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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 Compact Safe Cold-Start (CS2) System for Scramjets using Dilute Triethylaluminum Fuel Mixtures

    SBC: ACENT LABORATORIES LLC            Topic: A202

    This proposal leverages a highly successful Phase 1 feasibility effort to further develop a system that satisfies the cold-start requirements of scramjet engines. The system provides energy-dense, low volume hydrocarbon fuel conditioning based on the hydrolysis reaction of triethylaluminum (TEA) with water. TEA is an organometallic liquid that reacts exothermically with water and burns readily i ...

    SBIR Phase II 2011 National Aeronautics and Space Administration
  2. Acoustic Interactions with Spray Combustion in Liquid Propellant Rocket Thrust Chambers

    SBC: CFD RESEARCH CORPORATION            Topic: N/A

    N/A

    SBIR Phase I 1993 National Aeronautics and Space Administration
  3. Active High-Temperature Superconductor Circuits for Integrated Microwave Receivers and Antenna Arrays

    SBC: Parkview Research &            Topic: N/A

    N/A

    SBIR Phase I 1993 National Aeronautics and Space Administration
  4. Adaptive Aeroservoelastic Suppression for Aircraft Upset and Damage Conditions

    SBC: Impact Technologies            Topic: A107

    Impact Technologies, in collaboration with Tennessee State University, propose to develop and demonstrate an adaptive system identification and multi-loop control methodology that provides real-time aircraft structural mode suppression associated with aeroservoelastic interaction under upset and damage conditions. The proposed program will develop an effective real-time aircraft structural model, ...

    SBIR Phase I 2011 National Aeronautics and Space Administration
  5. Advanced Carbothermal Electric Reactor

    SBC: Orbital Technologies Corporation            Topic: X301

    The overall objective of the Phase 1 effort was to demonstrate the technical feasibility of the Advanced Carbothermal Electric (ACE) Reactor concept. Unlike state-of-the-art carbothermal reactors that use concentrated solar energy and/or laser energy to heat the regolith, the ACE Reactor uses an innovative method to electrically heat the regolith to temperatures over 1800ºC within a thermally ins ...

    SBIR Phase II 2011 National Aeronautics and Space Administration
  6. Aerodynamic Modeling with Heterogeneous Data Assimilation and Uncertainty Quantification

    SBC: CLEAR SCIENCE CORP            Topic: A205

    Clear Science Corp. proposes to develop an aerodynamic modeling tool that assimilates data from different sources and facilitates uncertainty quantification. The technical merit and feasibility of the technology will be demonstrated in Phase I through a series of verification and validation tests that utilize both computational and wind tunnel data in constructing aerodynamic models for the Orion ...

    SBIR Phase I 2011 National Aeronautics and Space Administration
  7. Aero-Effected Distributed Adaptive Control of Flexible Aircraft Using Active Bleed

    SBC: Atair Aerospace, Inc            Topic: A207

    The proposed research focuses on the development of a new adaptive control methodology for active control of wing aerodynamic shape to effect distributed aerodynamic forces and moments for maneuvering and stabilization of flexible airframes without moving control surfaces. The new aero-effected flight control will be achieved using output feedback adaptive control of distributed bleed across aero ...

    SBIR Phase I 2011 National Aeronautics and Space Administration
  8. A High Order Accuracy Computational Tool for Unsteady Turbulent Flows and Acoustics

    SBC: Frendi Research Corporation            Topic: A206

    The main objective of this research effort is to develop a higher order unsteady turbulent flow solver based on the FDV method, and to exploit its attributes of spanning the whole Mach number range.The well known advantages of the implicit FEM will be inherited along with robust boundary conditions implementation and sound mathematical bases. Efficient parallelization, using MPI through domain dec ...

    SBIR Phase I 2011 National Aeronautics and Space Administration
  9. A Light Weight, Mini Inertial Measurement System for Position and Attitude Estimation on Dynamic Platforms

    SBC: Impact Technologies            Topic: O405

    Impact Technologies, LLC in collaboration with the Rochester Institute of Technology, proposes to develop and demonstrate a flight-worthy hardware prototype of a miniature, low cost/weight/ power device that provides stable and highly accurate near continuous positioning, attitude, and inertial measurements while being subjected to highly dynamic maneuvers and high vibration effects. In contrast t ...

    SBIR Phase II 2011 National Aeronautics and Space Administration
  10. A Miniaturized Sensor for Microbial Monitoring of Spacecraft Water Environment

    SBC: CFD RESEARCH CORPORATION            Topic: X203

    Accurate real-time microbial monitoring of water environment is of paramount importance to crew health as well as to ensure proper functioning and control of the life support system during space exploration. The existing methods are time-consuming and labor-intensive, and the devices used are bulky, consumable-hungry, and ill-suited for spacecraft deployment. We propose to develop and demonstrate ...

    SBIR Phase II 2011 National Aeronautics and Space Administration
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