Performance Optimization and Verification of a New Type of Solar Panel for Microsatellites

Table 12

The analysis results of the relative deviation and .

Performance	Target	Calculation results	Simulation results
(temperature difference)	0.55	0.65	0.51	27.45%	18.18%
(compression stress)	30	33.81	31.86	6.12%	12.7%
(shear strength)	200	213.76	210.9	1.37%	6.88%
(weight)	46	44.86	43.44	3.27%	2.48%