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Synonyms were used for: Astronautics • Exposition • Forum • SPACE
Search without synonyms: title: AIAA SPACE and Astronautics Forum and Exposition

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    Probabilistic analysis of docking mechanism-induced loads for mir/shuttle mission

    Lin, H.Z. / Ghofranian, S. / Schmidt, M. et al. | Tema Archive | 1995
    This paper presents a methodology for probabilistic loads analysis and its application to the STS-71 orbiter/Mir space station docking. It ...
    Publisher: American Institute of Aeronautics and Astronautics (AIAA) , Washington

    Determination of helicopter rotor damping from simulated data using frequency domain system identification

    Jones, C.T. / Celi, R. | Tema Archive | 1995
    This paper addresses the problem of determining helicopter rotor mode damping from a state-space model of rotor, fuselage, and inflow in ...
    Publisher: American Institute of Aeronautics and Astronautics (AIAA) , Washington

    Soft-ride to orbit: viscoelastic treatments for launch load attenuation

    Thampi, S.K. / Le, D.N. / Wilke, P.S. | Tema Archive | 1995
    The high level vibroacoustic environment, typical for launch vehicles, can result in excessive loads and fatigue problems for space ...
    Publisher: American Institute of Aeronautics and Astronautics (AIAA) , Washington

    Simulation of Shuttle/Mir docking

    Ghofranian, S. / Schmidt, M.S. / Schliesing, J. et al. | Tema Archive | 1995
    This paper describes the simulation of the docking system of the Space Shuttle orbiter and the Russian space station Mir. The system is a ...
    Publisher: American Institute of Aeronautics and Astronautics (AIAA) , Washington

    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 allowable working temperature for the aeroshell components, and enable the system to operate at higher temperatures while sustaining ...
    Keywords: Anwendung in der Luft- und Raumfahrt , NASA (National Aeronautics and Space Administration)

    Multi-criterion preliminary design of a tetrahedral truss platform

    Wu, K.C. | Tema Archive | 1995
    trusses. Performance improvements are plotted in frequency-mass (criterion) space and compared to results for uniform trusses. Application of ...
    Publisher: American Institute of Aeronautics and Astronautics (AIAA) , Washington

    A new substructures system identification method

    Craig, R.R. jun. | Tema Archive | 1995
    A new method is proposed for system identification of substructures, such as payloads to be flown aboard the Space Shuttle. In the ...
    Publisher: American Institute of Aeronautics and Astronautics (AIAA) , Washington

    On the isolation of science payloads from spacecraft vibrations

    Belvin, W.K. / Sparks, D.W. / Horta, L.G. et al. | Tema Archive | 1995
    The remote sensing of the Earth's features from space requires precision pointing of scientific instruments. To this end, the NASA Langley ...
    Publisher: American Institute of Aeronautics and Astronautics (AIAA) , Washington

    Passive vibration suppression using thin tape with viscous lamina

    Minesugi, K. / Onoda, J. / Hanawa, Y. | Tema Archive | 1995
    weight increase and space. In this paper, a polymid tape with viscous lamina is noted on the application to the passive vibration suppression ...
    Publisher: American Institute of Aeronautics and Astronautics (AIAA) , Washington

    The short wavelength deflections of the shuttle orbiter skin panels when subjected to in-plane compressive forces

    Benson, P.L. | Tema Archive | 1995
    The Space Shuttle Orbiter's forward fuselage outer shell is an aluminum skin and hat section stringer design. The skin panels support a ...
    Publisher: American Institute of Aeronautics and Astronautics (AIAA) , Washington

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