Heliosaur — Origami Solar Sail

A folded photovoltaic solar sail that deploys from a 3U CubeSat into a 25 m² flower of thin-film cells. It both catches sunlight as power and as gentle thrust, letting tiny student spacecraft change orbit without fuel.

complexity: hardtolerance: ultra precision
Heliosaur — Origami Solar Sail

Snapshot

Feasibility at a glance

PT localization

6/10

Partial

Most steps can be localised in Portugal.

Per unit

€18,000–€28,000 per unit

at 8-unit volume

Starter batch

8units

minimum viable run

To first batch

20weeks

6 phases, design to ship

Budget

€144K–€314K

all-in estimate

Bottom line

Vacuum-deposit GaAs photovoltaic onto rolls of aluminised mylar.
Read full insight

Picked based on the localization score (6/10) plus the dominant process (cnc machining). For an early build at this batch size, this gives you the best balance of cost, risk, and speed of iteration.

What it does

4 capabilities

Stores compactly inside a CubeSat slot during launch.

Unfurls in vacuum into four overlapping petals using shape-memory hinges.

Catches photons as electricity AND as gentle thrust at the same time.

Folds back on command for a controlled de-orbit when the mission ends.

How it's made

4 stations · build route

  1. 1

    Coat the film

    Vacuum-deposit GaAs photovoltaic onto rolls of aluminised mylar.

  2. 2

    Crease the origami

    CNC-cut creases, folded by hand on a temperature-controlled jig.

  3. 3

    Wind the booms

    Filament-wound carbon composite — they roll up like a tape measure.

  4. 4

    Vacuum deploy

    Final qual is a full deployment in a thermal-vacuum chamber, twice.

Risks to watch

3 identified · 2 blocking

1 critical
1 high
1 medium

Critical

Deployment mechanism fails in vacuum

Vacuum deployments are unforgiving — one stuck hinge ends the mission.

Mitigation — Vacuum-cycle the hinge mechanism 50× before sign-off; redundant release path.

High

Material delamination after thermal cycling

Bonded composite + film stacks crack at ~50 cycles unless the bond is qualified.

Mitigation — Run 100 thermal-vacuum cycles on a witness panel before flight build.

Medium

Random-vibe load shears connectors

Launcher-induced vibe finds the weakest connector, every time.

Mitigation — Stake every connector and qualify on a vibe table to 12g RMS.

Production timeline

20 weeks to first batch

wk 1wk 7

CNC machining

wk 1–2

Composite lay-up

wk 3

Laser cutting

wk 4

Filament winding

wk 5

Final assembly

wk 6

Functional QA & batch sign-off

wk 7

wk 1–2 is the longest stretch — CNC machining takes 2 weeks of the 7 weeks on this build.

What goes into it

5 materials · 6 processes

Materials

2.5 µm aluminised mylar (sail film)Thin-film GaAs photovoltaic depositionCarbon-fibre composite boomsDyneema retraction linesShape-memory alloy hinges

Processes

cnc_machiningcomposite_layuplaser_cuttingfilament_windingfinal_assemblytesting_inspection

Design philosophy and best practices

5 principles

An origami solar sail must fold into a small volume and open reliably in space. The thin film, booms and hinges must work after launch and stay flat in sunlight.

1

Fold to avoid tearing

Fold patterns must avoid sharp creases that crack the film coating.

2

Make deployment repeatable

Booms and hinges need ground tests in vacuum and cold to prove they open every time.

3

Manage film tension

The sail must stay flat without tearing; tension paths and rip-stop help.

4

Plan for thermal and UV effects

Sunlight heats and ages the film. Choose coatings and materials tested for space.

5

Follow space test standards

Vibration, thermal vacuum and outgassing tests (for example ECSS standards) apply to every part.

Common pitfalls

Avoid

Shape-memory hinges that behave differently in vacuum and cold.

Avoid

Booms that buckle under uneven load.

Avoid

Static charge and dust during folding.

Avoid

Underestimating how long ground testing takes.

10-year evolution forecast (2026-2036)

4 phases

Solar sails have flown on several demonstration missions. The points below are trends.

2026–2028

Small demonstrations

Trend: CubeSat-sized sails test deployment.

2028–2031

Better booms

Trend: lighter composite booms that roll up.

2031–2034

Larger sails

Trend: bigger sails for science and deorbit.

2034–2036

Deorbit uses

Trend: drag sails help remove old satellites.

Outlook

Expect solar sails to stay specialist products for demos, science and deorbit.

Materials intelligence

5 materials

Aluminised polyester film

Medium supply risk

Sail film

Sourced from: Made by a few film producers in the US, Japan and Europe.

Thin-film GaAs cells

High supply risk

Power

Sourced from: Made by a few specialist makers in Europe, the US and China.

Carbon fibre

Medium supply risk

Booms

Sourced from: Carbon fibre is made mainly in Japan, the US and China.

Dyneema fibre

Medium supply risk

Retraction lines

Sourced from: Made mainly in the Netherlands and the US.

Nickel-titanium alloy

Medium supply risk

Shape-memory hinges

Sourced from: Made by a few specialist producers in the US, Europe and Asia.

Prototyping and rapid manufacturing in Portugal

4 companies from the atlas

Space PCB fabrication and soldering

Control electronics for deployment.

ROQ Laser

Vila Nova de Famalicão

Laser cutting

Thin metal fittings and templates.

DIB4T

Marinha Grande

Laser cutting and assembly

Fold test rigs and templates.

MAFEPRE

Marinha Grande

CNC machining

Boom end fittings and hinge blocks.

567 Portuguese manufacturers matched

None cover the whole build — it splits across steps.