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A Compendium of Wind Statistics and Models for the NASA Space Shuttle and Other Aerospace Vehicle ProgramsThe wind profile with all of its variations with respect to altitude has been, is now, and will continue to be important for aerospace vehicle design and operations. Wind profile databases and models are used for the vehicle ascent flight design for structural wind loading, flight control systems, performance analysis, and launch operations. This report presents the evolution of wind statistics and wind models from the empirical scalar wind profile model established for the Saturn Program through the development of the vector wind profile model used for the Space Shuttle design to the variations of this wind modeling concept for the X-33 program. Because wind is a vector quantity, the vector wind models use the rigorous mathematical probability properties of the multivariate normal probability distribution. When the vehicle ascent steering commands (ascent guidance) are wind biased to the wind profile measured on the day-of-launch, ascent structural wind loads are reduced and launch probability is increased. This wind load alleviation technique is recommended in the initial phase of vehicle development. The vehicle must fly through the largest load allowable versus altitude to achieve its mission. The Gumbel extreme value probability distribution is used to obtain the probability of exceeding (or not exceeding) the load allowable. The time conditional probability function is derived from the Gumbel bivariate extreme value distribution. This time conditional function is used for calculation of wind loads persistence increments using 3.5-hour Jimsphere wind pairs. These increments are used to protect the commit-to-launch decision. Other topics presented include the Shuttle Shuttle load-response to smoothed wind profiles, a new gust model, and advancements in wind profile measuring systems. From the lessons learned and knowledge gained from past vehicle programs, the development of future launch vehicles can be accelerated. However, new vehicle programs by their very nature will require specialized support for new databases and analyses for wind, atmospheric parameters (pressure, temperature, and density versus altitude), and weather. It is for this reason that project managers are encouraged to collaborate with natural environment specialists early in the conceptual design phase. Such action will give the lead time necessary to meet the natural environment design and operational requirements, and thus, reduce development costs.
Document ID
19990008476
Acquisition Source
Marshall Space Flight Center
Document Type
Contractor Report (CR)
Authors
Smith, O. E.
(Computer Sciences Corp. Huntsville, AL United States)
Adelfang, S. I.
(Computer Sciences Corp. Huntsville, AL United States)
Date Acquired
September 6, 2013
Publication Date
October 1, 1998
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
M-899
NAS 1.26:208859
NASA/CR-1998-208859
Report Number: M-899
Report Number: NAS 1.26:208859
Report Number: NASA/CR-1998-208859
Funding Number(s)
CONTRACT_GRANT: NAS8-60000
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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