Sierra Lobo, Inc.

Basic Information

OH
Fremont, OH, 43420-7400

http://www.sierralobo.com

Company Profile

n/a

Additional Details

Field Value
DUNS: 928298983
Hubzone Owned: N
Socially and Economically Disadvantaged: Y
Woman Owned: N
Number of Employees: 474


  1. Thermoacoustic Duplex Technology for Cooling and Powering a Venus Lander

    Amount: $125,000.00

    Sierra Lobo proposes to develop a technology that can provide both cooling and electric power generation using heat. When coupled with a radioisotope heat source, the technology is ideally suited to ...

    SBIR Phase I 2013 National Aeronautics and Space Administration
  2. Load-Bearing Tank-Applied Multi-Layer Insulation

    Amount: $124,960.00

    The proposed load-bearing, tank-applied, multi-layer insulation system consists of a set of highly reflective radiation shields made from 1 mil thick aluminized Mylar that is supported from a "po ...

    SBIR Phase I 2013 National Aeronautics and Space Administration
  3. A Compact, Passive, Cryogenic Cooling Unit for Shipboard Environments

    Amount: $79,888.00

    The Navy has stated a need for a backup cryogenic cooling method for shipboard superconducting systems. The cooling method must be as compact as practical and should operate without consumables even i ...

    SBIR Phase I 2012 Department of DefenseNavyDepartment of Defense
  4. Gaseous Helium Reclamation at Rocket Test Systems

    Amount: $674,938.00

    GHe reclamation is critical in reducing operating costs at rocket engine test facilities. Increases in cost and shortages of helium will dramatically impact testing of rocket engines for launch vehic ...

    STTR Phase II 2011 National Aeronautics and Space Administration
  5. A CubeSat-Scale Testbed for Cryogenic Fluid Management Technologies

    Amount: $94,480.00

    NASA has identified in-space cryogenic fluid management (CFM) as a high priority for technology development because the construction of an in-space propellant infrastructure is anticipated to dramatic ...

    SBIR Phase I 2011 National Aeronautics and Space Administration
  6. High-G Magnetic Capture System

    Amount: $729,962.00

    High-g testing through controlled deceleration has proven to be a key to the successful development of electronics that must survive gun launch. The need for this type of testing is expected to contin ...

    SBIR Phase II 2011 Department of DefenseArmyDepartment of Defense
  7. Gaseous Helium Reclamation at Rocket Test Systems

    Amount: $100,000.00

    The ability to restore large amounts of vented gaseous helium (GHe) at rocket test sites preserves the GHe and reduces operating cost. The used GHe is vented into the atmosphere, is non-recoverable, ...

    STTR Phase I 2010 National Aeronautics and Space Administration
  8. High-G Magnetic Capture System

    Amount: $119,989.00

    High-g testing through controlled deceleration has proven to be a key to the successful development of electronics that must survive gun launch. A magnetic method of deceleration has been widely impl ...

    SBIR Phase I 2009 ArmyDepartment of DefenseDepartment of Defense
  9. Advanced Insulation Techniques for Cryogenic Tanks

    Amount: $99,953.00

    The ability to store large amounts of cryogenic fluids for long durations has a profound effect on the success of many future space programs using these fluids for propellants, reactants, and life sup ...

    SBIR Phase I 2008 National Aeronautics and Space Administration
  10. Propellant Conditioning Using Improved Pulse Tube Cryocooler

    Amount: $69,452.00

    Application of the proposed technology (an affordable, large-scale, high-efficiency, low-temperature pulse tube cryocooler system), serves two NASA needs: an improved cryogenic propellant conditioning ...

    SBIR Phase I 2005 National Aeronautics and Space Administration

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