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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. A BIOREACTOR FOR SCRENNING AND PRODUCTION OF HIGH VALUE SECONDARY PLANT METABOLITES

    SBC: Phytoresource Research Inc            Topic: N/A

    THE BIOCHEMICAL AND SYNTHETIC CAPACITY OF HIGHER PLANTS, AS SHOWN BY THEIR NATURAL CONTENT OF SUBSTANCES, HAS BEEN USED FOR CENTURIES IN SUPPLYING MATERIALS IMPORTANT IN PHARMACOLOGY AND IN FLAVORS AND FRAGRANCES. MANY OF THESE SECONDARY PRODUCTS ARE IN SHORT SUPPLY AND AN ENORMOUS EFFORT HAS TO BE EXTENDED TO GET THEM. ATTEMPTS TO USE CELL CULTURES OF HIGHER PLANTS AS A MEANS OF PRODUCING SECONDA ...

    SBIR Phase I 1987 National Aeronautics and Space Administration
  2. 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
  3. Acoustic Reduction of Flow Separation

    SBC: LYNNTECH INC.            Topic: T201

    Airfoils produce more lift and less drag when the boundary layer is attached to the airfoil. With most aircraft there are combinations of airspeed and angle of attack where the boundary layer at least partially detaches from the airfoil. Reducing boundary layer detachment increases lift and reduce drag reducing fuel consumption and improving control for the pilot. Two methods known to improve b ...

    STTR Phase II 2011 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. ADAPTIVE COMPUTATIONAL METHOD FOR FLUID-STRUCTURE INTERACTION IN INTERNAL FLOWS

    SBC: Computational Mechan            Topic: N/A

    SUPER ACCURATE ADAPTIVE COMPUTATIONAL SCHEMES FOR THE ANALYSIS OF FLUID STRUCTURE INTERACTION AND COMPLEX THREE-DIMENSIONAL INTERNAL FLOWS ARE TO BE DEVELOPED. NEW PETROV-GALERKIN FINITE ELEMENT METHODS FOR SOLVING THE NAVIER-STOKES EQUATIONS. COUPLED WITH THE EQUATIONS OF MOTION OF ELASTIC DUCTS AND MANIFOLDS, ARE TO BE DEVELOPED AND USED TO SIMULATE FLOWS IN AEROSPACE PROPULSION SYSTEMS (SUCH AS ...

    SBIR Phase II 1987 National Aeronautics and Space Administration
  6. A Direct Methane Solid Oxide Fuel Cell (DMSOFC)

    SBC: LYNNTECH INC.            Topic: X801

    Producing return fuel on Mars rather than carrying it from Earth significantly reduces the mass that must be lifted from Earth for a manned mission to Mars. The most practical propulsion combination that can be produced is methane and oxygen. Using propellant components made on Mars to generate electric power on the return voyage further reduces the mass that must be lifted.We are proposing to d ...

    SBIR Phase I 2011 National Aeronautics and Space Administration
  7. ADVANCED HELIUM NAGNETOMETERS FOR SPACE APPLICATIONS

    SBC: POLATOMIC, INC.            Topic: N/A

    THE GOAL OF PHASE I IS DEVELOPMENT OF AN ADVANCED OPTICALLY PUMPED HELIUM MAGNETOMETER CONCEPT. THIS INSTRUMENT WILL MEASURE MAGNETIC FIELDS IN THE 1 TO 10-8 GAUSS RANGE WITH ORDER OF MAGNITUDE IMPROVEMENTS IN SENSITIVITY AND ABSOLUTE ACCURACY OVER EXISTING MAGNETOMETERS. OPTICALLY PUMPED HELIUM ISOTOPES CAN BE OPTICALLY PUMPED AND USED AS MAGNETOMETERS IN THE FOLLOWING THREE MODES: (1) VECTOR MOD ...

    SBIR Phase II 1987 National Aeronautics and Space Administration
  8. Advanced Modeling Tools for Controlling Complex Assets Across Time Delay

    SBC: Traclabs Inc.            Topic: X601

    The proposed innovation is a hybrid simulation module to replace the current "Behavioral Sim" in JSC's Predictive Interactive Graphical Interface (PIGI). PIGI helps an operator compensate for lunar-scale time delay, and is part of NASA's "RAPID Workbench". The Behavioral Sim acts as an oracle, taking initial conditions and a sequence of commands and producing trajectories and expected f ...

    SBIR Phase II 2011 National Aeronautics and Space Administration
  9. Advanced Oxidation Technology for Potable Water Disinfection

    SBC: LYNNTECH INC.            Topic: X301

    The availability of high-quality potable water is essential in crewed space missions. Closed loop water recycling systems as well as potable water holding tanks and waterlines provide environments for biofilm formation that can facilitate the growth of human pathogens, as well as organisms that can cause deterioration of distribution lines. Prevention requires the maintenance of a chemically stabl ...

    SBIR Phase I 2011 National Aeronautics and Space Administration
  10. Advanced Oxygen Evolution Catalysts for PEM Electrolyzers

    SBC: LYNNTECH INC.            Topic: X703

    Future NASA missions require high efficiency, lightweight, long life, and maintenance-free water electrolyzer technologies to generate oxygen and/or hydrogen for energy storage, propulsion, life-support systems, cabin-oxygen replenishment, and zero-g science activities. International Space Station, future Lunar and Martian Outposts, and future exploration vehicles require high efficiency electrol ...

    SBIR Phase II 2011 National Aeronautics and Space Administration
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