摘要
The article presents a structural analysis of a new space probe-solar sail.It was deployedsuccessfully on ground. The loads for an outer space mission was introduced and expressed withequation. As a special state, the largest load around earth was used to analyze the model by thefinite element method. Some results about strain and stress was obtained after setting some initialparameters. Compared to the results in the literature, the results presented here are significant.