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A stress index model for ascending balloonsAttention is given to the development on the part of NASA of a simplified stress 'index' model to establish the relative stress magnitudes along a balloon's gore position as a function of altitude. Application of this model to several hundred balloon flights showed a good correlation between balloon failure rate and stress 'index' level. This model can be used during the balloon design process to lower the levels of stress in the balloon. By increasing the wall thickness of the balloon, adding caps, lengthening caps, or using external caps, lower stress can be accomplished. As a result, in January 1985, the NASA Balloon Program established a stress index specification to limit the design and flight stresses for NASA balloons.
Document ID
19870028477
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Smith, I. S.
(NASA Wallops Flight Center Wallops Island, VA, United States)
Date Acquired
August 13, 2013
Publication Date
October 1, 1986
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
AIAA PAPER 86-2566
Accession Number
87A15751
Distribution Limits
Public
Copyright
Other

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