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 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
  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: $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
  5. 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
  6. 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
  7. 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
  8. 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
  9. 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
  10. Aircraft Tire Contact Patch Force and Shear Sensor

    Amount: $739,440.00

    ABSTRACT: Military aircraft tires must handle extreme loads during landing, take-off and taxi. New designs must be evaluated to determine if they meet mission capability requirements. A key evaluatio ...

    SBIR Phase II 2012 Department of DefenseAir ForceDepartment of Defense

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