The Standard Deviation of Launch Vehicle Environments
Author(s) -
Isam Yunis
Publication year - 2005
Publication title -
54th aiaa/asme/asce/ahs/asc structures, structural dynamics, and materials conference
Language(s) - English
Resource type - Conference proceedings
DOI - 10.2514/6.2005-1937
Subject(s) - launch vehicle , standard deviation , computer science , aerospace engineering , aeronautics , automotive engineering , engineering , statistics , mathematics
*Statistical analysis is used in the development of the launch vehicle environments of acoustics, vibrations, and shock. The standard deviation of these environments is critical to accurate statistical extrema. However, often very little data exists to define the standard deviation and it is better to use a typical standard deviation than one derived from a few measurements. This paper uses Space Shuttle and expendable launch vehicle flight data to define a typical standard deviation for acoustics and vibrations. The results suggest that 3dB is a conservative and reasonable standard deviation for the source environment and the payload environment.
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