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Table 2.
Temperature levels and thermal fluxes.
| Characteristic | Value |
|---|---|
| HTMLI temperature | Ranging from about 500°C at |
| 0.28 AU to 70°C at 1.2 AU | |
| Support panel temperature | Ranging from about 148°C at |
| 0.28 AU to −76°C at 1.2 AU | |
| Solar flux absorbed by | 110 000 W |
| front shield | |
| Flux transmitted to HTMLI | 1985 W |
| rear side | |
| Flux radiated by main gap | 1848 W |
| to space | |
| Flux transmitted to support | 137 W |
| panel | |
| Flux transmitted from support | 6 W |
| panel to spacecraft |
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