Sierra Lobo, Inc.

Company Information
Address OH
Fremont, OH, 43420-7400

http://www.sierralobo.com

Information

DUNS: 928298983

# of Employees: 474


Ownership Information

Hubzone Owned: N

Socially and Economically Disadvantaged: Y

Woman Owned: N



Award Charts




Award Listing

  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 ...

    SBIRPhase I2013National 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 ...

    SBIRPhase I2013National 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 ...

    SBIRPhase I2012Department of Defense Navy
  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 ...

    STTRPhase II2011National 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 ...

    SBIRPhase I2011National 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 ...

    SBIRPhase II2011Department of Defense Army
  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, ...

    STTRPhase I2010National 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 ...

    SBIRPhase I2009Army Department 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 ...

    SBIRPhase I2008National 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 ...

    SBIRPhase I2005National Aeronautics and Space Administration

Agency Micro-sites

US Flag An Official Website of the United States Government