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The Electric Propulsion Interactions Code (EPIC)Science Applications International Corporation is currently developing the Electric Propulsion Interactions Code, EPIC, as part of a project sponsored by the Space Environments and Effects Program at the NASA Marshall Space Flight Center. Now in its second year of development, EPIC is an interactive computer tool that allows the construction of a 3-D spacecraft model, and the assessment of a variety of interactions between its subsystems and the plume from an electric thruster. These interactions may include erosion of surfaces due to sputtering and re-deposition of sputtered materials, surface heating, torque on the spacecraft, and changes in surface properties due to erosion and deposition. This paper describes the overall capability of EPIC and provides an outline of the physics and algorithms that comprise many of its computational modules.
Document ID
20040111037
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
Mikellides, I. G.
(Science Applications International Corp. San Diego, CA, United States)
Mandell, M. J.
(Science Applications International Corp. San Diego, CA, United States)
Kuharski, R. A.
(Science Applications International Corp. San Diego, CA, United States)
Davis, V. A.
(Science Applications International Corp. San Diego, CA, United States)
Gardner, B. M.
(Science Applications International Corp. San Diego, CA, United States)
Minor, J.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
September 7, 2013
Publication Date
March 1, 2004
Publication Information
Publication: 8th Spacecraft Charging Technology Conference
Subject Category
Computer Programming And Software
Funding Number(s)
CONTRACT_GRANT: NAS8-02028
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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