Research Article
Efficiency of Hysteresis Rods in Small Spacecraft Attitude Stabilization
Table 3
In-flight data of existing selected satellites.
| Satellite |
Material |
Shape | | | | | | | |
On-board arrangement | | | | days | km | |
| TRANSIT-1B | AEM-4750 | CCSR | 32 | 0.78 | 8 | 16.86 | 6 | 804 | N.A. | N.A. | TRANSIT-2A | AEM-4750 | CCSR | 8 | 0.78 | 8 | 50.88 | 19 | 804 | N.A. | N.A. | DELFI-3C | Permenorm | CCSR | 11 | 0.07 | 2 | 0.0027 | 86 | 635 | 0.3 | In a plane perpendicular to the permanent magnet axis and passing through its center | TNS-0 | Mo-Permalloy | TFR | | 0.12 | 8 | 0.076 | 21 | 350 | 2.2 | In a plane perpendicular to the permanent magnet |
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