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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. Autonomous Composite Fan Containment Integrity Monitoring (AUTOCONFIRM) System

    SBC: ACELLENT TECHNOLOGIES INC            Topic: N/A

    New engine fan blade containment structures are being manufactured with advanced composite structures such that they can withstand blade-out events. The use of advance composites requires the understanding of the possible effects of aging degradation on the performance of "hard wall" or "soft wall" composite fan containment structures to ensure durability in their use in jet engine applications. A ...

    SBIR Phase I 2008 National Aeronautics and Space Administration
  2. Quantifiable and Reliable Structural Health Management Systems

    SBC: ACELLENT TECHNOLOGIES INC            Topic: N/A

    Major concerns for implementing a practical built-in structural health monitoring system are prediction accuracy and data reliability. It is proposed to develop robust state-of-the-art structural health management (SHM) technologies to overcome these concerns. The proposed solution will be capable of detecting and quantifying damage with a high probability of detection (POD), accurately predictin ...

    SBIR Phase I 2008 National Aeronautics and Space Administration
  3. Moisture Resistant Primer for Composite Bonded Repairs

    SBC: Adherent Technologies, Inc.            Topic: A101

    Aging and durability of aircraft in both the military and civilian sectors are becoming major issues as the existing fleet continues to age. Additionally, the increased use of composite structures in the civilian fleet, such as in the Boeing 787 Dreamliner and the Airbus A380, make the understanding and/or improvement of composite durability, particularly durability of repairs, even more critical ...

    SBIR Phase I 2008 National Aeronautics and Space Administration
  4. Lunar Regolith Stabilization for Excavation

    SBC: Adherent Technologies, Inc.            Topic: X502

    Establishing human presence outside the protective cover of earth's atmosphere is a challenge. On earth, the atmosphere does not only present breathing gas, it also acts as a thermal buffer and protects the biosphere from harmful radiation. Shielding of humans from harmful radiation during long-term stays on an extraterrestrial body like the moon is a difficult task. Lunar regolith provides an ...

    SBIR Phase I 2008 National Aeronautics and Space Administration
  5. Self-Healing Inflatable, Rigidizable Shelter for the Lunar Environment

    SBC: Adherent Technologies, Inc.            Topic: X601

    Any manned missions to extraterrestrial locations will require shelter structures for a variety of purposes ranging from habitat usage to biomass production. Such shelters need to be constructed in such a way to minimize stowed volume and payload weight. The structures must also be very durable and have the ability to survive punctures without collapsing. Ways of increasing available crew-load ...

    SBIR Phase I 2008 National Aeronautics and Space Administration
  6. Foamed Antenna Support for Very Large Apertures

    SBC: Adherent Technologies, Inc.            Topic: O104

    The proposed Phase I program will demonstrate the feasibility of the in-space production of large aperture antenna structures. The use of a novel open cell foam, previously developed for NASA space antennas, will allow the deployment of reflectors at low cost and very low transport volume compared to currently used technologies like solid metal or mesh reflector. The use of a foam substrate also ...

    SBIR Phase I 2008 National Aeronautics and Space Administration
  7. Virtual Satellite Integration Environment

    SBC: ADVATECH PACIFIC, INC.            Topic: N/A

    Advatech Pacific proposes to develop a Virtual Satellite Integration Environment (VSIE) for the NASA Ames Mission Design Center. The VSIE introduces into NASA Mission Design Commercial Off-The-Shelf (COTS) Product Lifecycle Management (PLM) tools and processes, which haven proven themselves in the industrial manufacturing world. In addition to COTS PLM tools, the VSIE hinges on two key concepts: ...

    SBIR Phase I 2008 National Aeronautics and Space Administration
  8. Wireless Data and Power Transfer on Small Spacecraft

    SBC: AEROASTRO, INC.            Topic: S403

    Achieving low-cost space missions implies lowering all phases of mission development, including spacecraft design, assembly, integration and test. The concept of the wireless spacecraft bus is something most technical people are at least half familiar with - the half which includes wireless data transfer, something available on every computer laptop today. But wireless is not really wireless if th ...

    SBIR Phase I 2008 National Aeronautics and Space Administration
  9. A Multi-Physics CFD Toolkit for Reentry Flows

    SBC: AEROSOFT INC            Topic: A206

    AeroSoft proposes to develop a full featured CFD toolkit for analysis of the aerothermal environment and its effect on space vehicles. In Phase I, AeroSoft proposes to implement multi-component ablation along with material response into AeroSoft's structured and unstructured CFD solver GASP. In Phase I, GASP's internal thermal solver will be augmented to include the effects of ablation. In Ph ...

    SBIR Phase I 2008 National Aeronautics and Space Administration
  10. Design and Simulation Tools for Planetary Atmospheric Entry Vehicles

    SBC: Aerospacecomputing, Inc.            Topic: S502

    Atmospheric entry is one of the most critical phases of flight during planetary exploration missions. During the design of an entry vehicle, experimental and analytical methods are used; however, the current integration level of experimental and analytical methods with planetary entry simulations is low. Comprehensive software, comprised of multiple design tool components for simulating planetary ...

    SBIR Phase I 2008 National Aeronautics and Space Administration
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