You are here

INNOVATIVE SCIENTIFIC SOLUTIONS INC

Company Information
Address
7610 MCEWEN RD
DAYTON, OH 45459-3908
United States


http://www.innssi.com

Information

UEI: GE6SB9D2NFM3

# of Employees: 111


Ownership Information

HUBZone Owned: No

Socially and Economically Disadvantaged: No

Woman Owned: No



Award Charts




Award Listing

  1. 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 ...

    SBIRPhase I2014Department of Defense Air Force
  2. 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 ...

    SBIRPhase I2014Department of Defense Air Force
  3. 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 ...

    SBIRPhase II2014National Aeronautics and Space Administration
  4. 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 ...

    SBIRPhase II2013Department of Defense Air Force
  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 ...

    SBIRPhase I2013National Aeronautics and Space Administration
  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 ...

    SBIRPhase I2012National 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 ...

    SBIRPhase I2012National 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 ...

    SBIRPhase I2012National 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 ...

    SBIRPhase I2012Department of Defense Air Force
  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 ...

    SBIRPhase II2012Department of Defense Air Force
US Flag An Official Website of the United States Government