### Abstract

An accurate thrust model is extremely important for the navigation and space mission of solar sails. The thrust is deeply affected by the deformation of the highly flexible structure. Thus, in this paper, the exact thrust models for two-point and infinite-point-connected sails are presented by calculating the static deformations for the sail support beam structure with geometrical nonlinearity based on the assumption that the deformation of the sail film coincides with the support beam. And the film is merely regarded as the structure that transfers the solar radiation pressure force to the support beam. The nonlinear finite element model of the support beam with the Von-Karman’s nonlinear strain–displacement relationships is obtained. Then the Newton iteration method is used to calculate the large deformation of the sail structure. The thrust-modification methods are proposed for the two-connected sail. The deformation of the two-point-connected sail is larger than the infinite-point-connected sail, and the thrust loss of the two-point-connected sail is larger than the infinite-point-connected sail by nonlinear static calculations. Some suggestions are given based on the calculation results and relevant analysis. The thrust model should be verified and modified by in-flight data in the future.

Original language | English |
---|---|

Pages (from-to) | 149-162 |

Journal | Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering |

Volume | 229 |

Issue number | 1 |

Early online date | 17 Mar 2014 |

DOIs | |

Publication status | Published - 01 Jan 2015 |

## Fingerprint Dive into the research topics of 'Nonlinear static analysis-based thrust for solar sail'. Together they form a unique fingerprint.

## Cite this

Liu, J., Cui, N., Shen, F., & Rong, S. (2015). Nonlinear static analysis-based thrust for solar sail.

*Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering*,*229*(1), 149-162. https://doi.org/10.1177/0954410014527921