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Advanced Space Shuttle simulation modelA non-recursive model (based on von Karman spectra) for atmospheric turbulence along the flight path of the shuttle orbiter was developed. It provides for simulation of instantaneous vertical and horizontal gusts at the vehicle center-of-gravity, and also for simulation of instantaneous gusts gradients. Based on this model the time series for both gusts and gust gradients were generated and stored on a series of magnetic tapes, 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. Conclusions and recommendations are presented. One-dimensional von Karman spectra are tabulated, while a discussion of the minimum frequency simulated is provided. The results of spectral and statistical analyses of the SSTT are presented.
Document ID
19820008270
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
January 11, 1982
Subject Category
Space Transportation
Report/Patent Number
EAI-TR-82-001
NASA-CR-161958
Report Number: EAI-TR-82-001
Report Number: NASA-CR-161958
Accession Number
82N16143
Funding Number(s)
CONTRACT_GRANT: NAS8-33818
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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