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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. Dust Mitigation for the Lunar Surface

    SBC: Adherent Technologies, Inc.            Topic: X502

    The lunar surface is to a large extent covered with a dust layer several meters thick. Known as lunar regolith, it poses a hazard in the form of dust clouds being generated by all forms of gas expansions in the high vacuum environment of the lunar surface. This is especially pronounced during spacecraft operations. Instruments placed on the moon by the Apollo mission showed marked degradation d ...

    SBIR Phase I 2009 National Aeronautics and Space Administration
  2. Foam-in-Place Contaminant Containment System

    SBC: Adherent Technologies, Inc.            Topic: S502

    Over the next few decades, NASA plans to launch a number of planetary probes to and return the samples to Earth for detailed investigation. Due to the rapid expanse of space exploration, a need has been identified for the proper handling of extraterrestrial samples. Not only must the sample return system maintain the physical integrity of the sample in sometimes rigorous conditions (e.g., rover ...

    SBIR Phase I 2009 National Aeronautics and Space Administration
  3. Health and Maintenance Status Determination and Predictive Fault Diagnosis System

    SBC: AMERICAN GNC CORPORATION            Topic: T1001

    The objective of this project is to demonstrate intelligent health and maintenance status determination and predictive fault diagnosis techniques for NASA rocket engines under online and offline conditions from either on-board or maintenance, test and analytic data. AGNC proposes a Health and Maintenance Status Determination and Predictive Fault Diagnosis System (HMSD/PFDS). The fuzzy qualitative ...

    STTR Phase I 2009 National Aeronautics and Space Administration
  4. Distributed Rocket Engine Testing Health Monitoring System

    SBC: AMERICAN GNC CORPORATION            Topic: N/A

    The on-ground and Distributed Rocket Engine Testing Health Monitoring System (DiRETHMS) provides a system architecture and software tools for performing diagnostics and prognostics for supporting NASA's Integrated System Health Management (ISHM) capability for rocket engine testing and ground operations. DiRETHMS architecture consists of a hierarchical, modular, scalable, and flexible system struc ...

    SBIR Phase I 2009 National Aeronautics and Space Administration
  5. Reconfigurable Robust Routing for Mobile Outreach Network

    SBC: AMERICAN GNC CORPORATION            Topic: O108

    The early lunar network communications involves the use of a variety of communication channels and networks such as IEEE 802.16, Ka-Band and S-Band satellite data-links. The sophisticated environment casts a major challenge to provide a reliable network communications supporting the performance of lunar missions. In addition, the delivery of a higher Quality of Service (QoS) is not only stifled by ...

    SBIR Phase I 2009 National Aeronautics and Space Administration
  6. Architectures/Algorithms/Tools for Ultra-Low Power, Compact EVA Digital Radio

    SBC: UniRF Technologies, Inc.            Topic: O104

    The EVA digital radio imposes tight constraints on power consumption, latency, throughput, form factor, reconfigurability, single event upset and fault tolerance, and security. This requires a complete rethink on the digital radio architecture. We propose such an architecture called CHANDRA that exploits a cycle-by-cycle reconfigurable FPGA that is based on state-of-the-art double-gate CMOS and n ...

    SBIR Phase I 2009 National Aeronautics and Space Administration
  7. Composite Matrix Systems for Cryogenic Applications

    SBC: APPLIED POLERAMIC INCORPORATED            Topic: X405

    As an alternative material to aluminum-lithium, cryotanks developed from fiber reinforced composites can offer significant weight savings in applications for fuel containment of liquid oxygen and hydrogen. For composite materials to be accepted and utilized in these structures, they must be resistant to microcracking. It is the objective of this work to develop a matrix system for aerospace comp ...

    SBIR Phase I 2009 National Aeronautics and Space Administration
  8. Multifunctional Composite Materials

    SBC: APPLIED POLERAMIC INCORPORATED            Topic: A201

    Polymeric composite materials that are currently utilized in aircraft structures are susceptible to significant damage from lightning strikes. Enhanced electrical and thermal conductivity in these polymeric composites could eliminate this damage. The addition of this multifunctional capability to composites will result in lower manufacturing costs and weight reductions in future aircraft since t ...

    SBIR Phase I 2009 National Aeronautics and Space Administration
  9. Laser Ablation- Optical Cavity Isotopic Spectrometer (LAOCIS)

    SBC: APPLIED SPECTRA INC            Topic: N/A

    This proposal addresses NASA astrobiology objectives, particularly the need for a compact instrument capable of in situ isotopic measurements. We propose the detailed conceptual development of a device for analyzing key isotopic composition in surface materials without sample preparation. We will combine absorption spectroscopy with laser induced vaporization of solid samples for high-resolution i ...

    SBIR Phase I 2009 National Aeronautics and Space Administration
  10. A Liquid Hydrogen Cooler with a Cooling Capacity of 20 Watts

    SBC: ATLAS SCIENTIFIC            Topic: X701

    For the future spaceport and long-term storage of liquid hydrogen NASA requires cryocoolers that can provide cooling power in the range of 20 watts at 20 K. The closed-cycle cooling alternatives currently available for such applications are not well suited to the requirements. In many cases reliability is low and vibration high. In other cases coolers are too massive and inefficient. This propo ...

    SBIR Phase I 2009 National Aeronautics and Space Administration
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