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Advanced Space Shuttle simulation modelThe effects of atmospheric turbulence in horizontal and near-horizontal flight during the return of the Space Shuttle are important for determining design, control, and pilot-in-the-loop effects. A nonrecursive model (based on vonKarman spectra) for atmospheric turbulence along the flight path of the Shuttle Orbiter has been developed which provides for simulation of instantaneous vertical and horizontal gusts at the vehicle center-of-gravity and also for simulation of instantaneous gust gradients. Based on this model the time series for gusts and gust gradients have been generated and stored on a series of magnetic tapes which are entitled Shuttle Simulation Turbulence Tapes (SSTT). The time series are designed to represent atmospheric turbulence from ground level to an altitude of 120,000 meters. A description of the turbulence generation procedure is provided, the results of validating the simulated turbulence are described, and conclusions and recommendations are presented. Appendices provide tabulated one-dimensional vonKarman spectra, a discussion of the minimum frequency simulated, and the results of spectral and statistical analyses of the SSTT.
Document ID
19820014426
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Tatom, F. B.
(Engineering Analysis, Inc. Huntsville, AL, United States)
Smith, S. R.
(Engineering Analysis, Inc. Huntsville, AL, United States)
Date Acquired
September 4, 2013
Publication Date
April 1, 1982
Publication Information
Publisher: NASA
Subject Category
Space Transportation
Report/Patent Number
NASA-CR-3541
M-377
NAS 1.26:3541
Report Number: NASA-CR-3541
Report Number: M-377
Report Number: NAS 1.26:3541
Accession Number
82N22300
Funding Number(s)
CONTRACT_GRANT: NAS8-33818
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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