1–7 of 7 hits
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    Structural system reliability under multiple failure modes

    Mahadevan, S. / Chamis, C.C. | Tema Archive | 1993
    This paper describes a computational method for system reliability estimation of propulsion structures. The failure domain of the entire ...

    Reliability analysis and quality assurance of rocket motor case considering proof testing

    Yang, J.N. / Chen, H.Y. / Chang, C.M. et al. | Tema Archive | 1993
    Proof testing has been used extensively in industry for quality assurance of some types of structural components, such as pressure vessels ...

    Derivation of 0-g structural control models from analysis and 1-g experimentation

    Glaese, R.M. / Miller, D.W. | Tema Archive | 1995
    process called updating. Once the model has been updated, it is verified through a combination of structural perturbation and closed-loop control ...
    Publisher: American Institute of Aeronautics and Astronautics (AIAA) , Washington

    An overview of the advanced lightweight aircraft fuselage structures (ALAFS) program

    Holzwarth, R.C. | Tema Archive | 1996
    The Advanced Lightweight Aircraft Structures (ALAFS) program is demonstrating cost and weight benefits obtainable for fighter fuselage ...
    Publisher: American Institute of Aeronautics and Astronautics (AIAA) , Reston

    Effects of alternative wing structural concepts on high speed civil transport life cycle costs

    Marx, W.J. / Mavris, D.N. / Schrage, D.P. | Tema Archive | 1996
    developed that is sensitive to material and product/process selections for the wing structure. The use of cost/time analyses is described and ...
    Publisher: American Institute of Aeronautics and Astronautics (AIAA) , Reston

    The role of structural health monitoring for future air vehicles

    Derriso, Mark M. / Olson, Steven E. | Tema Archive | 2006
    vehicle systems, which are likely to include advanced materials and advanced structural concepts. Composite materials are expected to be used ...

    Mechanical properties of T650-35/AFR-PE-4 at elevated temperatures for lightweight aeroshell designs

    Whitley, Karen S. / Collins, Timothy J. | Tema Archive | 2006
    the primary load-bearing structure (heat shield) of the spacecraft. New high-temperature resins and composite material manufacturing ...
    Keywords: NASA (National Aeronautics and Space Administration) , Strukturwerkstoff