| タイトル | The Electric Propulsion Interactions Code (EPIC) |
| 本文（外部サイト） | http://hdl.handle.net/2060/20040111037 |
| 著者（英） | Gardner, B. M.; Mandell, M. J.; Mikellides, I. G.; Kuharski, R. A.; Davis, V. A.; Minor, J. |
| 著者所属（英） | NASA Marshall Space Flight Center |
| 発行日 | 2004-03-01 |
| 言語 | eng |
| 内容記述 | 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. |
| NASA分類 | Computer Programming and Software |
| 権利 | No Copyright |
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