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T T H RESEARCH INC

Company Information
Address
7830 MY WAY
CLIFTON, VA 20124-2000
United States



Information

UEI: KB3BFJ94EQA3

# of Employees: 7


Ownership Information

HUBZone Owned: No

Socially and Economically Disadvantaged: No

Woman Owned: No



Award Charts




Award Listing

  1. Robust Two-Phase Cooling Technology for Megawatt Space-Based Systems

    Amount: $149,991.00

    Loop Heat Pipe (LHP) has been the leading two-phase heat transport technology for space-based thermal control subsystems (TCS) for more than 20 years.nbsp; LHPs are capillary-pumped devices having no ...

    SBIRPhase I2023National Aeronautics and Space Administration
  2. Passive Variable Heat Rejection Freeze-Tolerant Direct Condensation Heat Exchanger/Radiator

    Amount: $124,999.00

    The ever-increasing processing power of spacecraft and satellites puts a tremendous demand on the thermal control subsystem (TCS) to acquire, transport, and reject large amounts of heat.nbsp; Conseque ...

    SBIRPhase I2021National Aeronautics and Space Administration
  3. Manufacturing Method for Low-Cost Loop Heat Pipe Evaporator with Liquid-Vapor Weld Seal

    Amount: $124,891.00

    Vital to the LHP operation is the evaporator/reservoir assembly where waste heat from a heat-dissipating source is absorbed through the metal casing to vaporize the liquid on the outer surface of the ...

    SBIRPhase I2020National Aeronautics and Space Administration
  4. Miniature Loop Heat Pipe with Multiple Evaporators and Multiple Condensers

    Amount: $599,605.00

    Loop Heat Pipe (LHP) is a high performance heat transport device using capillary forces to circulate the working fluid in a closed loop. Conventional LHPs usually have one capillary pump (evaporator) ...

    SBIRPhase II2007National Aeronautics and Space Administration
  5. Passive Capillary Pumped Cryocooling System for Zero-Boil-Off Cryogen Storage Tanks

    Amount: $69,997.00

    Significant cost and weight savings of a space mission can be achieved by improving the cryogenic storage technology. Added cryogen mass due to the cryogen boil-off, the oversized tanks and storage s ...

    SBIRPhase I2006National Aeronautics and Space Administration
  6. Miniature Loop Heat Pipe with Multiple Evaporators and Multiple Condensers

    Amount: $69,999.00

    Cooling electronic components in the space environment still remains a challenge for thermal engineers. In the current design practice, copper straps are used to transfer the waste heat from various h ...

    SBIRPhase I2006National Aeronautics and Space Administration
  7. Helium Loop Heat Pipe for Large Area Cryocooling

    Amount: $300,000.00

    Next generation Far Infrared (FIR) Space Telescopes such as NASA?s SAFIR, SPIRIT, and SPECS require the entire mirrors, which can be as large as 10 meters in diameter, to be cooled to the temperature ...

    SBIRPhase II2004National Aeronautics and Space Administration
  8. Vapor Compression Refrigeration Loop with Spray Cooling for High Heat Flux Thermal Control

    Amount: $69,980.00

    Laser diodes are the key component in many space-based applications ranging from communication systems to optical sensors/detectors. Laser diode emitters however dissipate large amounts of waste heat ...

    SBIRPhase I2004National Aeronautics and Space Administration
  9. Helium Loop Heat Pipe for Large Area Cryocooling

    Amount: $69,995.00

    To take full advantage of the space environment, Far Infrared (FIR)/Submillimeter (SMM) interferometers require cold mirrors (4 K) and detectors (0.1 K or colder). The collecting mirrors for the propo ...

    SBIRPhase I2003National Aeronautics and Space Administration
  10. Cryogenic Advanced Loop Heat Pipe in Temperature Range of 20-30K

    Amount: $0.00

    The Next Generation Space Telescope (NGST) program has identified the need for cryogenic cooling transport devices that can provide cryogenic cooling in the temperature range of 20-30K, minimize vibra ...

    SBIRPhase I2002National Aeronautics and Space Administration
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