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TeSeR

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Cerrado

Technology for Self Removal of Spacecraft

Orbital space is getting increasingly crowded and a few collision events could jeopardize activities in important orbits and cause significant damage to the infrastructure in space. As a preventive measure to be included in future... ver más

31/03/2019

AIRBUS DEFENCE AND...

3M€

Presupuesto del proyecto: 3M€

Líder del proyecto

AIRBUS DEFENCE AND SPACE GMBH 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 11 Participantes

Financiación concedida El organismo H2020 notifico la concesión del proyecto el día 2019-03-31

PROTEC-1-2015: Passive means to reduce the impact... Scope:Specific Challenge: Reducing the impact of collisions between active satellites and orbital de...

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Cerrada hace 10 años

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Características del participante

Este proyecto no cuenta con búsquedas de partenariado abiertas en este momento.

Información adicional privada

No hay información privada compartida para este proyecto. Habla con el coordinador.

11 Participantes

AIRBUS DEFENCE AND SPACE GMB...

856.41K€ | Lider

DORBIT SPA

417.40K€ | Participante

HTG GmbH

34.59K€ | Participante

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Duración del proyecto: 40 meses Fecha Inicio: 2015-11-27
Fecha Fin: 2019-03-31

Líder del proyecto

AIRBUS DEFENCE AND SPACE GMBH 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 Orbital space is getting increasingly crowded and a few collision events could jeopardize activities in important orbits and cause significant damage to the infrastructure in space. As a preventive measure to be included in future S/C, TeSeR proposes a universal post mission disposal module to be carried into orbit by any S/C to ensure its proper disposal after ending its service lifetime, be it planned or unscheduled due to S/C failure. This module shall be independent of the S/C. Principal aims of TeSeR are to 1. develop a removal module beginning with the exploration of concepts, going for a functional design with the aim to manufacture and test an on-ground prototype module which demonstrates the main functions 2. perform a thorough qualitative and quantitative mission analysis of existing removal concepts 3. develop a ground breaking new semi-controlled removal concept based on a passive removal concept which ensures the deorbit of a large S/C (>1 t) into the Pacific Ocean without a propulsion system but with an accuracy of a fraction of one orbit 4. advance and manufacture removal subsystems prototypes, for controlled, semi-controlled and uncontrolled disposal, based on already existing technology with the focus on scalability and standardized implementation to the removal module via a common interface 5. analyse the feasibility and potential advantages of multi-purpose concepts of the module and its removal subsystems (e.g. shielding by deployable structures) 6. perform a market study and define a business case for TeSeR 7. use TeSeR as leverage to propose changes in legal aspects and advanced state of the art licensing standard for spacecraft including the improvement of international debris mitigation guidelines and standards

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