Strategic implementation of variable-thickness insulation layers for stratospheric airships

Excessive heat transfer from photovoltaic systems to airship hulls poses a threat to flight safety. To address this issue, a theoretical model was developed that combines thermal, heat transfer, and optimization models for airships with variable-thickness insulation layers. The study investigates the daily thermal behavior of stratospheric airships, focusing on the effects of thermal conductivity and insulation thickness. To balance weight reduction with insulation effectiveness, temperature constraints were used, and insulation thickness was optimized across different sections of the airship using a simulated annealing algorithm (SAA). Results indicate that adjusting thermal conductivity and insulation thickness can mitigate overheating and overpressure, albeit with a reduced solar energy output. Notably, variable-thickness insulation achieved a 9.7 % weight reduction at 40°N latitude, enhancing both photovoltaic system design and insulation material selection for stratospheric airships.