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ADVANCED COOLING TECHNOLOGIES INC

Company Information
Address
1046 NEW HOLLAND AVE
LANCASTER, PA 17601-5606
United States


http://www.1-ACT.com

Information

UEI: Z8KVZV3DR7J4

# of Employees: 241


Ownership Information

HUBZone Owned: No

Socially and Economically Disadvantaged: No

Woman Owned: No



Award Charts




Award Listing

  1. An Innovative VOCs Incinerator

    Amount: $149,989.00

    An innovative, high destruction efficiency, and low fuel consumption VOCs incinerator is proposed to reduce VOCs from condensate tank, or other low heat value waste gas emissions from different air po ...

    SBIRPhase I2014Department of Energy
  2. High Accuracy, Turnkey, Minimum Hot Surface Ignition Test Apparatus

    Amount: $150,000.00

    ABSTRACT: This Small Business Innovation Research (SBIR) Phase I project proposes to develop and demonstrate a test apparatus for determining the minimum hot surface ignition (HSI) temperature of fla ...

    SBIRPhase I2014Department of Defense Air Force
  3. Highly Efficient, Compact Hydrogen Generator for use in Marine Diesel Engines

    Amount: $149,953.00

    The proposed study will investigate several technology concepts capable of producing hydrogen on site from water and supplying it to an operating marine diesel engine. Addition of a small amount of hy ...

    SBIRPhase I2014Department of Defense Special Operations Command
  4. Low Cost Radiator for Fission Power Thermal Control

    Amount: $749,910.00

    NASA GRC is developing fission power system technology for future space transportation and surface power applications. The early systems are envisioned in the 10 to 100kWe range and have an anticipate ...

    SBIRPhase II2014National Aeronautics and Space Administration
  5. Titanium-Water Heat Pipe Radiator for Spacecraft Fission Power

    Amount: $124,902.00

    The proposed program will develop titanium/water heat pipes suitable for Spacecraft Fission Power. NASA is examining small fission power reactors for future space applications with the most recent be ...

    SBIRPhase I2014National Aeronautics and Space Administration
  6. Variable Heat Rejection Loop Heat Pipe radiator

    Amount: $124,976.00

    Thermal control systems are sized for the maximum heat load in the warmest continuous environment. This design process results in a larger radiator surface area than is needed for portions of a missi ...

    SBIRPhase I2014National Aeronautics and Space Administration
  7. Vapor Chamber with Phase Change Material-Based Wick Structure for Thermal Control of Manned Spacecraft

    Amount: $124,994.00

    In response to NASA SBIR solicitation H3.01 "Thermal Control for Future Human Exploration", Advanced Cooling Technologies, Inc. (ACT) is proposing a novel Phase Change Material (PCM) vapor chamber to ...

    SBIRPhase I2014National Aeronautics and Space Administration
  8. Hybrid Heat Pipes for High Heat Flux Applications

    Amount: $124,936.00

    The thermal transport requirements for future spacecraft missions continue to increase, approaching several kilowatts. At the same time the heat acquisition areas have trended downward, thereby increa ...

    SBIRPhase I2014National Aeronautics and Space Administration
  9. Low Mass, Two-Phase Thermal Switch

    Amount: $124,338.00

    Future human spacecraft will venture far beyond the relatively benign environment of low Earth orbit. They will transit through the deep space, but they may encounter warm transient environments such ...

    SBIRPhase I2014National Aeronautics and Space Administration
  10. A Sulfur Tolerant Non-catalytic Reformer

    Amount: $99,888.00

    A non-catalytic JP-8 reformer is proposed. The Swiss Roll reformer very effectively recirculates heat to optimize the reforming efficiency of thermal partial oxidation reaction without involving any ...

    SBIRPhase I2014Department of Defense Army
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