The high cost and long times required to develop research packages for space flight can often be offset by using ground test techniques. This paper describes a space shuttle launch and reentry simulating using the NASA Ames Research Center's 20G centrifuge facility. The combined G-forces and acoustic environment during shuttle launch and landing were simulated to evaluate the effect on a payload of laboratory rates. The launch G force and acoustic profiles are matched to actual shuttle launch data to produce the required G-forces and acoustic spectrum in the centrifuge test cab where the rats were caged on a free-swinging platform. For reentry, only G force is simulated as the aero-acoustic noise is insignificant compared to that during launch. The shuttle G-force profiles of launch and landing are achieved by programming the centrifuge drive computer to continuously adjust centrifuge rotational speed to obtain the correct launch and landing G forces. The shuttle launch acoustic environment is simulated using a high-power, low-frequency audio system. Accelerometer data from STS-56 and microphone data from STS-1 through STS-5 are used as baselines for the simulations. This paper provides a description of the test setup and the results of the simulation with recommendations for follow-on simulations.


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    Titel :

    Simulation of Shuttle launch G forces and acoustic loads using the NASA Ames Research Center 20G centrifuge


    Beteiligte:
    Shaw, T. L. (Autor:in) / Corliss, J. M. (Autor:in) / Gundo, D. P. (Autor:in) / Mulenburg, G. M. (Autor:in) / Breit, G. A. (Autor:in) / Griffith, J. B. (Autor:in)


    Erscheinungsdatum :

    1994-11-01


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Simulation of Shuttle Launch Forces and Acoustic Loads Using the NASA Ames Research Center 20G Centrifuge

    Shaw, T. L. / Corliss, J. M. / Gundo, D. P. et al. | British Library Conference Proceedings | 1994


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