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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 8 result(s)
 
  • Record 1 TO 8

  1. Crashworthy Seat Cushion Replacement

    SBC: J B DWERLKOTTE ASSOCIATES INC            Topic: N/A

    Dynamically certified seats (16g seats) are being fielded in all jet transports certified since 1988. In addition, the airlines are steadily replacing their older seats with 16g compatible seats in the older aircraft certified prior to that date. The implementation of the dynamic seat requirements has encountered one unanticipated problem. Under normal use, seat cushions must be replaced with iden ...

    SBIR Phase I 2001 National Aeronautics and Space Administration

  2. Innovative Thermal Protection System Approach to Reduce Parasitic Structures

    SBC: TOUCHSTONE RESEARCH LABORATORY, LTD.            Topic: N/A

    An opportunity exists to combine the structural elements of advanced launch vehicles with their thermal protection system (TPS) to create an integrated system, free of parasitic stand-offs and supports. An attractive approach, based on the marriage of two exciting technologies: continuously-brazed aluminum matrix composites (AMCs) and thermally-insulating carbon foam, can result in a more weight e ...

    SBIR Phase I 2001 National Aeronautics and Space Administration

  3. Brazed Aluminum Matrix Composite Material for Cryotanks, Lines and Ducts

    SBC: TOUCHSTONE RESEARCH LABORATORY, LTD.            Topic: N/A

    The next generation of reusable launch vehicle and satellite structures require new materials to meet aggressive program objectives such as decreasing vehicle weight in order to increase payload, and reducing cost per launch in order to decrease cost per pound of payload. Materials which have improved specific strength and specific stiffness, especially at cryogenic and elevated temperatures, will ...

    SBIR Phase I 2001 National Aeronautics and Space Administration

  4. A Lightweight, Structural Foam with Fire, Thermal, Noise and Impact Protection

    SBC: TOUCHSTONE RESEARCH LABORATORY, LTD.            Topic: N/A

    NASA is interested in innovative manufacturing methods and materials that will significantly reduce the cost and weight of general aviation aircraft, while improving cabin comfort and crash-worthiness. Energy absorption, in the form of projectile impact and crash protection, and fire resistance are major safety benefits, and noise reduction is a serious comfort consideration. Several engineering m ...

    SBIR Phase I 2001 National Aeronautics and Space Administration

  5. Variable Cell Blanket Sandwich Panel Technology

    SBC: Benecor, Inc.            Topic: N/A

    N/A

    SBIR Phase I 1998 National Aeronautics and Space Administration

  6. Suprises and Opportunities

    SBC: EMERGENT TECHNOLOGIES CORP.            Topic: N/A

    Emergent Technologies Corp. (ETC) in conjunction with research partners at West Virginia University has developed and recently patented an innovation antenna that promises to revolutionize the science of antenna design, construction and utilization. The antenna, labeled the Countrawound Toroidal Helical Antenna (CTTHA), offers a number of significant advantages over conventional antennas. The CT ...

    SBIR Phase I 1998 Department of DefenseSpecial Operations Command

  7. EVALUATION OF PVDF FILM AS A PRESSURE SENSOR

    SBC: B&d Instruments And Avionics            Topic: N/A

    THIS INNOVATION PROPOSAL WILL RESEARCH THE FEASIBILITY OF DEVELOPING A HIGHLY ACCURATE, LOW COST POLYMER SENSOR, UTILIZING THE PIEZOELECTRIC PROPERTIES OF PVDF COMBINED WITHA DIAPHRAGM AND/OR OTHER FORCE SENSITIVE STRUCTURE TO PRODUCE A PRESSURE SENSOR. THE POLYMER SENSOR WILL BE EASILY ADAPTED TO COMMERCIAL AND GENERAL AVIATION AIRCRAFT TO ADDRESS SENSORS UTILIZED IN SMART ANGLE OF ATTACK AND ANG ...

    SBIR Phase I 1990 National Aeronautics and Space Administration

  8. THIN MEMBRANE SENSORS

    SBC: Resource Technologies Group            Topic: N/A

    N/A

    SBIR Phase I 1990 National Aeronautics and Space Administration
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