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Award Data

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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 18885 results
  1. WEIGHT, COMPACT SOLAR WATER DISTILLATION PURIFICATION DEVICE

    SBC: Abel Company            Topic: N/A

    THIS STUDY WILL EXAMINE THE FEASIBILITY AND PRACTICALITY OF UTILIZING CHARCOAL CLOTH IN A LIGHT-WEIGHT SOLAR POWERED DISTILLATION PURIFICATION DEVICE INCORPORATING CHARCOAL CLOTH AS THE ENERGY ABSORBENT WATER WICK. IN THIS PROPOSED DEVICE, IT IS EXPECTED THAT THE CHARCOAL CLOTH WILL ACT NOT ONLY AS THE DISTILLATION MEDIA, BUT WILL ALSO REMOVE OBJECTIONABLE ODORS, CO-DISTILLABLE ORGANIC COMPOUNDS A ...

    SBIR Phase II 1984 Department of DefenseDefense Advanced Research Projects Agency
  2. JOINED WING AIRCRAFT

    SBC: Aca Industries, Inc.            Topic: N/A

    THE JOINED WING IS A NEW TYPE OF AIRCRAFT CONFIGURATION WHICH EMPLOYS TANDEM WINGS ARRANGED TO FORM DIAMOND SHAPES IN BOTH PLAN AND FRONT VIEWS. WIND TUNNEL TESTS AND FINITE- ELEMENT STRUCTURAL ANALYSES SHOW THAT THE JOINED WING PROVIDES THE FOLLOWING ADVANTAGES OVER A COMPARABLE CONVENTIONAL WING: LIGHTER WEIGHT AND HIGHER STIFFNESS, LESSINDUCED DRAG, LOWER WAVE DRAG, HIGHER TRIMMED MAXIMUM LIFT ...

    SBIR Phase II 1984 National Aeronautics and Space Administration
  3. ELIMINATION OF EXCESSIVE SURFACE DEFECTS IN GAAS IC MATERIALUSING NON-CONTACT POLISHING

    SBC: Aracor            Topic: N/A

    THE EXTENSION OF A NON-CONTACT POLISHING TECHNIQUE PREVIOUSLY DEVELOPED FOR IT-VI COMPOUNDS, IS PROPOSED FOR (100) GAAS WAFERS INTEGRATED CIRCUIT APPLICATIONS IN MIND. AN INITIAL TASK WILL BE TO CHARACTERIZE SUCH NON-CONTACT POLISHED SURFACES AND COMPARE THEM WITH CONVENTIONALLY POLISHED SURFACES. FOLLOWING SUCCESSFUL DEVELOPMENT OF THE TECHNIQUE, WE WILL INVESTIGATE THE FEASIBILITY OF SCALE-UP FO ...

    SBIR Phase II 1984 Department of DefenseDefense Advanced Research Projects Agency
  4. LONG LIFETIME, SPACEBORNE, CLOSED-CYCLE CRYOCOOLER

    SBC: Alabama Cryogenic Engineering, Inc.            Topic: N/A

    THIS PROJECT INVESTIGATES A CONCEPT FOR A CONTINUOUS REFRIGERATOR FOR OPERATION IN ZERO-GRAVITY WHILE COOLING SENSORS TO A TEMPERATURE DOWN TO 0.3 KELVIN. NO CAPABILITY SUCH AS THIS CURRENTLY EXISTS. THE CONCEPT ASSUMES A SUPERFLUID HELIUM DEWAR (1.5 KELVIN) AS THE HIGH-TEMPERATUREHEAT SINK. A SUPERFLUID HELIUM-4 STAGE, CALLED A "VORTEX" REFRIGERATOR, SERVES AS AN INTERMEDIATE COOLING SYSTEM TO IN ...

    SBIR Phase II 1984 National Aeronautics and Space Administration
  5. DEVELOPMENT OF SURFACE ACOUSTIC WAVE (SAW) ALTITUDE SENSOR

    SBC: Amerasia Technology, Inc.            Topic: N/A

    THERE IS A CONSTANT NEED FOR LESS COSTLY AIRCRAFT ALTITUDE SENSORS, FOR WHICH LARGE NUMBERS OF THESE SENSORS ARE REQUIRED. THE PROPOSED PROGRAM IS TO PERFORM STUDIES LEADING TO THE DEVELOPMENT OF A SURFACE ACOUSTIC WAVE (SAW) ALTITUDE SENSOR FOR AVIONICS AIR-DATA INSTRUMENTATION. THE OBJECTIVE OF THE PROPOSED PROGRAM IS TO DEVELOP A HIGH PERFORMANCE ALTITUDE SENSOR WHICH WILL UTILIZE STATE-OF-THE ...

