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Summary
| Description |
English: The coefficient of drag Cd for a magnetic sail operating in the radial orientation quantifies the applicability of the MHD model, namely that characteristic length L must be greater than the ion gyroradius rg to effectively transfer solar wind momentum to the spacecraft. The ratio rg/L defines this test such that when less than one momentum is effectively transferred, but at values greater than one the transfer is greatly reduced according to a percentage lost Thrust Tloss. |
| Date | |
| Source | Own work |
| Author | Dmcdysan |
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File history
Click on a date/time to view the file as it appeared at that time.
| Date/Time | Thumbnail | Dimensions | User | Comment | |
|---|---|---|---|---|---|
| current | 19:53, 28 October 2023 | | 1,016 × 697 (95 KB) | Dmcdysan | Changed font to 14 pt |
| 04:54, 27 October 2023 |  | 2,560 × 1,824 (224 KB) | User-duck | Cropped 2 % horizontally, 3 % vertically to denter using CropTool with lossless mode. | |
| 20:42, 12 September 2022 |  | 2,625 × 1,875 (272 KB) | Dmcdysan | Changed label for right axis to T_loss, lost Thrust. | |
| 03:02, 15 July 2022 |  | 2,908 × 2,083 (306 KB) | Dmcdysan | Higher resolution version. | |
| 19:09, 8 July 2022 |  | 1,175 × 787 (109 KB) | Dmcdysan | Added %Decrease plot and secondary vertical axis. | |
| 05:51, 8 July 2022 |  | 1,116 × 862 (78 KB) | Dmcdysan | Uploaded own work with UploadWizard |
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