Company Information
Address 4020 LONG BEACH BLVD FL 2
LONG BEACH, CA, 90807-2617


DUNS: 133626544

# of Employees: 12

Ownership Information

HUBZone Owned: N

Socially and Economically Disadvantaged: N

Woman Owned: N

Award Charts

Award Listing

  1. Verification and Optimization of Advanced Finite Element Modeling Techniques for Complex Submarine Hull Structures

    Amount: $129,983.00

    The finite element method has been well-established for modern structural design and analysis. However, significant modeling choices must still be made in trying to achieve answers accurate enough for ...

    SBIRPhase I2017Department of Defense Navy
  2. Reduced Order Nonlinear Dynamic Aeroservoelasticity

    Amount: $124,955.00

    M4 Engineering proposes to develop methods and software to generate reduced order nonlinear models of dynamic aeroserovelastic systems. The reduced order models will be based on a hybrid NARMAX-Wavel ...

    SBIRPhase I2016National Aeronautics and Space Administration
  3. Innovative Aerodynamic Modeling for Aeroservoelastic Analysis and Design

    Amount: $749,955.00

    We propose the development of a novel aerodynamic modeling approach making use of fully unstructured grids for unsteady panel aerodynamic models for aeroelastic and aeroservoelastic analysis. The uns ...

    STTRPhase II2016National Aeronautics and Space Administration
  4. Bonded Joint Analysis Method

    Amount: $911,398.00

    During Phase I and Phase II, M4 Engineering, Inc. and Sandia National Laboratories have created a unique bonded joint analysis methodology and associated software. During Phase II.5, the developed tec ...

    STTRPhase II2016Department of Defense Navy
  5. Dynamic ASE Modeling and Optimization of Aircraft with SpaRibs

    Amount: $749,816.00

    In aircraft design, reducing structural weight is often a prime objective, while various constraints in multiple disciplines, such as structure, aerodynamics and aeroelasticity should be imposed on th ...

    STTRPhase II2015National Aeronautics and Space Administration
  6. Innovative Aerodynamic Modeling for Aeroservoelastic Analysis and Design

    Amount: $124,990.00

    We propose the development of a modern panel code for calculation of steady and unsteady aerodynamic loads needed for dynamic servoelastic (DSE) analysis of flight vehicles. The code will be especial ...

    STTRPhase I2015National Aeronautics and Space Administration
  7. Physics-Based Conceptual Design Tools

    Amount: $749,941.00

    Approaches for weight prediction, in the conceptual design phase, typically consist of parametric relations or empirical databases. Historical databases work reasonably well when applied to existing ...

    SBIRPhase II2015National Aeronautics and Space Administration
  8. Multi-Disciplinary Analysis and Optimization of Integrated Spacecraft System Models

    Amount: $121,549.00

    M4 Engineering and Missouri S&T propose to investigate the viability of creating a multidisciplinary analysis and optimization architecture for analyzing spacecraft system models. The current approac ...

    STTRPhase I2015National Aeronautics and Space Administration
  9. Uncertainty Propagation to Modal Parameters and Metrics

    Amount: $149,875.00

    ABSTRACT:This proposal effort seeks to demonstrate the feasibility of developing a methodology for propagating measurement errors through common modal parameter estimation algorithms and assurance cri ...

    SBIRPhase I2015Department of Defense Air Force
  10. Dynamic ASE Modeling and Optimization of Aircraft with SpaRibs

    Amount: $124,393.00

    We propose development and demonstration of a dynamic aeroservoelastic modeling and optimization system based on curvilinear internal structural arrangements of variable topology. This will allow com ...

    STTRPhase I2014National Aeronautics and Space Administration

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