Innovative Scientific Solutions, Inc.

Company Information
Address OH
Dayton, OH, 45440-3638


DUNS: 884812025

# of Employees: 75

Ownership Information

HUBZone Owned: N

Socially and Economically Disadvantaged: N

Woman Owned: N

Award Charts

Award Listing

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

    Amount: $749,706.00

    Ground-based testing resources are essential for the development of aerospace systems. While these facilities can be expensive to maintain and operate, the cost to acquire data can be significantly re ...

    SBIRPhase II2016National Aeronautics and Space Administration
  2. In-Flight Measurements of Spray System Droplet Size for Aerial Chemical Application

    Amount: $99,689.00

    The spray application of pesticides, herbicides, fertilizers and growth regulators produces substantial benefits in crop yields. Aerial spray application of bulk materials offers advantages such as ef ...

    SBIRPhase I2016Department of Agriculture
  3. Development of an Elastomeric Force Balance

    Amount: $124,773.00

    One focus of NASA aerodynamics research is enabling energy efficient flight through drag reduction technologies. A variety of drag reduction techniques have shown promise and are under investigation, ...

    SBIRPhase I2016National Aeronautics and Space Administration
  4. Real Time Gas Turbine Engine Particulate Ingestion Sensor for Particle Size and Composition

    Amount: $79,983.00

    Modern gas turbine engines operating in environments with high particulate concentrations face significant durability, performance, and operability challenges. Ingestion of particulate materials can c ...

    SBIRPhase I2016Department of Defense Navy
  5. Arc jet Test-Article Surface Recession Rate Monitor

    Amount: $749,073.00

    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 t ...

    SBIRPhase II2016Department of Defense Air Force
  6. High-Speed, Two-Dimensional Sensor Suite for Fuel-Air Ratio and Heat-Release Rate for Combustor/Augmentor Stability

    Amount: $149,914.00

    ABSTRACT:The goal of the proposed effort will be to demonstrate a diagnostic technique that can simultaneously measure the combustion progress variable, the flow velocity, and the fuel-to-air ratio wi ...

    SBIRPhase I2015Department of Defense Air Force
  7. Temperature/Heat Flux Imaging of an Aerodynamic Model in High-Temperature, Continuous-Flow Wind Tunnels

    Amount: $149,269.00

    ABSTRACT:Heat transfer is an important quantity that remains difficult to predict using CFD. Phenomena such as transition and separation are difficult to capture with discrete sensors. Temperature-Sen ...

    SBIRPhase I2015Department of Defense Air Force
  8. 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 ...

    SBIRPhase I2015National Aeronautics and Space Administration
  9. Time-resolved Measurements of Temperature and Product Mass Fractions within Detonation-based Combustion Devices at Elevated Pressures and Temperatures

    Amount: $149,923.00

    The Phase I research effort proposed here is to design and demonstrate first-generation laser-absorption-based sensors for time-resolved measurements of combustion-product mass fractions and gas tempe ...

    STTRPhase I2015Department of Defense Navy
  10. 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 I2014Air Force Department of Defense

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