https://www.mdpi.com/2226-4310/12/9/785

*Authors: *Joel Town,Nishanth Pushparaj and Chantal Cappelletti

https://doi.org/10.3390/aerospace12090785

Published: *29 August 2025*

*Abstract*
As global temperatures continue to rise despite international mitigation
efforts, geoengineering has emerged as a potential avenue for climate
intervention. One of the most promising and ambitious concepts is the
Planetary sunshade—a large-scale structure located at Lagrange Point L1,
designed to reduce solar irradiance by physically blocking or redirecting
incoming photons. This paper presents a structural design solution for this
ambitious system, focusing on deployable mechanisms, frame architecture,
and sail configurations that enable rapid mass production and deployment of
solar sails components. The design process follows the European Cooperation
for Space Standardization (ECSS) methodology through its early-phase
stages, utilizing weighted decision matrices for concept selection and
material evaluation. Finite element analysis (FEA) was used to validate
structural integrity under Atlas V launch and operational conditions. The
final design features a 1297 m2 sail composed of four triangular segments,
deployed via booms and stowed using a vertical folding pattern around a
central spool. The booms incorporate arch-shaped cross-sections to enhance
stiffness. This configuration achieves a radius expansion ratio of 25 and a
sail efficiency factor of 0.5, ensuring survivability under Atlas V launch
loads.

*Source: MDPI*

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