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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. Highly Reliable LOX Pump for Vehicle Loading Operations

    SBC: Barber-Nichols, LLC            Topic: N/A

    This proposal will present an innovative Phase I research and design plan for a reliable LOX pumping system for use in NASA vehicle loading. Due to seal problems with the current LOX loading pumps, the main focus of the Phase I effort will involve design and development of an innovative sealing solution that does not use a failure prone mechanical seal. The seal solution proposed is a combination ...

    SBIR Phase I 2003 National Aeronautics and Space Administration
  2. A Long-Duration Commercial Microgravity Mouse Habitat: Waste/Odor Technologies

    SBC: Bioastronautical Systems Development Co.            Topic: N/A

    The Bioastronautical Systems Development Company (BSDC) proposes to develop habitat technologies for conducting long-term commercial research with mice in microgravity. Our research addresses solicitation section B4.02 Space Commercialization for the design/development of microgravity payloads for space station applications that lead to commercial products or services. In partnership with BioServe ...

    SBIR Phase I 2003 National Aeronautics and Space Administration
  3. Utilizing MIL-STD-1553B Digital Data Bus Devices Across an IEEE-1394A Serial Bus

    SBC: SEAKR ENGINEERING, LLC            Topic: N/A

    The MIL-STD-1553B Bus is a widely supported data bus for avionics applications and compatible with most of the avionics equipment. However, its low data rate (1 Mbps) and command-response architecture are not suitable for many modern applications such as on-board autonomy. Therefore, the avionics industry recently has been interested in adopting the IEEE 1394A Bus as the next generation avionics b ...

    STTR Phase I 2003 National Aeronautics and Space Administration
  4. Utilizing MIL-STD-1553B Digital Data Bus Devices Across an IEEE-1394A Serial Bus

    SBC: SEAKR ENGINEERING, LLC            Topic: N/A

    The MIL-STD-1553B Bus is a widely supported data bus for avionics applications and compatible with most of the avionics equipment. However, its low data rate (1 Mbps) and command-response architecture are not suitable for many modern applications such as on-board autonomy. Therefore, the avionics industry recently has been interested in adopting the IEEE 1394A Bus as the next generation avionics b ...

    STTR Phase II 2003 National Aeronautics and Space Administration
  5. Next Generation Write Head for Commercial Holographic Data Storage

    SBC: Displaytech Incorporated            Topic: N/A

    Enormous data capacities and high read/write rates make optical holographic data stor-age (HDS) systems the most promising approach for next-generation computer mass-storage solutions. Recent breakthroughs in holographic recording media have dramatically accelerated the development of commercial HDS products, and have shifted the development focus to opti-mization of HDS optical systems and compon ...

    SBIR Phase I 2003 National Aeronautics and Space Administration
  6. Orbital Pump for Microgravity Applications

    SBC: Fluid Flow Technologies, LLC            Topic: N/A

    This proposed work will develop a new pump design, which is based on a uniquely generated orbital motion. The pump is intrinsically sealed and mechanically balanced, resulting in quiet, safe operation. The pump design has no seals, valves, bearings, complex mechanical linkages, or drive motor. Its simplicity promises to provide a pump, which is compact and reliable, has low mass, and possesses qui ...

    SBIR Phase I 2003 National Aeronautics and Space Administration
  7. Enhanced-Resolution Fine-Steering Mirror

    SBC: Left Hand Design Corporation            Topic: N/A

    Using existing technology, high-accuracy precision 2-axis fine-steering mirror (FSM) applications are limited to position sensors with 0.4 to 1.0 urad resolution. A number of applications, such as JPL?s optical communication programs require 0.1 urad resolution. Three recently developed commercial off-the-shelf (COTS) sensors have inherently better resolution, but have not been proven in FSM appli ...

    SBIR Phase I 2003 National Aeronautics and Space Administration
  8. Cockpit System Situational Awarness Modeling Tool

    SBC: Micro Analysis & Design Inc            Topic: N/A

    The Cockpit System Situational Awareness Modeling Tool will use the principles of discrete event simulation to predict pilot situational awareness (SA). The human performance modeling environment of IMPRINT combined with the cognitive modeling tool ACT-R will provide a powerful tool for the designers of cockpit systems. IMPRINT can already be used to predict pilot workload and assess the effects o ...

    SBIR Phase I 2003 National Aeronautics and Space Administration
  9. Nitrous Oxide Propulsion System

    SBC: PIONEER ASTRONAUTICS            Topic: N/A

    The Nitrous Oxide Propulsion System (NOPS) is a new Extravehicular Mobility Unit (EMU) thruster concept using nitrous oxide as a monopropellant. Liquid monopropellants are often used in propulsion systems where simplicity of design, restartable/control on demand, and repeatability is desired. Unfortunately, many monopropellants are toxic and dangerous, ruling them out for EMU thruster application. ...

    SBIR Phase I 2003 National Aeronautics and Space Administration
  10. LOX Olefin Rocket Propulsion for Deep Space

    SBC: PIONEER ASTRONAUTICS            Topic: N/A

    The LOX Olefin engine (LOXO or LOX/LC2H4 or LOX/LC3H6) is a proposed technology designed to provide interplanetary spacecraft with high specific impulse, space storable propulsion. With the LOXO engine, the combination of liquid oxygen with sub-cooled liquid ethylene or liquid propylene as a rocket propellant enables development of compact lightweight high performance stages with isothermal common ...

    SBIR Phase I 2003 National Aeronautics and Space Administration
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