You are here

Award Data

For best search results, use the search terms first and then apply the filters
Reset

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. AERODYNAMIC HEATING UPGRADE OF THE PARABOLIZED NAVIER-STOKES(PNS) CODE

    SBC: Remtech Inc.            Topic: N/A

    THIS EFFORT WILL ENHANCE THE CAPABILITY OF THE AIR FORCE PARABOLIZED NAVIER STOKES CODE (AFWAL PNS CODE) TO PREDICT SKIN FRICTION AND HEAT TRANSFER TO HIGH SPEED FLIGHT VEHICLES. THE CURRENT PREDICTION TECHNIQUES REQUIRE EXTREMELY ACCURATE CALCULATIONS OF VELOCITY AND TEMPERATURE IN THE VICINITY OF THE WALL. THE EFFORT HERE WILL REPLACE THIS PROCEDURE BY USING INTEGRAL MOMENTUM AND ENERGY EQUATION ...

    SBIR Phase II 1987 National Aeronautics and Space Administration
  2. AN ALL-METAL COMPACT HEAT EXCHANGER FOR SPACEBORNE CRYOCOOLERS

    SBC: CREARE LLC            Topic: N/A

    THE OVERALL CYCLE EFFICIENCY (HENCE, INPUT POWER REQUIREMENTS) OF REVERSE-BRAYTON CRYOCOOLERS FOR SPACE APPLICATIONS IS HIGHLY SENSITIVE TO THE THERMAL EFFECTIVENESS OF THE HEAT EXCHANGERS. APPLICATIONS FOR THESE CRYOCOOLERS IN SPACE DICTATE THAT THESE HEAT EXCHANGERS BE AS SMALL AND LIGHT AS POSSIBLE. TO DATE, ONLYHEAT EXCHANGERS EMPLOYING ORGANIC MATERIALS HAVE BEEN ABLE TO ACHIEVE THE HIGH THER ...

    SBIR Phase II 1987 National Aeronautics and Space Administration
  3. Analysis Tools for Detection and Diagnosis of Biological Threats

    SBC: ALPHA-GAMMA TECHNOLOGIES, INC.            Topic: CBD04113

    DNA microarray technology, in combination with statistical and predictive modeling tools, could be used to evaluate thousands of genes against distinct gene expression patterns induced by chemical/biological agents to provide early identification and speed therapeutic intervention. The overall objective of this Phase II effort is to leverage existing public domain resources and commercial tools t ...

    SBIR Phase II 2005 Department of DefenseOffice for Chemical and Biological Defense
  4. A Novel Microfluidic Device for Fully Automated Extraction of RNA from Cell Cultures

    SBC: CFD RESEARCH CORPORATION            Topic: B203

    Obtaining high quality, intact RNA from cells is an ubiquitous need in the pursuit of space biology. Our overall objective is to develop and commercialize a microfluidics based miniaturized platform (MED-RNA) that can fully automate the complex process of RNA isolation. Starting from harvested whole mammalian cells in a culture medium, MED-RNA will lyse, capture, and isolate RNA content for later ...

    SBIR Phase II 2005 National Aeronautics and Space Administration
  5. A Novel Radiation Shielding Material

    SBC: Plasma Processes, LLC            Topic: B306

    Radiation shielding simulations showed that epoxy loaded with 10-70% polyethylene would be an excellent shielding material against GCRs and SEPs. Milling produced an elemental boron coating on the polyethylene particles suitable for protecting against low energy neutrons. For up to 30 volume percent particle loading of the composite there was the near random distribution of particles needed to p ...

    SBIR Phase II 2005 National Aeronautics and Space Administration
  6. Automated Computational Fluid Dynamics Design With Shape Optimization

    SBC: Optimal Solutions Software, LLC            Topic: A405

    Computational fluid dynamics (CFD) is used as an analysis tool to help the designer gain greater understanding of the fluid flow phenomena involved in the components being designed. The next step in the design process is to modify the design to improve the components performance, typically performed manually by the designer in a trial and error fashion. The innovations proposed herein will provide ...

    SBIR Phase II 2005 National Aeronautics and Space Administration
  7. AUTOMATIC FIRE DETECTION SYSTEM FOR LARGE FACILITIES

    SBC: Spectra Research, Inc.            Topic: N/A

    THE OBJECTIVE OF THIS PROJECT IS A NEW CONCEPT FOR IMPROVED FIRE DETECTION SYSTEMS FOR LARGE, HIGH CEILING, HIGH VOLUME FACILITIES SUCH AS THE ORBITER PROCESSING FACILITY. EMPHASIS IS PLACED ON SYSTEMS WHICH ARE ECONOMICAL, HIGHLY RELIABLE, HAVE RAPID RESPONSE TIMES, AND MINIMIZE FALSE ALARMS. THE ADVANCED DESIGN CONCEPT ASSESSED INCLUDES MULTISPECTRAL SENSORS AND THE CROSS CORRELATION OF SENSOR S ...

    SBIR Phase II 1984 National Aeronautics and Space Administration
  8. Carbon Nanotube Based Electric Propulsion Thruster with Low Power Consumption

    SBC: XINTEK, INC.            Topic: A502

    Field emission electric propulsion (FEEP) thrusters have gained considerable attention for spacecrafts disturbance compensation because of excellent characteristics. The application of current FEEP has been slow in developing mainly caused by high specific power, which limit the milli-Newton thruster development due to insufficient onboard power. Dramatic field improvement from nanometer carbon ...

    SBIR Phase II 2005 National Aeronautics and Space Administration
  9. Cryogenic Cooling System for Zero-Venting Storage of Supercritical Air Packs

    SBC: CREARE LLC            Topic: F302

    Supercritical air at cryogenic temperature is an attractive source of breathing air because of its very high density and low pressure. However, heat leak into the cryogenic tank causes the stored air to expand and vent, thus limiting the storage life of a charged system. We propose to develop a storage system for supercritical air packs that provides cryogenic cooling that will enable long-term ...

    SBIR Phase II 2005 National Aeronautics and Space Administration
  10. Effect of Ambipolar Potential on the Propulsive Performance of the GDM Plasma Thruster

    SBC: Reisz Engineers            Topic: T801

    The Gasdynamic Mirror (GDM) thruster is an electric propulsion device, without electrodes, that will magnetically confine a plasma with such density and temperature as to make the ion-ion collision mean free path much shorter than its length, but the macroscopic time scale is smaller than the characteristic time for electron-ion equilibrium. So, the electrons and ions have different temperatures a ...

    STTR Phase II 2005 National Aeronautics and Space Administration
US Flag An Official Website of the United States Government