE OF METAL MATRIX COMPOSITE PRECURSORS BY PHYSICAL VAPOR DEPOSITION TECHNIQUES HAVE CREATED AN OPPORTUNITY TO FABRICATE HIGH-QUALITY, FINE-GAGE COMPOSITE WIRES HAVING PRECISE DIMENSIONS AND FIBER VOLUME FRACTIONS. SPECIALLY DESIGNED DIES WILL BE USED TO DRAW ION-PLATED GRAPHITE/ALUMINUM AND GRAPHITE/MAGNESIUM COMPOSITE TAPES INTO 1.8-MM DIAMETER COMPOSITE WIRES ...

    SBIR Phase I 1984 National Aeronautics and Space Administration

  5. LOW-POWER SPECTRUM ANALYSIS AND REAL-TIME DATA COMPRESSION SYSTEM

    SBC: Defense Systems Inc.            Topic: N/A

    N/A

    SBIR Phase I 1984 National Aeronautics and Space Administration

  6. ATTACK

    SBC: Dei-tech Incorporation            Topic: N/A

    RECENT ADVANCES IN THE UNDERSTANDING OF FLIGHT AT POST STALL CONDITIONS HAVE SHOWN A POTENTIAL MANEUVERING BENEFIT IN ALLOWING QUICKER MORE AGILE TURNING WITH AN ATTENDANT TIME ON TARGET ADVANTAGE. FURTHERMORE, STALL AND SPIN RECOVERY HAS BEEN SHOWN TO BE MADE MORE EFFECTIVE USING A COMPANY PATENTED, MODIFIED HORIZONTAL CONTROL SURFACE. THIS PROJECT (PHASE I) IS AIMED AT DEVELOPING METHODS FOR THE ...

    SBIR Phase I 1984 National Aeronautics and Space Administration

  7. THIS PROJECT INVOLVES A DESIGN STUDY AND DEVELOPMENT OF A MULTI-ELEMENT HIGH REYNOLDS NUMBER NLF AIRFOIL THAT MINIMIZES THE TURBULENT SEPARATION PROBLEM AT OFF DESIGN CONDITIONS.

    SBC: Enzymed, Inc.            Topic: N/A

    THIS PROJECT INVOLVES A DESIGN STUDY AND DEVELOPMENT OF A MULTI-ELEMENT HIGH REYNOLDS NUMBER NLF AIRFOIL THAT MINIMIZES THE TURBULENT SEPARATION PROBLEM AT OFF DESIGN CONDITIONS. THE CONCEPT DEVELOPMENT WILL UTILIZE AN INTEGRATED MULTI-ELEMENT AIRFOIL SYSTEM TO BE DESIGNED TO FORM A SLOT BETWEEN THE UPPER AND LOWER SURFACE IN THE TURBULENT RECOVERY REGIONS. THIS SLOT BRINGS HIGHER ENERGY AIR FROM ...

    SBIR Phase I 1984 National Aeronautics and Space Administration

  8. SUPERCRITICAL (SC) LOW DRAG LFC AIRFOILS WITH HIGH DESIGN MACH NUMBERS OFFERING AN INCREASED OPERATING RANGE, WIDER HIGH SPEED BUFFET MARGINS (PREFERABLY WITHOUT BOUNDARY LAYER SUCTION IN THE REGION OF THE SPANWISE BENDING MATERIAL FOR COMPOSITE WINGS)

    SBC: Enzymed, Inc.            Topic: N/A

    SUPERCRITICAL (SC) LOW DRAG LFC AIRFOILS WITH HIGH DESIGN MACH NUMBERS OFFERING AN INCREASED OPERATING RANGE, WIDER HIGH SPEED BUFFET MARGINS (PREFERABLY WITHOUT BOUNDARY LAYER SUCTION IN THE REGION OF THE SPANWISE BENDING MATERIAL FOR COMPOSITE WINGS) AND SMALLER LIFT LOSS WITH TURBULENCE AT INTERMEDIATE MACH NUMBERS WILL BE DEVELOPED. INCREASED CLMAX NLF AND "HYBRID" TYPE SC LAMINAR FLOW AIRFOIL ...

    SBIR Phase I 1984 National Aeronautics and Space Administration

  9. PUMPED, TWO-PHASE, NON-AZEOTROPIC SPACECRAFT COOLING SYSTEMS

    SBC: Frederick A. Costello, Inc.            Topic: N/A

    N/A

    SBIR Phase I 1984 National Aeronautics and Space Administration

  10. THE DATA OBTAINED FROM MEASUREMENT OF RADON PROGENY AT REMOTE LOCATIONS AND VARYING ALTITUDES YIELDS VALUABLE INFORMATION ON GEOLOGIC PHENOMENA AND CONDITIONS, AND ON GLOBAL BIO-GEOCHEMICAL TRANSPORT MECHANISMS.

    SBC: Gull Engineering Inc.            Topic: N/A

    THE DATA OBTAINED FROM MEASUREMENT OF RADON PROGENY AT REMOTE LOCATIONS AND VARYING ALTITUDES YIELDS VALUABLE INFORMATION ON GEOLOGIC PHENOMENA AND CONDITIONS, AND ON GLOBAL BIO-GEOCHEMICAL TRANSPORT MECHANISMS. THE SURFACE GENERATION OF RADON, AND ITS SHORT HALF-LIFE PERMITS EVALUATION OF AIR MASS MOVEMENT. THIS IS OF PARTICULAR VALUE IF MEASURED ON A NEAR REAL-TIME BASIS. A REAL TIME AIR SAMPLER ...

    SBIR Phase I 1984 National Aeronautics and Space Administration
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