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The Award database is continually updated throughout the year. As a result, data for the given year is not complete until April of the following year. Annual Reports data is a snapshot of agency reported information for that year and hence might look different from the live data in the Awards Information charts.

  1. Design Environment for Educator-Student Collaboration Allowing Real-Time Engineering-centric, STEM (DESCARTES) Exploration in Middle Grades

    SBC: Parametric Studio, Inc.            Topic: none

    DESCARTES is a game-based engineering environment where students design, test, and build projects, including boats, airplanes, and other models. The web-based student-facing environment will include challenges, topic introductions, tutorials, and tools for analyzing and improving projects. Following completion of a concept in the environment, students will then build and test real world prototypes ...

    SBIR Phase II 2017 Department of EducationInstitute of Education Sciences
  2. The Iowa Assessment of Skills and Knowledge for Automatic Word Recognition and Decoding (iASK)

    SBC: Foundations In Learning, Inc            Topic: edIES15R0008

    Video Demonstration of the Phase I Prototype: http://youtu.be/P716_x5KhPk Purpose: This project team will develop and test iASK, an app intended to assess and support increased word recognition among middle school students who struggle to read. The 2013 National Assessment of Education Progress reported that 66% of middle school students scored below proficient in reading, and 22% scored below ba ...

    SBIR Phase II 2015 Department of EducationInstitute of Education Sciences
  3. A Computational Tool for High Advance Ratio Configurations

    SBC: Sukra Helitek Inc.            Topic: A306

    Newer vertical lift configurations consider speed as an important design parameter with forward speeds upwards of 230 Knots, which is well above the acceptable incompressible flow regime. In such high speed vertical lift configurations, even though the aircraft may be cruising at compressible Mach numbers, incompressible flow pockets can occur in the wake of the fuselage. Hence, in contrast to mos ...

    SBIR Phase I 2014 National Aeronautics and Space Administration
  4. RotCFD: A Viscous Design Tool for Advanced Configurations

    SBC: Sukra Helitek Inc.            Topic: A209

    During initial design studies, parametric variation of vehicle geometry is routine. In addition, rotorcraft engineers traditionally use the wind tunnel to evaluate and finalize designs. Correlation between wind tunnel results and flight tests, when not good, have been often attributed in part to uncertainty in blockage corrections. Estimation of rotor blockage is significantly more complex than bl ...

    SBIR Phase II 2012 National Aeronautics and Space Administration
  5. An Aero-Acoustic Tool for Terminal Area Operations

    SBC: Sukra Helitek Inc.            Topic: A209

    In this highly interconnected world, transportation systems must feature increased flexibility and shorter door-to-door trip times to be successful. Shorter door-to-door trip times require an increased usage of rotary wing and runway independent V/STOL technology. One of the limiting factors to the increased adoption of this technology for providing feeder service to major hubs is the limited un ...

    SBIR Phase I 2012 National Aeronautics and Space Administration
  6. RotCFD: A Viscous Design Tool for Advanced Configurations

    SBC: Sukra Helitek Inc.            Topic: A209

    The incorporation of viscous analysis in design is vital for a completeunderstanding of aerodynamic problems.This proposal offers to develop and integrate with RotCFD a method for semi-automatically generating grids suitable for viscous analysis on complex configurations as well as parallelize the solver in RotCFD to take advantage of today's multi-core machines. The principle idea behind th ...

    SBIR Phase I 2011 National Aeronautics and Space Administration
  7. Computational Wind Tunnel: A Design Tool for Rotorcraft

    SBC: Sukra Helitek Inc.            Topic: A210

    During initial design studies, parametric variation of vehicle geometry is routine. In addition, rotorcraft engineers traditionally use the wind tunnel to evaluate and finalize designs. Estimation of rotor tunnel blockage is significantly more complex than bluff body corrections as the correction depends on operational characteristics such as rotor RPM and thrust produced. This proposal offers to ...

    SBIR Phase II 2009 National Aeronautics and Space Administration
  8. Computational Wind Tunnel: A Design Tool for Rotorcraft

    SBC: Sukra Helitek Inc.            Topic: A210

    Rotorcraft engineers traditionally use the wind tunnel to evaluate and finalize designs. Insufficient correlation between wind tunnel results and flight tests, have been often attributed in part to uncertainty in blockage corrections. Estimation of rotor blockage is significantly more complex than bluff body blockage as the correction depends on operational characteristics such as rotor RPM and ...

    SBIR Phase I 2008 National Aeronautics and Space Administration
  9. High Temperature Telemetry Transmitter for Venus Exploration

    SBC: SOFTRONICS, LTD.            Topic: S402

    The proposed S-band telemetry transmitter will operate in the exterior Venusian high pressure, 465?aC ambient atmosphere without being contained in a thermally protective container. The sealed, radiation-hardened, high-reliability, silicon-carbide-based transmitter uses an ambient heatsink to cool its high temperature transistors without the power, volume, and weight of auxiliary cooling. An inn ...

    SBIR Phase II 2006 National Aeronautics and Space Administration
  10. Development of a Multipurpose Extruder/Press Food Processing System

    SBC: Triple F, Inc.            Topic: B304

    This project is to develop versatile, low mass, energy efficient, and easily maintained multipurpose seed processing (MSP) equipment for food processing in space environments. Phase-1 of the project yielded a conceptual drawing for a MSP. Phase-II consists of six main tasks. The first model MSP will be manufactured, programmed and tested for ESM, function, and quality of processed product. The ...

    SBIR Phase II 2006 National Aeronautics and Space Administration

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