Gloyer-Taylor Laboratories LLC

Basic Information

TN
Tullahoma, TN, 37388-5583

http://www.gtlcompany.com

Company Profile

n/a

Additional Details

Field Value
DUNS: 144158677
Hubzone Owned: N
Socially and Economically Disadvantaged: N
Woman Owned: N
Number of Employees: 16


  1. CNT enhanced KineticCore FES system

    Amount: $79,918.00

    The introduction of USN electric ship initiatives and advanced weapons systems such as rail guns, lasers, and other future pulse loads to future warships creates power and energy demands that exceed w ...

    SBIR Phase I 2015 Department of DefenseNavyDepartment of Defense
  2. UCDS for Augmentor Damping

    Amount: $149,963.00

    ABSTRACT:Combustion instability (aka thermoacoustic instability) is a significant issue in propulsion systems including augmentors. Oscillations can increase heat transfer to walls 10 fold and cause v ...

    SBIR Phase I 2015 Department of DefenseAir ForceDepartment of Defense
  3. ACE Booster

    Amount: $124,929.00

    GTL has been developing three transformational technologies that have the capability to disrupt the traditional launch vehicle paradigm. BHL composite cryotank technology provides a four times improv ...

    STTR Phase I 2014 National Aeronautics and Space Administration
  4. Advanced Solid Ramjet Fuel

    Amount: $79,988.00

    The potential for solid fuel ramjets (SFRJ) has been demonstrated over the last 40 years. SRFJ"s have significantly higher impulse than rockets (Isp>1200 sec) making them a competitive solutio ...

    SBIR Phase I 2014 NavyDepartment of DefenseDepartment of Defense
  5. Augmentor Stability

    Amount: $149,962.00

    ABSTRACT: As with all other combustion devices, the augmentors in high-performance gas turbine engines are at risk of combustion instability. While it is tempting to apply brute force CFD to address ...

    SBIR Phase I 2013 Department of DefenseAir ForceDepartment of Defense
  6. High Pressure Breathing System

    Amount: $79,951.00

    GTL proposes to develop a small diameter High Pressure Breathing Apparatus concept design capable of achieving 10,000-psi operating pressures. The HPBA incorporates a high-pressure regulator and valve ...

    SBIR Phase I 2013 NavyDepartment of DefenseDepartment of Defense
  7. Nonlinear Data Analysis Tool for Scramjets and Other Engines

    Amount: $124,861.00

    The UCDS process is the result of 50 years of research into combustion instability by the worlds leading scientists and engineers. The breakthroughs that created UCDS have provided a solid analytical ...

    SBIR Phase I 2012 National Aeronautics and Space Administration
  8. UCDS Unsteady Reaction Model

    Amount: $999,946.00

    The overall objective of the Phase II effort is to enhance the capability of the UCDS process to simulate and predict the characteristics of combustion instability in propulsion devices, specifically ...

    STTR Phase II 2012 Department of DefenseMissile Defense AgencyDepartment of Defense
  9. Advanced Flywheel

    Amount: $99,919.00

    The Advanced FlywheelTM (AF) technology utilizes an innovative configuration in conjunction with modern materials to deliver a flywheel energy storage system with an energy density in excess of 500 W- ...

    SBIR Phase I 2012 Department of DefenseDefense Advanced Research Projects AgencyDepartment of Defense
  10. SMFB Technology

    Amount: $999,945.00

    In the Phase II effort, GTL will build upon the foundation provided by the Phase I effort to develop a family of SMFB products that can be used by thermoplastic matrix composite (TPMC) developers and ...

    SBIR Phase II 2012 ArmyDepartment of DefenseDepartment of Defense

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