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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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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

Keywords: Raumfahrt

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

Keywords: Raumfahrt

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

Keywords: Raumfahrt

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

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

Development and ground testing of a compactly stowed scalable inflatably deployed solar sail

Lichodziejewski, David / Derbes, Billy / Reinert, Rich et al. | Tema Archive | 2004

The development and ground testing of a scalable solar sail configuration to address NASA's future space propulsion needs were discussed ...

Keywords: Anwendung in der Luft- und Raumfahrt

Modeling of shock propagation and attenuation in viscoelastic materials

Rusovici, R. / Lesieutre, G.A. / Inman, D.J. | Tema Archive | 2000

address modeling of geometrically complex structures. These finite elements are then used to model shock propagation and absorption through ...

Publisher: American Institute of Aeronautics and Astronautics (AIAA) , Reston

Optimum design and testing of a post-buckled stiffened panel

Lillico, M. / Butler, R. / Hunt, G.W. et al. | Tema Archive | 2000

of an initial overall imperfection. The resulting panel has been analyzed using the non-linear FE package ABAQUS and four laboratory ...

Publisher: American Institute of Aeronautics and Astronautics (AIAA) , Reston