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The Award database is continually updated throughout the year. As a result, data for FY19 is not expected to be complete until April, 2020.

  1. Rapid Development of Thermodynamic Capability for Integrated Computational Materials Engineering

    SBC: Computherm, LLC            Topic: AF15AT30

    ABSTRACT: CompuTherm, LLC proposes a pilot project to develop an innovative modeling tool for rapid deployment of thermodynamic capability for Integrated Computational Materials Engineering (ICME). To be developed on the basis of CompuTherms current capability, Pandat software, the proposed modeling tool represents the next generation of CALPHAD software. The significant advances of the proposed m ...

    STTR Phase I 2015 Department of DefenseAir Force
  2. Skin Substitute Technology for Chimeric Autologous/Allogeneic Constructs for Skin Regeneration- Preclinical Studies

    SBC: Stratatech Corporation            Topic: OSD11H10

    Complex skin defects, including burns and trauma, represent a major medical problem affecting both military and civilian populations. In recent military engagements, burns account for approximately 5% of combat casualties. Furthermore, approximately 1.25 million Americans each year require medical attention for complex skin defects, with 50,000 people hospitalized for burns and 13,000 requiring sk ...

    SBIR Phase II 2015 Department of DefenseDefense Health Program
  3. High Performance Low Integration Cost Magnetometer System

    SBC: A&E INNOVATION            Topic: AF083218

    An innovative data collection and analysis approach is proposed to enable body mount magnetometers for space application. In order to achieve high accurate magnetic field measurement in space, the magnetometer has to be located in a âmagnetically cleanâ place, where the magnetic field from spacecraft is negligible. Usually, the magnetometers are placed on deployable booms, so that the field sens ...

    SBIR Phase I 2009 Department of DefenseAir Force
  4. Accelerated Development of High-Performance Mo-Si-B-X Alloys via an Approach of Integrating Thermodynamic Modeling with Experimental Study

    SBC: Computherm, LLC            Topic: AF07T003

    The proposed study aims at accelerated development of Mo-Si-B-X (X=Ti, Zr, Hf, Re, Mn) alloys with an optimized balance of properties, via an approach of integrating thermodynamic modeling with experimental study.   On the basis of the Mo-Si-B-X (X=Ti, Zr, Hf) database developed in Phase I, a thermodynamic database of the Mo-Si-B-O-X (X=Ti, Zr, Hf, Re, Mn) system will be developed using the Calp ...

    STTR Phase II 2009 Department of DefenseAir Force
  5. A Modeling Tool for Predicting the Durability of Environmental Barrier Coatings (EBC) for Ceramic Matrix Composites (CMC)

    SBC: Computherm, LLC            Topic: AF083070

    CompuTherm, LLC proposes a pilot project to develop a modeling tool that can be used to assess the durability of environmental barrier coatings (EBCs) for ceramic matrix composites (CMCs) under combustion environment. The modeling tool includes a thermodynamic database for the gas phase, a thermodynamic database for the silicate system (EBCs), and a computer software package that deals with thermo ...

    SBIR Phase I 2009 Department of DefenseAir Force
  6. Energetic Polyazide Materials

    SBC: Orbital Technologies Corporation            Topic: AF08T022

    Orbital Technologies Corporation and Penn State University propose to examine and characterize novel energetic formulations in solid fuels to replace conventional, low-energy, binders such as HTPB. The proposed solid fuels will provide higher enthalpy, higher density, and improved rocket engine performance. In Phase I, we will calculate theoretical rocket performance of selected materials, chara ...

    STTR Phase I 2009 Department of DefenseAir Force
  7. Self Pressurizing Gas Generator (SPGG)

    SBC: Orbital Technologies Corporation            Topic: AF083111

    Orbital Technologies Corporation (ORBITEC) proposes to develop a monopropellant Self-Pressurizing Gas Generator (SPGG) warm gas pressurization system for satellite propulsion system applications.  The SPGG system will utilize a novel method to pressurize the propellant.  The proposed system offers significant advantages over the traditional helium gas pressurization system.  The SPGG will provi ...

    SBIR Phase I 2009 Department of DefenseAir Force
  8. Advanced Microwave Electrothermal Thruster for Dual-Mode Water Rocket Propulsion (AMET-DMWRP)

    SBC: Orbital Technologies Corporation            Topic: AF081065

    ORBITEC proposes to develop the Advanced Microwave Electrothermal Thruster (AMET) for use as one of the primary thrusters in the Dual-Mode Water Rocket Propulsion system.  The AMET uses an electrodeless microwave discharge to produce thrust from water vapor propellant, delivering specific impulse in excess of 800 seconds with a highly efficient process.  Microwave energy is introduced to a reson ...

    SBIR Phase I 2009 Department of DefenseAir Force
  9. Heat Transfer Model for Bubbly Flows

    SBC: Orbital Technologies Corporation            Topic: AF083119

    ORBITEC proposes to develop a heat transfer model to predict heat transfer coefficient in bubbly flows in small tubes.  This model is intended for application to thermal management systems in a variety of propulsion systems, including both air-breathing and rocket engines.  The Phase I work will include parallel experimental and modeling work.  The experimental program will measure heat transfe ...

    SBIR Phase I 2009 Department of DefenseAir Force
  10. Injector Stability Screening Technique (ISST)

    SBC: Orbital Technologies Corporation            Topic: AF083112

    ORBITEC proposes to demonstrate and validate a laboratory scale experimental injector stability screening technique which will quantify injector element stability characteristics.  The experimental approach promises to dramatically reduce development cost by utilizing a gaseous single element test facility which presents savings in hardware manufacturing, consumables such as propellant and test p ...

    SBIR Phase I 2009 Department of DefenseAir Force

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