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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 Multi-Wavelength Seed Derived Laser for In-Situ Validation of Airborne Remote Sensing Instruments

    SBC: ADVR, INC.            Topic: S107

    This Phase I SBIR will establish the feasibility of developing a collinear three wavelength source for an in-situ, 1800, back scatter nephelometer. The three wavelength source is being developed to facilitate on-board validation measurements of airborne remote backscatter lidar. Currently, commercial nephelometers utilized for in-situ validation measurements employ wavelengths that are both not ...

    SBIR Phase I 2015 National Aeronautics and Space Administration
  2. Compact, Rugged and Low-Cost Atmospheric Ozone DIAL Transmitter

    SBC: Bridger Photonics, Inc.            Topic: S101

    Bridger Photonics Inc. (Bridger) proposes developing the most efficient, compact, rugged, low-power consumption and cost-effective UV ozone differential absorption lidar (DIAL) transmitter available. Bridger will demonstrate pulse energies above 0.5 mJ with a goal of 1 mJ/pulse with a pulse repetition frequency of 1 kHz. The proposed transmitter will enable widespread deployment of ozone DIAL s ...

    SBIR Phase I 2015 National Aeronautics and Space Administration
  3. Contact Stress Design Parameters for Titanium Bearings

    SBC: AIR-LOCK, INCORPORATED            Topic: H402

    In response to NASA 2015 SBIR Topic H4.02, Air-Lock proposes to define the maximum allowable contact stress for Titanium bearings. The modulus of Titanium is lower than legacy spacesuit bearing materials (Stainless Steel). Due to this, Titanium bearings are more susceptible to deflection under man and plug load scenarios. Bearing deflection causes a limited number of balls to absorb the full load ...

    SBIR Phase I 2015 National Aeronautics and Space Administration
  4. Developing and Improving Commercial Marine Algal Culture in the United States

    SBC: Maine Fresh Sea Farms, LLC            Topic: 811F

    Maine Fresh Sea Farms (MFSF) will build a multi-species, multi-season prototype farm with the goal of having crops of fresh sea vegetables available throughout the year. What isn’t utilized fresh will be dried for longer-term storage and used in other products. Our team will gather data on water quality, nutrients, light levels, and hydrodynamics to assemble profiles of key parameters that deter ...

    SBIR Phase II 2015 Department of CommerceNational Oceanic and Atmospheric Administration
  5. Diagnosis-Driven Prognosis for Decision Making

    SBC: QUALTECH SYSTEMS, INC.            Topic: A104

    In Phase II, the QSI-Vanderbilt team seeks to develop a system-level diagnostics and prognostic process that incorporates a "sense and respond capability," which first uses error codes and discrete sensor values to correctly diagnose the system health including degradations and failures of sensors and components, and then invokes appropriate prognostics routines for the assessment of RUL and perfo ...

    SBIR Phase II 2015 National Aeronautics and Space Administration
  6. Digital Acquisition and Wavelength Control of Seed Laser for Space-Based LIDAR Applications

    SBC: ADVR, INC.            Topic: S101

    This SBIR Phase II proposes the development and delivery of a compact, space qualifiable, diode-based seed laser system that utilizes a digital controller to allow autonomous acquisition of lock to the required wavelength in remote environments for multi-wavelength flight and space-based lidar applications. Successful development of this technology, due to its compact, efficient, and reliable des ...

    SBIR Phase II 2015 National Aeronautics and Space Administration
  7. Efficient, High Power Density Hydrocarbon-Fueled Solid Oxide Stack System

    SBC: PRECISION COMBUSTION, INC.            Topic: H802

    Precision Combustion, Inc. (PCI) proposes to develop and demonstrate an innovative high power density design for direct internal reforming of regolith off-gases (e.g., methane and high hydrocarbons) within a solid oxide stack. The resulting enhanced heat transfer design offers the potential for higher overall efficiency, simplifies the system, and enables further compactness and weight reduction o ...

    SBIR Phase I 2015 National Aeronautics and Space Administration
  8. Fault Management Technologies

    SBC: QUALTECH SYSTEMS, INC.            Topic: S505

    There has been a renewed push across NASA centers and programs to make Systems Engineering & Integration (SE&I) processes more efficient and results-oriented than the current cumbersome and expensive cross-checking processes using text documents, and transition to a repeatable and a cost-effective process of Model Based Systems Engineering (MBSE). In parallel, Systems Health management (SHM), with ...

    SBIR Phase II 2015 National Aeronautics and Space Administration
  9. Fault Management Technologies- Metrics Evaluation and V&V

    SBC: QUALTECH SYSTEMS, INC.            Topic: S505

    Functional robustness, resulting from superior engineering design, along with appropriate and timely mitigating actions, is a key enabler for satisfying complex mission goals, and for enhancing mission success probability. Fault Management (FM) is a crucial mechanism to ensure system functionality from system design through the operational phase of a mission. FM is implemented with spacecraft har ...

    SBIR Phase I 2015 National Aeronautics and Space Administration
  10. Highly Efficient Electrochemical Cryogenic Purge Gas Recovery System

    SBC: SKYRE, INC            Topic: H1001

    Ongoing rocket test operations at NASA Stennis Space Center (SSC) result in substantial quantities of hydrogen gas that is flared from the facility in addition to valuable helium gas that is vented to the atmosphere. One method that can dramatically reduce the cost of test operations is to recover these gases using an electrochemical process. A Hydrogen Recovery System (HRS), which has recently b ...

    SBIR Phase I 2015 National Aeronautics and Space Administration
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