    SBIR Phase II 1984 Department of Transportation
  6. A HIGH TEMPERATURE CERAMIC COMPOSITE

    SBC: Amercom Inc            Topic: N/A

    THERE IS A NEED FOR A GOOD STRUCTURAL CERAMIC MATERIAL THAT CAN BE USED AT HIGH TEMPERATURES IN THE OXIDIZING AND CORROSIVE ATMOSPHERE OF TURBINE ENGINES AND THAT CAN BE FORMED ECONOMICALLY TO COMPLEX SHAPE WITH LOW WEIGHT. THE OBJECTIVE OF THIS RESEARCH PROJECT IS TO INVESTIGATE A NEW FAMILY OF CERAMIC COMPSITE MATERIALS THAT MAY MEET THOSE REQUIREMENTS. IT IS BASED ON CHEMICALLY VAPOR DEPOSITED ...

    SBIR Phase II 1984 Department of DefenseAir Force
  7. COMPOSITE THERMAL PROTECTION MATERIAL

    SBC: Amercom Inc            Topic: N/A

    HEAT SHIELDS FOR EARTH ORBITING, REENTRY VEHICLES REQUIRE A LOW WEIGHT, DURABLE THERMAL PROTECTION SYSTEM THAT CAN OPERATE AT HIGH TEMPERRATURES IN AN OXIDIZING ATMOSPHERE. THE OBJECTIVE OF THIS RESEARCH PROJECT IS TO INVESTIGATE A NEW CERAMIC MATRIX COMPOSITE MATERIAL THAT MAY MEET THOSE REQUIREMENTS. THE MATERIAL IS MADE BY INFILTRATING SILICON CARBIDE IN THE GAS PHASE INTO A CERAMIC REINFORCEME ...

    SBIR Phase II 1984 National Aeronautics and Space Administration
  8. MICROPROCESSOR-BASED PSYCHOMETRIC TESTING DEVICE

    SBC: American Innovision, Inc.            Topic: N/A

    ADVANCES IN MICROCOMPUTERS AND VIDEO STORAGE TECHNOLOGY HAVE MADE FEASIBLE MAJOR IMPROVEMENTS IN SYSTEMS FOR ADMINISTERING PSYCHOLOGICAL TESTS. IN RESPONSE TO THE REQUEST FOR COMPUTERIZED PSYCHOMETRIC INSTRUMENTS BY THE NIMH IN THE SBIR OMNIBUS SOLICITATION, AMERICAN INNOVATION, INC. PROPOSES TO BUILD A MICROPROCESSOR-BASED TESTING INSTRUMENT WHICH STORES IMAGE AND TEXT DATA ON A VIDEO DISK.LOW CO ...

    SBIR Phase II 1984 Department of Health and Human Services
  9. ADVANCED FLIGHT PLANNING SYSTEM

    SBC: ANALYTICAL MECHANICS ASSOCIATES, INC.            Topic: N/A

    CURRENTLY, AIRLINE AND MILITARY AIRSPACE USERS DO NOT HAVE COORDINATED NOR CONSISTENT METHODS OF GENERATING FLIGHT PLANS (PRE-FLIGHT ROUTE STRUCTURE DEFINITION). SOME USE ANTIQUATED METHODS OF ROUTE GENERATION. SOME USE WEATHER DATA OVER 24 HOURS OLD. NONE ACCOUNT FOR THE POSSIBLE EXISTENCE OF AN ON-BOARD FLIGHT MANAGEMENT SYSTEM (FMS). THE OBJECTIVE OF THIS RESEARCH IS TO CORRECT THESE PROBLEMS B ...

    SBIR Phase II 1984 National Aeronautics and Space Administration
  10. AN INEXPENSIVE PEAK ACCELERATION INDICATOR FOR AIR CRASH MONITORING.

    SBC: ANCO ENGINEERS, INC.            Topic: N/A

    THE DOD HAS EXPRESSED INTEREST IN A LOW-COST, PASSIVE, SIMPLE, AND SMALL DEVICE OR TECHNIQUE THAT WOULD ALLOW QUANTITATIVE ASSESSMENT OF PEAK ACCELERATION ACHIEVED DURINGAN AIR CRASH. THESE DEVICES WOULD BE PLACED IN ALL SERVICE AIRCRAFT AND, IN THE EVENT OF A CRASH, COULD BE USED TO COR-RELATE INJURY WITH PEAK ACCELERATION. IT IS PROPOSED HEREIN TO DEVELOP A DEVICE BAED ON SMALL PELLETS OF DIFFER ...

    SBIR Phase II 1984 Department of DefenseArmy
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