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Correlation of Canopy Distortion with Asymmetric Loading in Large Diameter Ringsail ParachutesThe second generation of the main parachutes for the Orion Capsule Parachute Assembly System (CPAS) were subjected to multiple flight tests. Three of the tests included were instrumented with the Tension Measuring System (TMS) to record main dispersion bridle loads. While these units were not able to resolve the individual suspension line loads, they were able to record a course representation of the asymmetric loading of the main parachutes during inflation. These tests were also equipped with upward looking cameras mounted on the test vehicles to collect detailed imagery of main deployment and inflation. When analyzed independently, both data sources exhibit similar features. These similarities provide evidence that the suspension line loads and the distortions in the canopy geometry are not independent. This paper will examine both data sources simultaneously to establish a correlation between asymmetric loading at the canopy skirt and the deformations of the canopy. This correlation will be used to build a model which can estimate individual suspension line loads from a measured riser load and detailed imagery.
Document ID
20220003984
Acquisition Source
Johnson Space Center
Document Type
Conference Paper
Authors
Samuel A. Janssen
(Jacobs Technology, Inc. Houston, TX)
Eric S. Ray
(Johnson Space Center Houston, Texas, United States)
Date Acquired
March 4, 2022
Subject Category
Spacecraft Design, Testing And Performance
Meeting Information
Meeting: 26th AIAA Aerodynamic Decelerator Systems Technology Conference and Seminar (ADSTCS)
Location: Toulouse
Country: FR
Start Date: May 16, 2022
End Date: May 19, 2022
Sponsors: American Institute of Aeronautics and Astronautics, DGA Techniques aéronautiques
Funding Number(s)
WBS: 484997.01.06.01.02
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
Parachutes
Aerodynamic Decelerators
Orion
Entry Descent and Landing
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