SIERRA ENGINEERING, INC.

Company Information
Address 603 East Robinson Street
Suite 7
Carson City, NV, -


Information

DUNS: 6620553

# of Employees: 4


Ownership Information

HUBZone Owned: N

Socially and Economically Disadvantaged: N

Woman Owned: N



Award Charts




Award Listing

  1. Prediction and Measurement of the Carbon Build-Up in Film-Cooled Rocket Engines

    Amount: $149,998.00

    ABSTRACT: Sierra Engineering Inc. (Sierra) believes that existing chemical kinetic models can be efficiently incorporated into commercial CFD codes to predict the mixing, pyrolysis, soot formation and ...

    STTRPhase I2015Department of Defense Air Force
  2. Improved Thrust Termination Modeling for Solid Rocket Motors

    Amount: $999,991.00

    This effort addresses the need for a predictive model which characterizes the motor ejecta from thrust terminated and burn-to-depletion solid rocket motors. Two models will be developed: an engineeri ...

    SBIRPhase II2013Department of Defense Missile Defense Agency
  3. Improved Thrust Termination Modeling for Solid Rocket Motors

    Amount: $99,917.00

    To improve the predictive capabilities of solid rocket motor end-of-burn phenomena, two analysis tools will be further developed. An existing engineering tool will go through continued development an ...

    SBIRPhase I2011Department of Defense Missile Defense Agency
  4. Improved Ballistics, Acoustics and Combustion Stability Modeling for Solid Rocket Motors

    Amount: $749,948.00

    A new, improved fidelity solid rocket ballistics model is being built on a commercial CFD platform. The CFD platform includes a coupled solid mechanics solver, allowing for tight coupling between the ...

    SBIRPhase II2011Navy Department of Defense
  5. Improved Ballistics, Acoustics and Combustion Stability Modeling for Solid Rocket Motors

    Amount: $149,828.00

    A new, improved fidelity solid rocket ballistics model will be built on a commercial CFD platform. The CFD platform includes a coupled solid mechanics solver, allowing for tight coupling between the g ...

    SBIRPhase I2010Navy Department of Defense
  6. Advanced Combustion Stability Analysis Tools for Ox-rich Preburners

    Amount: $99,998.00

    The goal of this SBIR is the enhancement of the current state-of-the-art combustion instability analysis tools.  The planned enhancement is focused on capturing the effects of injection element distr ...

    SBIRPhase I2009Air Force Department of Defense
  7. Resonance Igniter for Rocket Engine Ignition

    Amount: $99,971.00

    The goal of this SBIR is the design and demonstration of an opposed flow acoustic resonance igniter concept that can be applied to a range of rocket propellant combinations. Along with the hardware d ...

    SBIRPhase I2008Air Force Department of Defense
  8. Plume Diagnostics for Combustion Stability

    Amount: $599,998.00

    Sierra Engineering Inc. and Purdue University propose to develop a non-intrusive plume instrument capable of detecting and diagnosing combustion instability. This Stability Diagnostic System (SDS) wi ...

    STTRPhase II2007National Aeronautics and Space Administration
  9. Triaxial Swirler Liquid Injector Development

    Amount: $50,000.00

    Sierra Engineering Inc. (Sierra) believes that the subject triaxial liquid propellant swirl injector has the potential to meet many of NASA's Earth-to-Orbit (ETO) propulsion systems goals. The triaxia ...

    SBIRPhase II2006National Aeronautics and Space Administration
  10. Plume Diagnostics for Combustion Stability

    Amount: $99,995.00

    Sierra Engineering and Purdue University propose to leverage combustion stability testing, already funded and planned for the second and third quarters of next year at Purdue, by developing a non-intr ...

    STTRPhase I2006National Aeronautics and Space Administration

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