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Performance Evaluation of Pressure Transducers for Water ImpactsThe Orion Multi-Purpose Crew Vehicle is being designed for water landings. In order to benchmark the ability of engineering tools to predict water landing loads, test programs are underway for scale model and full-scale water impacts. These test programs are predicated on the reliable measurement of impact pressure histories. Tests have been performed with a variety of pressure transducers from various manufacturers. Both piezoelectric and piezoresistive devices have been tested. Effects such as thermal shock, pinching of the transducer head, and flushness of the transducer mounting have been studied. Data acquisition issues such as sampling rate and anti-aliasing filtering also have been studied. The response of pressure transducers have been compared side-by-side on an impulse test rig and on a 20-inch diameter hemisphere dropped into a pool of water. The results have identified a range of viable configurations for pressure measurement dependent on the objectives of the test program.
Document ID
20120011929
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Vassilakos, Gregory J.
(Analytical Mechanics Associates, Inc. Hampton, VA, United States)
Stegall, David E.
(Analytical Mechanics Associates, Inc. Hampton, VA, United States)
Treadway, Sean
(Corvid Technologies, Inc. Mooresville, NC, United States)
Date Acquired
August 26, 2013
Publication Date
June 26, 2012
Subject Category
Structural Mechanics
Report/Patent Number
NF1676L-13497
Report Number: NF1676L-13497
Meeting Information
Meeting: 28th Aerodynamic Measurement Technology, Ground Testing, and Flight Testing Conference
Location: New Orleans, LA
Country: United States
Start Date: June 25, 2012
End Date: June 28, 2012
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
WBS: WBS 432938.11.01.07.43.22.01
Distribution Limits
Public
Copyright
Public Use Permitted.
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