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EARS

Financiado

Cerrado

European Advanced Reusable Satellite

This program proposes to design and build a low-cost spacecraft capable of supporting a variety of small experiments for orbital periods potentially longer than a year. The vehicle is to be designed to operate and return to Earth... ver más

31/12/2024

CNR

1M€

Presupuesto del proyecto: 1M€

Líder del proyecto

CONSIGLIO NAZIONALE DELLE RICERCHE 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 6 Participantes

Financiación concedida El organismo HORIZON EUROPE notifico la concesión del proyecto el día 2024-12-31

HORIZON-CL4-2021-SPACE-01-23: New space transportation solutions... ExpectedOutcome:Projects are expected to contribute to all of the following outcomes:

I+D

Cerrada hace 2 años

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Información adicional privada

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

6 Participantes

CNR

200.00K€ | Lider

DEIMOS CASTILLA LA MANCHA

293.30K€ | Participante

UNIPD

99.95K€ | Participante

NANOAVIONICS

208.97K€ | Participante

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Duración del proyecto: 26 meses Fecha Inicio: 2022-10-18
Fecha Fin: 2024-12-31

Líder del proyecto

CONSIGLIO NAZIONALE DELLE RICERCHE No se ha especificado una descripción o un objeto social para esta compañía.

TRL 4-5

Presupuesto del proyecto 1M€

Fecha límite de participación Sin fecha límite de participación.

Descripción del proyecto This program proposes to design and build a low-cost spacecraft capable of supporting a variety of small experiments for orbital periods potentially longer than a year. The vehicle is to be designed to operate and return to Earth autonomously, to be reusable with minimal refurbishment, and to be compatible with common launch vehicles secondary payload attachments. The spacecraft is based on a current microsatellite platform with the addition of a heat shield, a powerful propulsion system and a recover system. The spacecraft is launched in LEO and perform its mission, which can be IOD/IOV, microgravity scientific experiments, or commercial activities like microgravity manufacturing. Thanks to its own propulsion system the spacecraft can re-position itself and perform a controlled reentry. After reentry and when the vehicle slows to the designated Mach number, a drogue parachute will be deployed which will decelerate the vehicle to a condition permitting deployment of the steerable gliding parachute. Terminal descent on the main parachute is controlled so that the vehicle soft-lands at a designated landing site. The reusability feature has four main advantages: - Recover of the payload for usage/inspection/analysis - Possibility to reuse the satellite for different missions - Possibility to abort a mission without loss of the payload - Limited pollution, debris mitigation both on ground and in orbit This platform follows the call indications as it deals with re-entry technologies, green propulsion, advanced GNC. Marketing surveys have indicated that there is considerable user interest for such a platform.

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