DocumentCode :
790406
Title :
Nascap-2k Spacecraft Charging Code Overview
Author :
Mandell, Myron J. ; Davis, Victoria A. ; Cooke, David L. ; Wheelock, Adrian T. ; Roth, C.J.
Author_Institution :
Sci. Applications Int. Corp., San Diego, CA
Volume :
34
Issue :
5
fYear :
2006
Firstpage :
2084
Lastpage :
2093
Abstract :
Nascap-2k is a modern spacecraft charging code, replacing the older codes NASA Charging Analyzer Program for GEosynchronous Orbit (NASCAP/GEO), NASA Charging Analyzer Program for Low-Earth Orbit (NASCAP/LEO), Potentials Of Large objects in the Auroral Region (POLAR), and Dynamic Plasma Analysis Code (DynaPAC). The code builds on the physical principles, mathematical algorithms, and user experience developed over three decades of spacecraft charging research. Capabilities include surface charging in geosynchronous and interplanetary orbits, sheath, and wake structure, and current collection in low-Earth orbits, and auroral charging. External potential structure and particle trajectories are computed using a finite element method on a nested grid structure and may be visualized within the Nascap-2k interface. Space charge can be treated either analytically, self-consistently with particle trajectories, or consistent with imported plume densities. Particle-in-cell (PIC) capabilities are available to study dynamic plasma effects. Auxiliary programs to Nascap-2k include Object Toolkit (for developing spacecraft surface models) and GridTool (for constructing nested grid structures around spacecraft models). The capabilities of the code are illustrated by way of four examples: charging of a geostationary satellite, self-consistent potentials for a negative probe in a low-Earth orbit spacecraft wake, potentials associated with thruster plumes, and PIC calculations of plasma effects on a very low frequency (about 1 to 20 kHz) antenna
Keywords :
spacecraft charging; GridTool; Nascap-2k spacecraft charging code; Object Toolkit; auroral charging; current collection; external potential structure; finite element method; geostationary satellite; geosynchronous orbits; interplanetary orbits; low-Earth orbit spacecraft wake; nested grid structure; particle trajectories; particle-in-cell calculations; plasma effects; plume densities; self-consistent potentials; spacecraft surface models; surface charging; thruster plumes; wake structure; Computer interfaces; Finite element methods; Grid computing; Low earth orbit satellites; NASA; Plasma sheaths; Space vehicles; Surface charging; Surface treatment; Visualization; Antenna theory; ion engines; particle tracking; plasma interactions; plasma measurement; space plasma; surface charging;
fLanguage :
English
Journal_Title :
Plasma Science, IEEE Transactions on
Publisher :
ieee
ISSN :
0093-3813
Type :
jour
DOI :
10.1109/TPS.2006.881934
Filename :
1710085
Link To Document :
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