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The Award database is continually updated throughout the year. As a result, data for FY21 is not expected to be complete until September, 2022.

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.

  1. Additively Manufactured Bimetallic Combustion Chambers for Small Launch Vehicles

    SBC: Cornerstone Research Group, Incorporated            Topic: Z9

    Arctic Slope Technical Services, Inc. (ASTS) is pleased to propose to continue the development of an additive manufacturing (AM) approach for fabricating bimetallic combustion chambers. Our chamber design, which is applicable to future NASA small launch vehicles, exploits the combined capabilities of selective laser melting (SLM) and magnetic pulse welding (MPW), in order to reduce manufacturing ...

    SBIR Phase II 2018 National Aeronautics and Space Administration
  2. 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
  3. 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
  4. An Additive Manufacturing Technique for the Production of Electronic Circuits

    SBC: MORNINGBIRD MEDIA CORPORATION            Topic: T12

    Under the support of a FY 2016 NASA Phase I Small Business Technology Transfer (STTR) contract (NASA contract number NNX16CM40P), Morningbird Media Corporation in collaboration with Alabama A&M University Research, Innovation in Science and Engineering (AAMU-RISE) Foundation, has devised a unique method for an additive manufacturing technique for the direct 3D printing of functional electronics. T ...

    STTR Phase II 2018 National Aeronautics and Space Administration
  5. 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
  6. A Novel Microfludic Device for Drug Toxicity Studies

    SBC: CFD Research Corporation            Topic: CBD10103

    Current drug discovery and development efforts are severely limited by expensive animal trials and oversimplified in vitro models. Results obtained from in vitro models are not predictive of in vivo toxicity owing to significant difference from the in vivo physiological conditions. In this context, we propose to develop and demonstrate a novel microfluidic device that reproduces the physiological ...

    SBIR Phase II 2011 Department of DefenseOffice for Chemical and Biological Defense
  7. A Novel, Ultra-Light, Heat Rejection System for Nuclear Power Generation

    SBC: CREARE LLC            Topic: X802

    For lunar-based fission power systems that will support In-Situ Resource Utilization (ISRU) or Mars robotic and manned missions, power requirements may vary from 10s to 100s of kWe to support initial human missions and longer term lunar bases. Due to the large amounts of waste heat generated by these systems, a key consideration is the development of lightweight, highly efficient heat rejection s ...

    SBIR Phase II 2008 National Aeronautics and Space Administration
  8. A Two-Phase Pumped Loop Evaporator with Adaptive Flow Distribution for Large Area Cooling

    SBC: CREARE LLC            Topic: S3

    NASA’s future remote sensing science missions require advanced thermal management technologies to maintain multiple instruments at very stable temperatures and utilize waste heat to keep other critical subsystems above minimum operational temperatures. Two-phase pumped loops are an ideal solution for these applications. A critical need for these pumped loops is a microgravity-compatible evaporat ...

    SBIR Phase II 2018 National Aeronautics and Space Administration
  9. Compact Vacuum Pump for Titan Lander Missions

    SBC: CREARE LLC            Topic: S109

    For a number of years Creare has developed, fabricated, and tested highly miniaturized, high vacuum pumps specifically designed for mass spectrometers used on NASA Mars missions. These pumps would also be useful on other missions to planets and satellites with atmosphere, such as Titan, as well as terrestrial applications on Earth. In order to allow these high vacuum pumps to operate in high-pr ...

    SBIR Phase II 2011 National Aeronautics and Space Administration
  10. Computational Tool for Coupled Simulation of Nonequilibrium Hypersonic Flows with Ablation

    SBC: CFD Research Corporation            Topic: X901

    The goal of this SBIR project is to develop a predictive computational tool for the aerothermal environment around ablation-cooled hypersonic atmospheric entry vehicles. This tool is based on coupling the relevant physics models to the LeMANS code for hypersonic flows and to the MOPAR code for material response, both developed by the University of Michigan. In Phase I of this project, we developed ...

    SBIR Phase II 2011 National Aeronautics and Space Administration
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