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Wind Study for High Altitude Platform DesignAn analysis of upper air winds was performed to define the wind environment at potential operating altitudes for high altitude powered platform concepts. Wind conditions of the continental United States, Pacific area (Alaska to Sea of Japan), and European area (Norwegian and Mediterranean Sea) were obtained using a representative network of sites selected based upon adequate high altitude sampling, geographic dispersion, and observed upper wind patterns. A data base of twenty plus years of rawinsonde gathered wind information was used in the analysis. Annual variations from surface to 10 mb pressure altitude were investigated to encompass the practical operating range for the platform concepts. Parametric analysis for the United States and foreign areas was performed to provide a basis for vehicle system design tradeoffs. This analysis of wind magnitudes indicates the feasibility of annual operation at a majority of sites and more selective seasonal operation for the extreme conditions between the pressure altitudes of 100 to 25 mb based upon the assumed design speeds.
Document ID
19800004408
Acquisition Source
Goddard Space Flight Center
Document Type
Other - NASA Reference Publication (RP)
Authors
Thomas W Strganac
(Wallops Flight Facility Wattsville, Virginia, United States)
Date Acquired
September 4, 2013
Publication Date
December 1, 1979
Publication Information
Publisher: National Aeronautics and Space Administration
Subject Category
Meteorology And Climatology
Report/Patent Number
NASA-RP-1044
Accession Number
80N12661
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
High altitude powered platform studies
High altitude winds
High altitude vehicle design
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