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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. Triple3 Redundant Spacecraft Subsystems (T3RSS)

    SBC: REDEFINE TECHNOLOGIES, INC.            Topic: T101

    T3RSS is the system engineer's tool that allows a systematic approach to ensuring that even if one or more failures occur in a single component or subsystem, then the subsystem will continue to function and most, if not all, mission objectives can still be achieved. T3RSS does this by using a Configuration Manager for a Dynamically Reconfigurable System (CMDRS). This piece of logic employs a Missi ...

    STTR Phase II 2007 National Aeronautics and Space Administration
  2. 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
  3. Cooled Bolometer IR Monolithic FPA

    SBC: BFE Acquisition Sub II, LLC            Topic: S401

    Future space-based observatories imaging in the 4-40 ìm spectral regime will be passively cooled. The objective of this research effort is to demonstrate near theoretical performance of bolometer-based infrared focal plane arrays (FPAs) covering the 4-40 ìm wavelength region by operating the FPA at reduced temperature. Amorphous silicon-alloy resistive bolomoters exhibit increased temperature co ...

    SBIR Phase I 2007 National Aeronautics and Space Administration
  4. Precision Hinge Actuator for Advanced Telescope Systems

    SBC: COMPOSITE TECHNOLOGY DEVELOPMENT, INC.            Topic: S303

    CTD proposes to investigate the deployment repeatability and microdynamic stability of a hinge and demonstration this repeatability in a deployable mirror test article, which incorporates the proposed precision self-locking hinge actuator. If successful, the proposed device will be substantially lighter, simpler, more robust, and more easily controlled than other state-of-the-art actuators for de ...

    SBIR Phase I 2007 National Aeronautics and Space Administration
  5. Thermal Data Exchange Using International Standards

    SBC: Cullimore & Ring Technologies, Inc.            Topic: S706

    Spacecraft projects today consist of many different cooperating companies and institutions. The project members typically use different thermal design analysis software, making the vital exchange of data between team members difficult, costly, or impossible. One solution would be for everyone to use the same software, such that there would be no loss of data when exchanging models and predictions. ...

    SBIR Phase I 2007 National Aeronautics and Space Administration
  6. Simple, Micro-Miniature Total Organic Carbon Analyzer

    SBC: ENVIRONMENTAL & LIFE SUPPORT TECHNOLOGY            Topic: X303

    Development of a simple method for on-orbit or advanced mission Total Organic Carbon (TOC) monitoring has been a goal for many years. This proposal seeks to develop a method that is, above all else, simple, inexpensive, and maintenance-free. Previous programs to develop flight hardware, including CHeCS, PCWQM, and previous SBIR-funded efforts, failed to produce workable hardware and were relativel ...

    SBIR Phase I 2007 National Aeronautics and Space Administration
  7. Stratospheric Deployment Parafoil

    SBC: PIONEER ASTRONAUTICS            Topic: S406

    The Stratospheric Deployment Parafoil is a proposed technology that will be designed and tested to provide a greatly superior parachute precision delivery system under thin atmosphere conditions, including Mars entry. Current systems incorporate a parachute which lacks the controllability necessary for precision landing. The non-controllable parachutes act only as a delivery system but afford no ...

    SBIR Phase I 2007 National Aeronautics and Space Administration
  8. Advanced Gashopper Mobility Technology

    SBC: PIONEER ASTRONAUTICS            Topic: S101

    The Mars Gas Hopper, or "gashopper" is a novel concept for propulsion of a robust Mars flight and surface exploration vehicle that utilizes indigenous CO2 propellant to enable greatly enhanced mobility. The gashopper will first retrieve CO2 gas from the Martian environment to store it in liquid form at a pressure of about 10 bar. When enough CO2 is stored to make a substantial flight to another Ma ...

    SBIR Phase I 2007 National Aeronautics and Space Administration
  9. Integrated MLI: Advanced Thermal Insulation Using Micro-Molding Technology

    SBC: Quest Product Development Corporation            Topic: X901

    Current Multilayer Insulation (MLI) technology is over 50 years old, and is typically comprised of 10 to 120 layers of metalized polymer films separated by polyester netting. MLI is the best thermal insulation in a vacuum, and is the insulation of choice for spacecraft and cryogenic system insulation, but has problems relating to density control and performance, application labor, and difficulty c ...

    SBIR Phase I 2007 National Aeronautics and Space Administration
  10. Self-Regulating Freezable Heat Exchanger and Radiator

    SBC: TDA RESEARCH, INC.            Topic: T501

    At present, both the astronaut's metabolic heat and that produced by the Portable Life Support System are rejected to space by a sublimator that consumes up to 8 pounds of water per use; the single largest expendable during an eight-hour EVA. Unfortunately, this will not be acceptable for lunar and interplanetary missions where resupply is difficult. We can greatly reduce the water consumption b ...

    STTR Phase I 2007 National Aeronautics and Space Administration
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