LEO Satellite Solution

LEO Satellite Solution
LEO Satellite Solution

Project
Overview

  • Project Type

    Aerospace deployable solar array / custom space power solution

  • Application Scenario

    Low Earth orbit (LEO) satellites and space missions

  • Light Condition

    Unobstructed space solar irradiance (AM0)

  • Product Type

    Roll-up ultra-thin flexible perovskite solar sail membrane

  • Device Type

    LEO satellite deployable solar array — 400 m² roll-up sail

  • Power Support

    Primary on-orbit power generation for satellite systems

Technical Highlights

1. A massive 400 m² perovskite membrane rolls up like a scroll for launch and unfurls in orbit — impossible with rigid panels.

2. Ultra-light thin-film delivers exceptional specific power (W/g) and minimal stowed volume, critical for launch cost and payload limits.

3. Flexible sail withstands deployment stress, thermal cycling and the mechanical vibration of launch and orbit.

4. Large-area array scales power for high-draw missions: communications, sensing and electric propulsion systems.

5. Fully custom engineering: sail geometry, reel mechanism, layup structure and electrical specs tailored per mission.

Project
Highlights

1. Co-developed with Nayuta Space: a 400 m² roll-up flexible perovskite solar sail for low Earth orbit.

2. Solves the core trade-off of small satellites — high power without high weight or launch volume.

3. Deep custom capability spanning material, structure, deployment mechanism and electrical integration.

4. Enabling the next generation of large-scale, cost-effective space solar power.


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