| タイトル | Validation of NASCAP-2K Spacecraft-Environment Interactions Calculations |
| 本文（外部サイト） | http://hdl.handle.net/2060/20040111077 |
| 著者（英） | Minor, J.; Gardner, B. M.; Cooke, D. L.; Mandell, M. J.; Mikellides, I. G.; Neergaard, L. F.; Davis, V. A. |
| 著者所属（英） | NASA Marshall Space Flight Center |
| 発行日 | 2004-03-01 |
| 言語 | eng |
| 内容記述 | The recently released Nascap-2k, version 2.0, three-dimensional computer code models interactions between spacecraft surfaces and low-earth-orbit, geosynchronous, auroral, and interplanetary plasma environments. It replaces the earlier three-dimensional spacecraft interactions codes NASCAP/GEO, NASCAP/LEO, POLAR, and DynaPAC. Nascap-2k has improved numeric techniques, a modern user interface, and a simple, interactive satellite surface definition module (Object ToolKit). We establish the accuracy of Nascap-2k both by comparing computed currents and potentials with analytic results and by comparing Nascap-2k results with published calculations using the earlier codes. Nascap-2k predicts Langmuir-Blodgett or Parker-Murphy current collection for a nearly spherical (100 surfaces) satellite in a short Debye length plasma depending on the absence or presence of a magnetic field. A low fidelity (in geometry and time) Nascap-2k geosynchronous charging calculation gives the same results as the corresponding low fidelity NASCAP/GEO calculation. A high fidelity calculation (using the Nascap-2k improved geometry and time stepping capabilities) gives higher potentials, which are more consistent with typical observations. Nascap-2k predicts the same current as a function of applied potential as was observed and calculated by NASCAP/LEO for the SPEAR I rocket with a bipolar sheath. A Nascap-2k DMSP charging calculation gives results similar to those obtained using POLAR and consistent with observation. |
| NASA分類 | Computer Programming and Software |
| 権利 | No Copyright |
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