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REVUS

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Reducing the Vulnerability of Space Systems

It is accepted that space debris will increase in the next decades despite any considerable effort made to limit their generation. Debris of more than 10cm can be avoided by the satellites and also the very small particles of less... ver más

31/12/2013

AIRBUS DEFENCE AND...

3M€

Presupuesto del proyecto: 3M€

Líder del proyecto

AIRBUS DEFENCE AND SPACE SAS No se ha especificado una descripción o un objeto social para esta compañía.

TRL 4-5

Fecha límite participación Sin fecha límite de participación.

Ver 9 Participantes

Financiación concedida El organismo FP7 notifico la concesión del proyecto el día 2013-12-31 No tenemos la información de la convocatoria

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9 Participantes

AIRBUS DEFENCE AND SPACE SAS

0.00€ | Lider

ULEIC

N.D. | Participante

SOUTHAMPTON

N.D. | Participante

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Líder del proyecto

AIRBUS DEFENCE AND SPACE SAS No se ha especificado una descripción o un objeto social para esta compañía.

TRL 4-5

Presupuesto del proyecto 3M€

Fecha límite de participación Sin fecha límite de participación.

Descripción del proyecto It is accepted that space debris will increase in the next decades despite any considerable effort made to limit their generation. Debris of more than 10cm can be avoided by the satellites and also the very small particles of less than 0.1cm are taken into account in the current designs. The debris from 0.1 to 10cm is however not predictable, not taken into account today and could severely damage a spacecraft. The probability of damage by such particles could reach an unacceptable level thus creating a new paradigm for LEO satellites. A better protection of space systems against damage caused by debris collision is the aim of the ReVuS study, articulated around 4 lines: - To restore the existing models and works for the prediction and the knowledge of damage assessment (LDEF, SS, Colombus…). - To assess the solutions  At system level, with distributed/fractionated architectures, or by using active detection and mitigation strategies. On the satellite exterior, by defining and testing new shielding materials derived from ground markets In the satellite interior , by editing new rules of harness routing & equipment configuration - Resilience analysis, evaluating the proposed solutions & generating recommendations/design rules. Assess possible standardisation. - To dispatch the results to the space community. METOP and a Radar satellite will be used as a guiding principle for all the analysis The consortium led by Astrium Satellites gathers all expertise required. The Ernst-Mach-Institut (EMI Fraunhoffer), the universities of Surrey, Southampton & Braunschweig will provide the background knowledge and models. The shielding materials will be defined by TenCate Advanced Composites, and tested in the EMI facilities. The users will participate in the analysis. HisCox will represent the insurer of the satellite. The dissemination of the results will be ensured by Astri Polska Sp.z o.o

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