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Reconstruction of Twist Torque in Main Parachute RisersThe reconstruction of twist torque in the Main Parachute Risers of the Capsule Parachute Assembly System (CPAS) has been successfully used to validate CPAS Model Memo conservative twist torque equations. Reconstruction of basic, one degree of freedom drop tests was used to create a functional process for the evaluation of more complex, rigid body simulation. The roll, pitch, and yaw of the body, the fly-out angles of the parachutes, and the relative location of the parachutes to the body are inputs to the torque simulation. The data collected by the Inertial Measurement Unit (IMU) was used to calculate the true torque. The simulation then used photogrammetric and IMU data as inputs into the Model Memo equations. The results were then compared to the true torque results to validate the Model Memo equations. The Model Memo parameters were based off of steel risers and the parameters will need to be re-evaluated for different materials. Photogrammetric data was found to be more accurate than the inertial data in accounting for the relative rotation between payload and cluster. The Model Memo equations were generally a good match and when not matching were generally conservative.
Document ID
20150003468
Acquisition Source
Johnson Space Center
Document Type
Conference Paper
Authors
Day, Joshua D.
(Embry-Riddle Aeronautical Univ. Prescott, AZ, United States)
Date Acquired
March 23, 2015
Publication Date
March 30, 2015
Subject Category
Astronautics (General)
Report/Patent Number
JSC-CN-32553
Report Number: JSC-CN-32553
Meeting Information
Meeting: AIAA Aerodynamic Decelerator Systems Technology Conference and Seminar
Location: Daytona Beach, FL
Country: United States
Start Date: March 30, 2015
End Date: April 2, 2015
Sponsors: American Inst. of Aeronautics and Astronautics
Distribution Limits
Public
Copyright
Public Use Permitted.
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