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Bolt cutter functional evaluationThe Aerospace Corporation has been implementing finite difference and finite element codes for the analysis of a variety of explosive ordnance devices. Both MESA-2D and DYNA3D have been used to evaluate the role of several design parameters on the performance of a satellite separation system bolt cutter. Due to a lack of high strain rate response data for the materials involved, the properties for the bolt cutter and the bolt were selected to achieve agreement between computer simulation and observed characteristics of the recovered test hardware. The calculations provided insight into design parameters such as the cutter blade kinetic energy, the preload on the bolt, the relative position of the anvil, and the anvil shape. Modeling of the cutting process clarifies metallographic observation of both cut and uncut bolts obtained from several tests. Understanding the physical processes involved in bolt cutter operation may suggest certain design modifications that could improve performance margin without increasing environmental shock response levels.
Document ID
19960020702
Acquisition Source
Headquarters
Document Type
Conference Paper
Authors
S. Goldstein
(The Aerospace Corporation El Segundo, California, United States)
T. E. Wong
(The Aerospace Corporation El Segundo, California, United States)
S. W. Frost
(The Aerospace Corporation El Segundo, California, United States)
J. V. Gageby
(The Aerospace Corporation El Segundo, California, United States)
R. B. Pan
(The Aerospace Corporation El Segundo, California, United States)
Date Acquired
August 17, 2013
Publication Date
February 1, 1994
Publication Information
Publication: Second NASA Aerospace Pyrotechnic Systems Workshop
Publisher: National Aeronautics and Space Administration
Subject Category
Spacecraft Design, Testing And Performance
Meeting Information
Meeting: 2nd NASA Aerospace Pyrotechnics Systems Workshop
Location: Albuquerque, NM
Country: US
Start Date: February 8, 1994
End Date: February 9, 1994
Sponsors: National Aeronautics and Space Administration
Accession Number
96N24225
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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