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Concepts NREC, LLC

Company Information
Address
217 Billings Farm Rd
White River Junction, VT 05001-9486
United States


http://www.conceptsnrec.com

Information

UEI: PKMJNWK4V2U1

# of Employees: 87


Ownership Information

HUBZone Owned: No

Socially and Economically Disadvantaged: No

Woman Owned: No



Award Charts




Award Listing

  1. Extremely High Suction Performance Inducers for Space Propulsion

    Amount: $100,000.00

    Advanced pump inducer design technology that uses high inlet diffusion blades, operates at a very low flow coefficient, and employs a cavitation control and stability device. A preliminary scoping in ...

    STTRPhase I2010National Aeronautics and Space Administration
  2. Recovery Act- Development of a Wave Energy-Responsive, Self-Acuated Blade Articulation Mechanism for an OWC Turbine

    Amount: $149,789.00

    An oscillating water-air column (OWC) is one of the most technically viable and efficient options for converting wave energy into useful electric power. However, there is a need to increase the overal ...

    SBIRPhase I2010Department of Energy
  3. Development of a Self-Adaptive Air Turbine for Wave Energy Conversion using an Oscillaating Water Column (OWC) Air System

    Amount: $99,239.00

    The oscillating water column (OWC) is a candidate technology for the economical recovery of the projected 17.5 x 1012 kW-hr energy that is available from the world┬┐s oceans. While the relative dynam ...

    STTRPhase I2009Department of Energy
  4. Knowledge-Based Multi-Diciplinary Optimization of Rocket Turbopump Design

    Amount: $1,049,400.00

    The design of turbomachinery components is a complex process requiring many steps and hundreds of minute decisions in an iterative process. The design proceeds from engine cycle performance and meanli ...

    SBIRPhase II2005Department of Defense Air Force
  5. Dynamic Transfer Function Measurements for Cavitating Pumps

    Amount: $599,997.00

    The Phase I effort demonstrated the feasibility of measuring cavitating inducer dynamic transfer functions using an upgraded Concepts NREC pump test facility. As there are no analytical tools or expe ...

    SBIRPhase II2004National Aeronautics and Space Administration
  6. Knowledge-Based Multi-Diciplinary Optimization of Rocket Turbopump Design

    Amount: $99,720.00

    The design of turbomachinery components is a complex process requiring many steps and hundreds of minute decisions in an iterative process. The design proceeds from meanline design through 3D viscous ...

    SBIRPhase I2004Department of Defense Air Force
  7. High Suction Specific Speed Inducers for Cryogenic Upper Stage Engines

    Amount: $749,827.00

    There is a significant opportunity to meet higher upper stage engine performance levels by combining a much higher chamber pressure expander cycle engine with advanced technology turbomachinery. The ...

    SBIRPhase II2003Department of Defense Air Force
  8. Intelligent Virtual Rotor-Bearing System Design

    Amount: $99,904.00

    Lateral analysis of multi-level or multi-spool turbofan and turbojet engines has been regularly performed for more than 30 years by commercial engine manufacturers. Similarly, engine bearing designer ...

    SBIRPhase I2003Department of Defense Air Force
  9. Dynamic Transfer Function Measurements for Cavitating Pumps

    Amount: $69,996.00

    There are no analytical tools or experimental facilities in the world today that can quantify the dynamic transfer function for a cavitating inducer. The goal of this research is to fill this void. An ...

    SBIRPhase I2003National Aeronautics and Space Administration
  10. Advanced Cooling Techniques for Hydrocarbon Liquid Rocket Engine Components

    Amount: $99,973.00

    Developing new techniques for combustion chamber cooling are critical to increasing engine life to 60 missions or greater. Concepts NREC will explore several chamber cooling options that minimize or ...

    SBIRPhase I2003Department of Defense Air Force
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