SIERRA ENGINEERING, INC.

Basic Information

603 East Robinson Street
Suite 7
Carson City, NV, -

Company Profile

n/a

Additional Details

Field Value
DUNS: 6620553
Hubzone Owned: N
Socially and Economically Disadvantaged: N
Woman Owned: N
Number of Employees: 4


  1. 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 ...

    SBIR Phase II 2013 Department of Defense Missile Defense Agency
  2. 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 ...

    SBIR Phase I 2011 Department of Defense Missile Defense Agency
  3. 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 ...

    SBIR Phase II 2011 Navy Department of Defense
  4. 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 ...

    SBIR Phase I 2010 Navy Department of Defense
  5. 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 ...

    SBIR Phase I 2009 Air Force Department of Defense
  6. 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 ...

    SBIR Phase I 2008 Air Force Department of Defense
  7. 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 ...

    STTR Phase II 2007 National Aeronautics and Space Administration
  8. 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 ...

    SBIR Phase II 2006 National Aeronautics and Space Administration
  9. 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 ...

    STTR Phase I 2006 National Aeronautics and Space Administration
  10. Triaxial Swirler Liquid Injector Development

    Amount: $69,960.00

    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 ...

    SBIR Phase I 2005 National Aeronautics and Space Administration

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