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Quality Control Algorithms and Proposed Integration Process for Wind Profilers Used by Launch Vehicle SystemsImpact of winds to space launch vehicle include Design, Certification Day-of-launch (DOL) steering commands (1)Develop "knockdowns" of load indicators (2) Temporal uncertainty of flight winds. Currently use databases from weather balloons. Includes discrete profiles and profile pair datasets. Issues are : (1)Larger vehicles operate near design limits during ascent 150 discrete profiles per month 110-217 seasonal 2.0 and 3.5-hour pairs Balloon rise time (one hour) and drift (up to 100 n mi) Advantages of the Alternative approach using Doppler Radar Wind Profiler (DRWP) are: (1) Obtain larger sample size (2) Provide flexibility for assessing trajectory changes due to winds (3) Better representation of flight winds.
Document ID
20110015754
Acquisition Source
Marshall Space Flight Center
Document Type
Presentation
Authors
Decker, Ryan
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Barbre, Robert E., Jr.
(Jacobs Technologies Engineering Science Contract Group Huntsville, AL, United States)
Date Acquired
August 25, 2013
Publication Date
August 1, 2011
Subject Category
Space Transportation And Safety
Report/Patent Number
M11-0758
Report Number: M11-0758
Meeting Information
Meeting: 15th Conference on Aviation, Range, and Aerospace Meteorology
Location: Los Angeles,CA
Country: United States
Start Date: August 1, 2011
End Date: August 4, 2011
Distribution Limits
Public
Copyright
Public Use Permitted.
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