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CHEOPS MEDIUM POWER

Financiado

Cerrado

Consortium for Hall Effect Orbital Propulsion System Phase 2 covering MEDIUM P...

Consortium for Hall Effect Orbital Propulsion System Phase 2 covering MEDIUM POWER needs To prepare future large satellite missions, replace obsolete networks or introduce new on-board technological advances, Europe must offer to its satellite industry a competitive and highly reliable European dual mode Hall-effect E... ver más

31/03/2025

SAFRAN SPACECRAFT...

6M€

Presupuesto del proyecto: 6M€

Líder del proyecto

SAFRAN SPACECRAFT PROPULSION No se ha especificado una descripción o un objeto social para esta compañía.

Fecha límite participación Sin fecha límite de participación.

Ver 11 Participantes

Financiación concedida El organismo H2020 notifico la concesión del proyecto el día 2020-11-05

SPACE-28-TEC-2020: SRC - In-space electrical propulsio...

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

11 Participantes

SAFRAN SPACECRAFT PROPULSION

2.24M€ | Lider

DECOLETAJE Y TORNILLERIA SA

277.50K€ | Participante

CNRS

331.00K€ | Participante

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Duración del proyecto: 52 meses Fecha Inicio: 2020-11-05
Fecha Fin: 2025-03-31

Líder del proyecto

SAFRAN SPACECRAFT PROPULSION No se ha especificado una descripción o un objeto social para esta compañía.

Presupuesto del proyecto 6M€

Fecha límite de participación Sin fecha límite de participación.

Descripción del proyecto To prepare future large satellite missions, replace obsolete networks or introduce new on-board technological advances, Europe must offer to its satellite industry a competitive and highly reliable European dual mode Hall-effect Electric Propulsion System able to provide sufficient power to perform both orbit raising (7kW) and station keeping (3kW) duties. Based on CHEOPS Phase I results, CHEOPS MEDIUM POWER will perform incremental developments on system and sub-system levels in order to achieve TRL6/7 by 2025. CHEOPS MEDIUM POWER will further mature the different system elements (Thruster Unit, PPU, FMS) by addressing the following key challenges: non-recurring and recurring cost reduction in terms of design, manufacturing, test qualification and time to deliver, as well as propellent efficiency in order to increase valuable payload and generate revenues. These advancements will fit into a less than 10kg thruster working between 300 and 450V. CHEOPS MEDIUM POWER will deliver for the thruster unit an optimised design for a very high thrust and improved lifecycle durations. On an industrial level the project aims at reduced fabrication cycles, improved quality, leaner manufacture, faster assembly lead times, and improved tolerance management. The Power processing unit will be optimised by removing unnecessary functions and re-selecting cheaper key components with at least constant reliability levels. The project’s scope extends to FMS level where space qualifiable COTS will be used to provide maximum mission suitability for variable number of thrusters per satellite. CHEOPS MEDIUM POWER will have a medium-term impact on the European space industry and its overall competitiveness, but also on the satellite design and manufacturing paradigm in the long term.

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