COMPACT AND PROPELLANT-LESS ELECTRODYNAMIC TETHER SYSTEM BASED ON IN-SPACE SOLAR ENERGY
E.T.COMPACT aims to advance three in-space technologies for solar energy harvesting and green propulsion, enhancing efficiency and reducing costs for future space missions.
Projectdetails
Introduction
E.T.COMPACT is aimed at reaching technology readiness level four for three in-space technologies in the domain of solar energy harvesting and green propulsion.
Technology Overview
Thin Film Tandem Module
The first technology is a thin film 2-terminal tandem CIGS/Perovskite module with:
- Efficiency larger than 15%
- Power-per-weight ratio larger than 50W/kg
This technology is designed to reduce the cost of in-space solar panels.
Miniaturized Green-Propulsion Mobility Module
The second technology is a miniaturized (target volume 3U) green-propulsion mobility module device based on an electrodynamic tether. Key features include:
- Tether reel-in/reel-out capability
- Equipped with a field emission cathode
The mobility module can use the harvested in-space solar energy to produce propulsion (both thrust and drag) without using propellant or expellant.
Research on Ultrathin Structures
For the mobility module and the satellite platform to host it, research on ultralight structures based on 3D printed compliant polymeric techniques is conducted. The goals are:
- Mass reduction
- Integration of compliance mechanisms for both tether deployment and thin-film solar panel unfolding
Novel Bare-Photovoltaic Tether
The third technology combines the experience and knowledge of the consortium on photovoltaic and tether technologies. It features a novel bare-photovoltaic tether that:
- Uses the metallic tape tether for both electron collection and as the back contact of tandem CIGS/Perovskite modules
- Integrates solar energy harvesting and propellant-less propulsion in a single device
Project Impact
Project impact is enhanced by activities on:
- Market analysis
- Unit mass production
- Early commercialization
These activities are solidly supported by simulation work to assess the use of these technologies in the fields of:
- Post mission disposal
- Active debris removal
- In-orbit servicing
- Space tugs
Financiële details & Tijdlijn
Financiële details
Subsidiebedrag | € 3.972.890 |
Totale projectbegroting | € 3.972.890 |
Tijdlijn
Startdatum | 1-10-2024 |
Einddatum | 30-9-2027 |
Subsidiejaar | 2024 |
Partners & Locaties
Projectpartners
- UNIVERSIDAD CARLOS III DE MADRIDpenvoerder
- DEIMOS ENGINEERING AND SYSTEMS SLU
- UNIVERSITA DEGLI STUDI DI PADOVA
- TECHNISCHE UNIVERSITAET DRESDEN
- HALOCELL EUROPE SRL
- SUNPLUGGED - SOLARE ENERGIESYSTEME GMBH
- PERSEI SPACE SL
Land(en)
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