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    Space program supporting technologies: structures, materials, and signal processing

    Schutzenhofer, L.A. / Blalock, S.J. / Johnston, L. et al. | Tema Archive | 1995
    task provides a benefit that addresses a problem area or meets a need in a space program. These benefits and past application of existing ...
    Publisher: American Institute of Aeronautics and Astronautics (AIAA) , Washington

    Modal vibration test facilities and methods for space station modules

    Tinker, M.L. | Tema Archive | 1995
    Development of a large modal survey test fixture for measuring constrained-boundary modes and frequencies of space station modules and ...
    Publisher: American Institute of Aeronautics and Astronautics (AIAA) , Washington

    Space Shuttle Orbiter landing loads optimization

    Purtle, L.V. / Fann, C.P. / Eich, P.G. | Tema Archive | 1995
    The paper discusses the method used in the Space Shuttle program to optimize landing gear loads and requirements to support increased ...
    Publisher: American Institute of Aeronautics and Astronautics (AIAA) , Washington

    High thermal conductivity graphite in space applications

    Peck, S.O. | Tema Archive | 1995
    Applications of high thermal conductivity graphite fibers to space structures are discussed in the context of a composite scan mirror and ...
    Publisher: American Institute of Aeronautics and Astronautics (AIAA) , Washington

    Dynamic loads analysis of photovoltaic arrays for the space station

    Kim, H.M. / Van Horn, D.A. / West, T.S. | Tema Archive | 1995
    This paper summarizes a study conducted to evaluate the fidelity of structural dynamic models for the Space Station photovoltaic arrays and ...
    Publisher: American Institute of Aeronautics and Astronautics (AIAA) , Washington

    Configuration-shape-size optimization of space structures using the webbing approach

    Vandenbelt, D.N. / Felippa, C.A. | Tema Archive | 1995
    This project investigates the configuration-shape-size optimization (CSSO) of orbiting and planetary space structures. The CSSO problem has ...
    Publisher: American Institute of Aeronautics and Astronautics (AIAA) , Washington

    Space shuttle reusable solid rocket motor actuator bracket bolted joint certification analysis

    Nielsen, D.B. / Stratton, T.C. | Tema Archive | 1995
    Webster and Nielsen. As the RSRM design is very performance oriented, structural design required the use of lightweight materials whenever ...
    Publisher: American Institute of Aeronautics and Astronautics (AIAA) , Washington

    Dynamic control of docking of adaptive space structure based on artificial potential method

    Matsuzaki, Y. / Miura, T. / Ichiyanagi, A. et al. | Tema Archive | 1995
    For the soft docking of a space vehicle with a target, it is important for the vehicle to accurately adjust the approaching velocity and ...
    Publisher: American Institute of Aeronautics and Astronautics (AIAA) , Washington

    Effects of a non-linear system (free play) on space shuttle body flap modal responses

    Park, C.C. / Misel, J.E. | Tema Archive | 1995
    A non-linear transient response analysis was performed to understand the modal responses of the body flap of the Space Shuttle Orbiter. The ...
    Publisher: American Institute of Aeronautics and Astronautics (AIAA) , Washington

    Aeroelastic stability analysis of an airfoil with structural nonlinearities using a state space unsteady aerodynamics model

    Murty, H.S. | Tema Archive | 1995
    airfoil. This analysis was carried out using a state space formulation for the aerodynamic model. This formulation enables hard coupling between ...
    Publisher: American Institute of Aeronautics and Astronautics (AIAA) , Washington

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