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Non-Invasive Tension Measurement Devices for Parachute CordageThe need for lightweight and non-intrusive tension measurements has arisen alongside the development of high-fidelity computer models of textile and fluid dynamics. In order to validate these computer models, data must be gathered in the operational environment without altering the design, construction, or performance of the test article. Current measurement device designs rely on severing a cord and breaking the load path to introduce a load cell. These load cells are very reliable, but introduce an area of high stiffness in the load path, directly affecting the structural response, adding excessive weight, and possibly altering the dynamics of the parachute during a test. To capture the required data for analysis validation without affecting the response of the system, non-invasive measurement devices have been developed and tested by NASA. These tension measurement devices offer minimal impact to the mass, form, fit, and function of the test article, while providing reliable, axial tension measurements for parachute cordage.
Document ID
20160012716
Acquisition Source
Johnson Space Center
Document Type
Conference Paper
Authors
Litteken, Douglas A.
(NASA Johnson Space Center Houston, TX, United States)
Daum, Jared S.
(NASA Johnson Space Center Houston, TX, United States)
Date Acquired
October 28, 2016
Publication Date
October 27, 2016
Subject Category
Space Transportation And Safety
Report/Patent Number
JSC-CN-37810
Meeting Information
Meeting: AIAA Aviation Forum 2017
Location: Denver, CO
Country: United States
Start Date: June 5, 2017
End Date: June 9, 2017
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
OTHER: IRD Funding
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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