Balloon Strain Relief System

A balloon strain relief system for use during pre-launch activities was developed and its effect on balloon tensile strength was examined. Various clamp materials and balloons and tensile test specimens from the balloons were laboratory tested. This restraint system was deemed feasible if a limited localized loss in film tensile strength could be tolerated.

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Copyright Author(s). This work is licensed under a Creative Commons Attribution-NonCommercial 4.0 International License.
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Metadata Contact Email opensky@ucar.edu
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Author National Center for Atmospheric Research
Raven Industries, Inc.
Scientific Balloon Facility (SBF)
Publisher UCAR/NCAR - Library
Publication Date 1969-01-01T00:00:00
Digital Object Identifier (DOI) Not Assigned
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Topic Category geoscientificInformation
Progress N/A
Metadata Date 2023-08-18T18:05:50.069343
Metadata Record Identifier edu.ucar.opensky::technotes:31
Metadata Language eng; USA
Suggested Citation National Center for Atmospheric Research, Raven Industries, Inc., Scientific Balloon Facility (SBF). (1969). Balloon Strain Relief System. UCAR/NCAR - Library. http://n2t.net/ark:/85065/d7m61jpr. Accessed 21 November 2024.

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