Research Article
Membrane Material-Based Rigid Solar Array Design and Thermal Simulation for Stratospheric Airships
Table 1
Materials physical parameters of lightweight and high-efficiency solar cell module.
| Number | Material | Thickness (10−3 m) | Thermal conductivity (W/m·K) | Emissivity | Light transmittance |
| 1 | Surface packaging film | 0.12 | 0.22 | 0.92 | 92% | 2 | Transparency adhesive film | 0.3 | 0.32 | — | 91% | 3 | Si solar cell | 0.2 | 0.21 | — | — | 4 | Lightweight adhesive film | 0.1 | 0.6 | — | — | 5 | Electric insulation film | 0.05 | 0.12 | — | — | 6 | Monolayer carbon fiberboard | 0.125 | 0.78 | — | — | 7 | Nomex honeycomb core | 10 | 0.17 | 0.94 | — | 8 | Monolayer carbon fiberboard | 0.125 | 0.78 | 0.98 | — |
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