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Foldable photo voltaic sails might assist with aerobraking and atmospheric reentry

October 15, 2025
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Foldable photo voltaic sails might assist with aerobraking and atmospheric reentry
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Foldable solar sails could help with aerobraking and atmospheric reentry
Artist’s idea of NASA’s Superior Composite Photo voltaic Sail System (ACS3) in orbit. Credit score: NASA

Use circumstances for sensible supplies in area exploration hold cropping up all over the place. They’re utilized in the whole lot from antenna deployments on satellites to rover deformation and reformation.

One of many newest concepts is to make use of them to remodel the photo voltaic sails that might primarily be used as a propulsion system for a mission right into a warmth defend when that mission reaches its remaining vacation spot. A brand new paper by Joseph Ivarson and Davide Guzzetti, each of Auburn College’s Division of Aerospace Engineering, published in Acta Astronautica, describes how the thought may work and lists some potential purposes for exploring varied elements of the photo voltaic system.

The idea, which they name the Form Shifting Sailer (3S), is easy—have a skinny sheet of fabric that acts as a photo voltaic sail for many of a craft’s journey to its vacation spot. As soon as it reaches that vacation spot, change the sheet’s orientation in order that it will possibly act as a warmth defend and drag machine for the probe getting into the goal world’s environment or aerobraking into its orbit.

That change might be so simple as a set of form reminiscence alloy (SMA) hinges that fold the normally flat photo voltaic sail into extra of a cone or defend form to help with drag, which might sluggish the probe down, and likewise to help with deflecting a number of the warmth itself, basically performing as a—admittedly solely partially efficient—warmth defend.

Earlier than they tried to construct such a system, although, the engineers did what all good engineers would—they modeled the system first. On this case, they separated their modeling work into two completely different phases—a “design area” research and a feasibility research.

In engineering language, a “design area” does not have something to do with outer area—it is a time period for attempting to seize all of the various factors that might have an effect on a given metric, corresponding to the load or peak temperature a probe getting into Mars’s environment would expertise. By various these elements in simulation, engineers can develop a way of crucial design selections they must make, particularly concerning tradeoffs like reducing a sail’s weight or growing its thermal shielding impact.

Of their paper, the authors checked out case research for 5 potential goal worlds—Earth, Mars, Titan, Uranus, and Neptune. They then turned to a semi-autonomous algorithm referred to as a genetic algorithm that optimized the tradeoff of the sail’s peak temperature and its peak strain. They discovered these two metrics to be opposed, because the bodily shapes that reduce a type of two traits have a tendency to maximise the opposite.

To reduce the strain, it is best to be formed like a leaf—massive floor space, however very mild weight, whereas to attenuate temperature, it is best to be formed like a cannonball—very small, thick, and dense, which usually implies excessive thermal inertia—that means how a lot total warmth a cloth can take.

Within the subsequent section of their research, they opened up potential flight paths into the environment and orbit across the varied worlds within the research. Round Earth, they discovered the fabric might not less than considerably assist with the general thermal load, lowering the height heating price by 20–25%, however provided that the sail had been jettisoned throughout reentry. Mars was one of the best case situation for utilizing the 3S concept, because it confirmed—once more, throughout a jettison situation—that heating on the getting into probe might be lowered by as a lot as 40%.

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Sadly, the outcomes weren’t as nice for Titan, Uranus, and Neptune. On the fuel giants, utilizing the system in any respect proved infeasible, because the entry speeds required for aerobraking of their atmospheres had been too excessive and would fritter away any possible materials that might be doubtlessly manufactured within the close to future. On Titan, the 3S system could be possible, however would require about as a lot mass within the sail as there could be within the payload with a view to be efficient. On condition that getting mass to Titan is pricey in itself, it appears unlikely that the thought will take off—or land, for that matter.

However even when the thought is simply relevant to Mars exploration, that would be the focus of lots of future missions as NASA continues its path from the moon to Mars. Given the promising outcomes of the simulations proven within the paper, it may be price spending some cash creating a prototype of the 3S system to see if there are any kinks within the plan. However, given the present state of area exploration funding, which may have to attend for a while but.

Extra info:
Joseph Ivarson et al, Form shifting sailer: Entry and descent capabilities of self-foldable form reminiscence membranes, Acta Astronautica (2026). DOI: 10.1016/j.actaastro.2025.09.054

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