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Biaxial Stress Limit for ULDB FilmThe current ULDB design applies stress to the shell film biaxially to control creep in the latitudinal direction. The recent change in design paradigm, from a uniaxial to biaxial stress state basis, arose from a new perspective that the biaxial loading can control strain in both principal surface dimensions as discussed below. The current ULDB project path was thus enabled by a more thorough understanding of the nonlinear viscoelastic properties of the shell film material, linear low-density polyethylene (LLDPE). Although a very similar material is also used in NASA zero-pressure (ZPB) and long-duration balloons (LDB), the different stress state requires a new approach to shell material qualification.
Document ID
20050179468
Acquisition Source
Goddard Space Flight Center
Document Type
Preprint (Draft being sent to journal)
Authors
Sterling, W. J.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Rand, J. L.
(Winzen Engineering, Inc. San Antonio, TX, United States)
Date Acquired
August 29, 2013
Publication Date
January 1, 2005
Subject Category
Structural Mechanics
Meeting Information
Meeting: American Institute of Aeronautics and Astronautics ATIO Conference
Location: Arlington, VA
Country: United States
Start Date: September 26, 2005
End Date: September 28, 2005
Sponsors: American Inst. of Aeronautics and Astronautics
Distribution Limits
Public
Copyright
Public Use Permitted.
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