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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.

  1. Reconfigurable Ultra-Low Power Miniaturized EVA Radio

    SBC: Teranovi Technologies            Topic: N/A

    EVA radio is an important integral part of lunar missions and beyond. To minimize power consumption and mass of an EVA radio, innovative solutions are needed for the design of various modules ranging from RF front end to networking protocols. In this protocol, a comprehensive design architecture that can achieve ultra-low power miniaturized EVA radio is proposed. Under this architecture, new MEMS- ...

    SBIR Phase I 2009 National Aeronautics and Space Administration
  2. Scalable Lunar Surface Networks and Adaptive Orbit Access

    SBC: Teranovi Technologies            Topic: O108

    Innovative network architecture, protocols, and algorithms are proposed for both lunar surface networks and orbit access networks. Firstly, an overlaying architecture is proposed to seamlessly integrate lunar surface networks and orbit access networks. Secondly, for lunar surface networks, a network architecture based on hybrid mesh networking technologies is developed to support both fixed and mo ...

    SBIR Phase I 2009 National Aeronautics and Space Administration
  3. Micro Pulsed Inductive Thruster with Solid Fuel Option (uPIT_SF)

    SBC: EAGLE HARBOR TECHNOLOGIES, INC.            Topic: S201

    The Micro Pulsed Inductive Thruster with Solid Fuel Option (µPIT_SF) is a high-precision impulse bit electromagnetic plasma micro-thruster. The µPIT prototype is a small (< 230 g) thruster that produces and accelerates plasma. In the solid fuel mode, µPIT_SF is able to substantially extend the performance of standard PPT systems by ionization and heating of the high density neutral gas produce ...

    SBIR Phase I 2009 National Aeronautics and Space Administration
  4. TEPC Microdosimeter for LEO and Beyond

    SBC: LVI Systems, Inc.            Topic: X1301

    A new generation of Tissue Equivalent Proportional Counters (TEPCs) for micro-dosimetric measurements will be designed, incorporating recent advances in the electronics industry and a new detector configuration. The unit is projected to be 2.5x4.5x1 in, weigh less than 8 oz, and consume less than 100 mW of power. A detector configuration of thirteen half-inch spheres arranged in a 2-D array wi ...

    SBIR Phase I 2009 National Aeronautics and Space Administration
  5. Reusable In Situ AirCore System for CO2 and Trace Gas Measurements

    SBC: KALSCOTT ENGINEERING INC.            Topic: S108

    A novel design for an in situ atmospheric sensor for CO2 and trace gases is proposed. The sensor, named AirCore, provides the advantages of existing in situ sensors (e.g. high resolution) but eliminates possible biases in analysis that often originate from imperfect measurement condition. The AirCore provides a significant savings in cost and weight while increasing the capabilities of existing ...

    SBIR Phase I 2009 National Aeronautics and Space Administration
  6. Single-Frequency Semiconductor Lasers Operating at 1.5 and 2.0 microns

    SBC: nLight Photonics            Topic: S101

    While conventional injection seeding sources (such as DFB diode lasers and rare-earth doped solid-state microchip lasers) are available at 1.5 microns, these sources typically lack the ultra-narrow (

    SBIR Phase I 2009 National Aeronautics and Space Administration
  7. Low Cost Method of Manufacturing Cooled Axisymmetric Scramjets

    SBC: Ormond, LLC            Topic: A201

    Scramjet engine developers are working on advanced axisymmetric engine concepts that may not be feasible due to limitations of currently available manufacturing methods. The primary goal of this SBIR is to make available a new technology that will make it feasible to manufacture small diameter one-piece cooled axisymmetric scramjet combustors. The availability of the proposed technology will re ...

    SBIR Phase I 2009 National Aeronautics and Space Administration
  8. Carbon Foam Self-Heated Tooling for Out-of-Autoclave Composites Manufacturing

    SBC: TOUCHSTONE RESEARCH LABORATORY, LTD.            Topic: X406

    This proposal addresses NASA's need for non-autoclave composites manufacture. The Constellation program, including the Ares V launch vehicle, will require very large-scale structures and conventional autoclave-based composites which are very costly and suffer from logistical problems. Out of autoclave (OOA) composite manufacturing technology has the potential to solve the constraint issues of aut ...

    SBIR Phase I 2009 National Aeronautics and Space Administration
  9. Atmospheric Water Vapor Adsorption for Mars In Situ Resource Utilization

    SBC: Adroit Systems, Inc.            Topic: N/A

    N/A

    SBIR Phase I 1998 National Aeronautics and Space Administration
  10. Variable Cell Blanket Sandwich Panel Technology

    SBC: Benecor, Inc.            Topic: N/A

    N/A

    SBIR Phase I 1998 National Aeronautics and Space Administration
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