Research Article
Performance Optimization and Verification of a New Type of Solar Panel for Microsatellites
Table 13
The analysis results of the relative deviation
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| Performance | Honeycomb aluminum plate | New type of solar panel | |
| (temperature difference) | 7.76 | 0.65 | 91.62% | (compression stress) | 63.72 | 33.81 | 46.94% | (shear strength) | 260.4 | 213.76 | 17.91% | (weight) | 50 | 44.86 | 10.28% |
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