DocumentCode :
603783
Title :
Experimental observation and computational modeling of hypervelocity impacts with emphasis on plasma formation and its consequences
Author :
Crawford, D.A.
Author_Institution :
Sandia Nat. Labs., Albuquerque, NM, USA
fYear :
2013
fDate :
9-12 Jan. 2013
Firstpage :
1
Lastpage :
1
Abstract :
In experiments performed at the NASA Ames Vertical Gun Range (AVGR), optical and radiofrequency electromagnetic emissions, plasma formation and electrostatic charge separation during hypervelocity impact have been characterized for a variety of impactor and target geometries. While being investigated as potentially diagnostic of an event, such effects could also interfere with communications or remote sensing equipment if an impact occurred on a satellite. The highly conducting plasma could act as a current path across normally shielded circuits, potentially leading to satellite loss. In the AVRG experiments, early time solid debris ejected from the impact site are negatively charged and impact-generated plasma, late-time ejecta and materials left in the transient cavity are positively charged. Charge separation can lead to large electrostatic fields with implications for dust motion, especially in low gravity environments. The motion of charged ejecta can create transient magnetic fields. The experiments demonstrate that total charge separation is a function of impactor kinetic energy with a near linear mass dependence and velocity dependence proportional to v2.6. CTH is a Sandia developed, well validated, Eulerian, multi-material, computational hydrocode designed to treat a wide range of shock propagation and material motion phenomena in one, two, or three dimensions. Adaptive mesh refinement is available for maximizing resolution in regions of interest. CTH has models suitable for most conditions encountered in hypervelocity impact including material strength, fracture and multi-state materials, including plasma. It has been used extensively in hypervelocity impact studies at laboratory and large scale. Computational studies using CTH have shown that a simple two dimensional model based on electrostatic probe theory can match experimentally observed plasma and electrostatic charge separation. We are extending the CTH model to three dimensions to improve our abil- ty to predict plasma formation and charge separation under more general circumstances.
Keywords :
artificial satellites; dusty plasmas; electrostatic precipitators; fracture; impact (mechanical); magnetic shielding; plasma electromagnetic wave propagation; plasma shock waves; remote sensing; separation; space debris; weapons; AVGR; AVRG; Ames Vertical Gun Range; CTH; adaptive mesh refinement; dust motion; electrostatic charge separation; electrostatic field; electrostatic probe theory; fracture; gravity environment; hypervelocity impact; impact generated plasma; impactor kinetic energy; late time ejecta; linear mass dependence; material motion phenomena; material strength; multistate material; optical emission; plasma formation; plasma separation; radiofrequency electromagnetic emission; regions of interest; remote sensing equipment; satellite loss; shielded circuit; shock propagation; solid debris ejection; target geometry; transient cavity; transient magnetic field; two dimensional model; velocity dependence; Computational modeling; Electrostatics; Laboratories; Materials; Plasmas; Satellite broadcasting; Satellites;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Radio Science Meeting (USNC-URSI NRSM), 2013 US National Committee of URSI National
Conference_Location :
Boulder, CO
Print_ISBN :
978-1-4673-4776-1
Type :
conf
DOI :
10.1109/USNC-URSI-NRSM.2013.6525001
Filename :
6525001
Link To Document :
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