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Nextgen Aeronautics, Inc.

Company Information
Address
4030 SPENCER ST STE 108
TORRANCE, CA 90503-2463
United States


http://www.nextgenaero.com

Information

UEI: ZKMCL2QBEN46

# of Employees: 14


Ownership Information

HUBZone Owned: No

Socially and Economically Disadvantaged: Yes

Woman Owned: No



Award Charts




Award Listing

  1. Smart Materials and Adaptive and Novel Technologies Applied to Unmanned Underwater Riverine Craft (MANTA-UURC)

    Amount: $198,906.00

    Our basic concept consists of a bio-mimetic manta ray like autonomous underwater vehicle which incorporates SMA actuated mechanical structure surrounded by compliant skins to duplicate the efficient ...

    SBIRPhase I2007Department of Defense Defense Advanced Research Projects Agency
  2. Adjustable Fidelity Computational Aeroelasticity Procedure (AFCAP)

    Amount: $99,452.00

    NextGen proposes an approach to significantly enhance aeroelastic analysis capabilities over what is commonly available in linear analysis environments such as NASTANTM The approach to accomplish this ...

    SBIRPhase I2007National Aeronautics and Space Administration
  3. Advanced Modeling Concepts for Conceptual Design

    Amount: $99,919.00

    Preliminary design of aircraft structures is multidisciplinary, involving knowledge of structural mechanics, aerodynamics, aeroelasticity, structural dynamics and design concepts. Even though analysis ...

    SBIRPhase I2007National Aeronautics and Space Administration
  4. Cradle-to-Grave Monitoring of Composite Aircraft Structures

    Amount: $98,242.00

    NextGen is proposing a simple yet powerful damage identification technique for advanced composite structures. We propose to develop a damage index based on vibration signature comparison with origina ...

    SBIRPhase I2007National Aeronautics and Space Administration
  5. Fretting Fatigue Modeling and Life Prediction

    Amount: $400,037.00

    Fretting fatigue problems are found in nearly all mechanical components that have loaded contact surfaces subjected to high frequency, low amplitude vibratory loading such as aircraft engine blade-to- ...

    SBIRPhase II2007Department of Defense Navy
  6. Physics-Based Identification and Management of Aeroelastic Limit-Cycle Oscillations (LCO)

    Amount: $99,997.00

    A highly qualified team consisting of NextGen Aeronautics Inc., the University of Illinois, Texas A&M University and NES Tech, Inc., proposes an approach to the problem of aircraft limit cycle oscilla ...

    STTRPhase I2007Department of Defense Air Force
  7. Innovative Reconfigurable Wing Designs for Future Short Take-Off and Landing (STOL) Aircraft

    Amount: $98,939.00

    A promising application of a morphing wing whose geometry can be significantly changed is to reduce aircraft takeoff and landing speeds. Wing morphing can provide both an increase in wing area and cha ...

    STTRPhase I2007Department of Defense Defense Advanced Research Projects Agency
  8. A CAD-Based Software Tool for Design and Analysis of Materials under Ballistic Impact

    Amount: $99,797.00

    In battlefield environments, ballistic impact may result in the failure of military structures and materials, including armor. To improve the reliability and safety of military structures and materia ...

    STTRPhase I2007Department of Defense Army
  9. Advanced Structural Optimization Using Genetic Algorithm and Neural Network

    Amount: $723,284.00

    The goal of this work is to develop a software package that seamlessly integrates the processes of computer-aided design, computer-aided analysis, and structural optimization. A final implementation o ...

    SBIRPhase II2006Department of Defense Army
  10. High-Strength and High-Durability Radio Frequency (RF) Transparent Structures

    Amount: $749,178.00

    A team led by NextGen Aeronautics Inc., plans to develop RF transparent materials for conformal, load-bearing antenna structures (CLAS). While the technology being developed will be applicable to mul ...

    SBIRPhase II2006Department of Defense Air Force
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