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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. Ultra-Miniaturized Star Tracker for Small Satellite Attitude Control

    SBC: CREARE LLC            Topic: T801

    Creare and Embry-Riddle Aeronautical University (ERAU) propose to complete the design, development, and testing of an ultra compact star tracker specifically intended for small satellites such as the CubeSat platform. Our design is based on proprietary "folded optics" technology previously developed by ERAU for use in military and commercial optical applications that require a compact footprint a ...

    STTR Phase II 2014 National Aeronautics and Space Administration
  2. Miniature Nontoxic Nitrous Oxide-Propane (MINNOP) Propulsion

    SBC: Orbital Technologies Corporation            Topic: S302

    ORBITEC proposes to develop the Miniature Nontoxic Nitrous Oxide-Propane (MINNOP) propulsion system, a small bipropellant propulsion system which we offer as an alternative to miniature hydrazine monopropellant thrusters for CubeSat-class spacecraft. As compared to state-of-the-art hydrazine systems, MINNOP propulsion will provide significant increases in specific impulse (in bipropellant mode) a ...

    SBIR Phase I 2014 National Aeronautics and Space Administration
  3. Fabrication of T-SOFC via Freeze Cast Methods for Space and Portable Applications

    SBC: Yanhai Power LLC            Topic: H801

    As NASA space missions become longer in duration the need for high efficiency power generator sets that can operate on NASA logistical fuel become critical. Historically NASA has used fuel cells as part of the energy solution. Space bound energy and power systems require rapid start and stop cycle times as well as high power densities. The high operational efficiency, coupled with the use of logi ...

    SBIR Phase I 2014 National Aeronautics and Space Administration
  4. Space Evaporator Absorber Radiator for Life Support and Thermal Control Systems

    SBC: CREARE LLC            Topic: H2002

    Future human space exploration missions will require advanced life support technology that can operate across a wide range of applications and environments. Thermal control systems for space suits and spacecraft will need to meet critical requirements for water conservation and adaptability to highly variable thermal environments. To achieve these goals, we propose an International Space Station ...

    SBIR Phase I 2014 National Aeronautics and Space Administration
  5. Dualband MW/LW Strained Layer Superlattice Focal Plane Arrays for Satellite-Based Wildfire Detection

    SBC: QMAGIQ LLC            Topic: S103

    Dualband focal plane arrays (FPAs) based on gallium-free Type-II strained layer superlattice (SLS) photodiodes have recently experienced significant advances. We propose to develop a new class of devices capable of producing simultaneous and spatially-registered images in two spectral bands, namely, a fire channel in the 3 to 5 micron window and a thermal channel covering the range of 8 to 12 mic ...

    SBIR Phase I 2014 National Aeronautics and Space Administration
  6. Space Evaporator Absorber Radiator (SEAR) for Thermal Storage on Manned Spacecraft

    SBC: CREARE LLC            Topic: H301

    Future manned exploration spacecraft will need to operate in challenging thermal environments. State-of-the-art technology for active thermal control relies on sublimating water ice and venting the vapor overboard in very hot environments. This approach can lead to large loss of water and a significant mass penalty for the spacecraft. We propose to develop a Space Evaporator Absorber Radiator ( ...

    SBIR Phase I 2014 National Aeronautics and Space Administration
  7. Multipurpose Cooling Garment for Improved Space Suit Environmental Control

    SBC: CREARE LLC            Topic: H401

    Future manned space exploration missions will require space suits with capabilities beyond the current state of the art. Portable Life Support Systems for these future space suits face daunting challenges, since they must maintain healthy and comfortable conditions inside the suit for long-duration missions while minimizing weight and water venting. We propose to develop an innovative, multipurp ...

    SBIR Phase I 2014 National Aeronautics and Space Administration
  8. Plastic Melt Waste Compactor Flight Demonstrator Payload (PFDP)

    SBC: Orbital Technologies Corporation            Topic: H2002

    The PMWC Flight Demonstrator Payload is a trash dewatering and volume reduction system that uses heat melt compaction to remove nearly 100% of water from trash while significantly reducing the volume. Recent advances have proven that ORBITEC's HEHO-PMWC is a viable technology for producing 16" square tiles for radiation protection. ORBITEC proposes to enhance the current SOA by repackaging all the ...

    SBIR Phase I 2014 National Aeronautics and Space Administration
  9. Dust Separation and Measurement System for Mars ISRU Applications

    SBC: CREARE LLC            Topic: H101

    NASA has recognized that in future exploration and human missions to Mars, the problem of Martian dust contaminating gas processing systems and human habitats will need to be solved. The dust content of Martian atmosphere is only sparsely known, and in particular the variation over the surface and the dust particle size distribution are largely unknown. Creare proposes to develop a compact, inte ...

    SBIR Phase I 2014 National Aeronautics and Space Administration
  10. A Green, Safe, Dual-Pulse Solid Motor for CubeSat Orbit Changing

    SBC: Digital Solid State Propulsion, Inc            Topic: S302

    Small satellites such as CubeSats are in need of responsive propulsion, but are limited due to their size. Though single pulse, AP/HTPB fueled solid rocket motors exist in the market, greater mission flexibility is to be had from a motor with the capability of a second ignition in the same volume constraints. Digital Solid State Propulsion (DSSP) proposes research into the technology to not only t ...

    SBIR Phase I 2014 National Aeronautics and Space Administration
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