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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. A GIS Software Toolkit for Converting NASA HDF-EOS Data Products to GIS and Other Geospatial Formats

    SBC: Aniuk Consulting, LLC            Topic: S603

    Aniuk Consulting, LLC, proposes to create a GIS software toolkit for easily converting NASA HDF-EOS data into formats that can be readily used within a Geographic Information System (GIS) or other geospatial software programs. The Hierarchical Data Format (HDF) is a widely used scientific data format and serves as the standard format for NASA EOS products. The HDF-EOS toolbar will allow a user t ...

    SBIR Phase I 2009 National Aeronautics and Space Administration
  2. Advanced Microwave Electrothermal Thruster (AMET)

    SBC: Orbital Technologies Corporation            Topic: T301

    Orbital Technologies Corporation (ORBITEC) and the University of Alabama at Huntsville (UAH) propose to develop the Advanced Microwave Electrothermal Thruster (AMET), a high-efficiency thruster which will use water propellant to enable various Lunar and Mars missions. The proposed AMET will incorporate a number of innovations to dramatically improve upon existing designs, including the use of a l ...

    STTR Phase I 2009 National Aeronautics and Space Administration
  3. High-Fidelity Lunar Dust Simulant

    SBC: Orbital Technologies Corporation            Topic: X704

    The severity of the lunar dust problems encountered during the Apollo missions were consistently underestimated by ground tests, illustrating the need to develop significantly better lunar dust simulants and simulation facilities. ORBITEC is proposing to continue developing high-fidelity lunar dust simulants that better match the unique properties of lunar dust than existing regolith simulants (s ...

    SBIR Phase II 2009 National Aeronautics and Space Administration
  4. Algorthms and Regolith Erosion Models for the Alert Code

    SBC: Orbital Technologies Corporation            Topic: T701

    ORBITEC and Duke University have teamed on this STTR to develop the ALERT (Advanced Lunar Exhaust-Regolith Transport) code which will include new developments in modeling of regolith erosion and entrainment as well as plume transport with full mass and momentum conservation. The Plume is handled in a Vlasov formalism with drag force on dust grains, dust equations of motion are solved over a size s ...

    STTR Phase I 2009 National Aeronautics and Space Administration
  5. FIR Detectors/Cameras Based on GaN and Si Field-Effect Devices

    SBC: Sensor Electronic Technology, Inc.            Topic: S104

    SETI proposes to develop GaN and Si based multicolor FIR/THz cameras with detector elements and readout, signal processing electronics integrated on a single chip. The active detector elements will be submicron gated channels with 2 dimensional electron gas (2DEG). The devices with gated 2DEG (commonly known as field-effect transistors) respond to the incoming FIR radiation due to the rectificat ...

    SBIR Phase I 2009 National Aeronautics and Space Administration
  6. Enhanced Brine Dewatering System

    SBC: Orbital Technologies Corporation            Topic: X302

    The purpose of the Enhanced Brine Dewatering System (EBDS) is to provide an easily scalable means of completely recovering usable water from byproducts created by reverse osmosis water purification systems without the use of consumable wicks. Extended duration Lunar and Mars missions will require the conservation and recovery of water to allow for autonomous closed environments that in turn can dr ...

    SBIR Phase I 2007 National Aeronautics and Space Administration
  7. Plasma Air Decontamination System (PADS)

    SBC: Orbital Technologies Corporation            Topic: X301

    The proposed Plasma Air Decontamination System (PADS) is a trace contaminant control device based on non-thermal atmospheric pressure plasma technology that operates at ambient pressure and temperature and has the potential to replace the existing Trace Contaminant Control System (TCCS) used on the International Space Station and future exploration vehicles. Non-thermal atmospheric plasma has been ...

    SBIR Phase I 2007 National Aeronautics and Space Administration
  8. Just-in-Time Simulation Platform

    SBC: Planet, LLC            Topic: X1202

    Long-duration missions may one day present the most demanding situations ever encountered in manned spaceflight. Success will therefore depend on the knowledge and flexibility of the crew and the critical tools at their disposal. This Phase I proposes to combine intelligent tutoring with highly interactive 3D simulation software to create an on-demand situational training and operations support sy ...

    SBIR Phase I 2007 National Aeronautics and Space Administration
  9. Plume Diagnostics for Combustion Stability

    SBC: SIERRA ENGINEERING, INC.            Topic: T901

    Sierra Engineering Inc. and Purdue University propose to develop a non-intrusive plume instrument capable of detecting and diagnosing combustion instability. This Stability Diagnostic System (SDS) will be designed, assembled, and tested during this effort. The SDS will include a high-speed video camera and multiple photodiode detectors for observing the plume. It will also include a software pa ...

    STTR Phase II 2007 National Aeronautics and Space Administration
  10. Affordable High Power Density Engine Designs for Personal Air Vehicles

    SBC: GSE INC            Topic: T701

    Next generation General Aviation (GA) Sport Class air vehicles limited to 1200lbs, represent the first opportunity to overhaul the FAA certification process necessary to manufacture affordable aircraft. With propulsion representing over one-third of the direct manufacturing costs of the entire aircraft, dramatic reductions in aircraft engine costs must be achieved by design, economy of scale, and ...

    STTR Phase I 2004 National Aeronautics and Space Administration
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