Innovative Scientific Solutions, Inc.

Basic Information

OH
Dayton, OH, 45440-3638

http://www.innssi.com

Company Profile

n/a

Additional Details

Field Value
DUNS: 884812025
Hubzone Owned: N
Socially and Economically Disadvantaged: N
Woman Owned: N
Number of Employees: 75


  1. Fast Pressure-Sensitive Paint System for Production Wind Tunnel Testing

    Amount: $124,923.00

    Significant advances in the use of fast responding Pressure-Sensitive Paint have recently been achieved as demonstrated by a multi-camera fast PSP test conducted in the 16 foot transonic wind tunnel a ...

    SBIR Phase I 2015 National Aeronautics and Space Administration
  2. Aircraft Wheel-Tire Dynamic Interface Pressure

    Amount: $147,047.00

    ABSTRACT: A new sensor for the measurement of ground reaction forces that terminate into the aircraft wheel-tire interface is proposed. Current measurement methods are limited to capturing normal for ...

    SBIR Phase I 2014 Air ForceDepartment of DefenseDepartment of Defense
  3. Arc jet Test-Article Surface Recession Rate Monitor

    Amount: $149,769.00

    ABSTRACT: Quantitative ablation recession rate measurements of heat shield surfaces are essential for evaluating the performance of heat shield materials. Currently, these measurements are limited to ...

    SBIR Phase I 2014 Air ForceDepartment of DefenseDepartment of Defense
  4. Fast Responding Pressure-Sensitive Paint for Large-Scale Wind Tunnel Testing

    Amount: $749,875.00

    The proposed work focuses on implementing fast-response pressure-sensitive paint for measurements of unsteady pressure in rotorcraft applications. Significant rotorcraft problems such as dynamic stall ...

    SBIR Phase II 2014 National Aeronautics and Space Administration
  5. Fast Responding Pressure-Sensitive Paint for Large-Scale Wind Tunnel Testing

    Amount: $123,670.00

    The proposed work focuses on implementing fast-response pressure-sensitive paint for measurements of unsteady pressure in rotorcraft applications. Significant rotorcraft problems such as dynamic stall ...

    SBIR Phase I 2013 National Aeronautics and Space Administration
  6. Hypersonic Propulsion: Improvements in Controls and Instrumentation

    Amount: $749,913.00

    ABSTRACT: Among the technical challenges associated with current Air Force scramjet technology development is coupling between the combustor and isolator that leads to isolator unstart. Performance i ...

    SBIR Phase II 2013 Department of DefenseAir ForceDepartment of Defense
  7. Fast Responding Pressure-Sensitive Paint for Large-Scale Wind Tunnel Testing

    Amount: $124,835.00

    The proposed work focuses on implementing fast-response pressure-sensitive paint for measurements of unsteady pressure in rotorcraft applications. Significant rotorcraft problems such as dynamic stall ...

    SBIR Phase I 2012 National Aeronautics and Space Administration
  8. Skin Friction and Pressure Measurements in Supersonic Inlets

    Amount: $124,835.00

    Supersonic propulsion systems include internal ducts, and therefore, the flow often includes shock waves, shear layers, vortices, and separated flows. Passive flow control devices such as micro-vortex ...

    SBIR Phase I 2012 National Aeronautics and Space Administration
  9. Simultaneous Skin Friction and Pressure Sensitive Paint

    Amount: $123,500.00

    Currently, the contribution of skin friction to the total drag of a wind tunnel model is estimated by comparing measurements of the total drag to the integrated pressure drag. While this yields an est ...

    SBIR Phase I 2012 National Aeronautics and Space Administration
  10. Hypersonic Propulsion: Improvements in Controls and Instrumentation

    Amount: $149,926.00

    ABSTRACT: Among the technical challenges associated with current Air Force scramjet technology development is coupling between the combustor and isolator that leads to isolator unstart. Performance i ...

    SBIR Phase I 2012 Department of DefenseAir ForceDepartment of Defense

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