CHEOPS Very High-Power Building Blocks

Información del proyecto

CHEOPS-VHP-BB

Identificador del acuerdo de subvención: 101082532

DOI

10.3030/101082532

Fecha de la firma de la CE 25 Noviembre 2022

Fecha de inicio 1 Enero 2023

Fecha de finalización 31 Marzo 2026

Financiado con arreglo a

• Digital, Industry and Space

Coste total

€ 1 971 131,25

Aportación de la UE

€ 1 499 853,00

Coordinado por

SAFRAN ELECTRONICS & DEFENSE
France

CORDIS proporciona enlaces a los documentos públicos y las publicaciones de los proyectos de los programas marco HORIZONTE.

Los enlaces a los documentos y las publicaciones de los proyectos del Séptimo Programa Marco, así como los enlaces a algunos tipos de resultados específicos, como conjuntos de datos y «software», se obtienen dinámicamente de OpenAIRE .

Resultado final

Documents, reports (5)

Public website of the project and established social media profiles

Website will be developed and published online. Report on rationale of website will be provided. Social media accounts will be established and published.

Propellant selection for VHP Hall thruster characterization testing

The document will provide the trade-off analysis of the propellant options (Xe, Kr, Ar, N2) including aspects related to performance, cost, system, integrability, mission analysis, criticalities vs facilities/health issues, etc

Data Management Plan

The document will describe the partners data management processes, agreed rules and criteria adopted for the data exchange and exploitation on the various activities.

System level impact on spacecraft and required HET performance for VHP thrusters

Based on previous mission analyses, a specification of VHP thursters (use duration,…) is provided.

Power systems architecture trade-off report

This document lists and compares different power architectures compatible with the different missions based on EDDA and CHEOPS-VHP tests.

Publicaciones

Conference proceedings (6)

Characterisation of the 20 kW TANDEM Hall Thruster Cathode and 3D-printed Anodes in the Framework of the CHEOPS-VHP-BB Project

Autores: Francesco Marconcini, Raffaello Bottai, Lorenzo Petroni, Davide Picciau, Federico Dini, Ugo Cesari, Federico Cannelli, Simone Scaranzin, Elisa Bonelli, Leonardo Sestini, Marco Bartali, Francesco Avanzi, Lorenzo Bruni, Pietro Pacciani, and Fabrizio Scortec
Publicado en: 39th International Electric Propulsion Conference, Imperial College London, London, United Kingdom 14-19 September 2025
Editor: Researchgate

Technology Demonstration testing of the PPS20k Thruster

Autores: Antonio Piragino, Alexandros Papamatthaiou, Olivier Duchemin, Claude-Martin Brito Frederic Marchandise, Giovanni Coduti, Benjamin Laurent and Vanessa Vial – Safran Spacecraft Propulsion France Alexis Lecervoisier and Stephane Mazouffre – ICARE – CNRS F
Publicado en: 39th International Electric Propulsion Conference Imperial College London, London, United Kingdom, 14-19 September 2025
Editor: Researchgate

Development of a Hight-current cathode for the CHEOPS VHP BB project

Autores: Guidi, F. Marconcini, G. Giammarinaro
Publicado en: Space Propulsion 2024, 2024
Editor: 3AF

Characterisation of a 20 kW Dual Channel HT with Different Propellants (Xe/Kr/Ar)

Autores: S. Scaranzin, F. Scortecci, E. Bonelli, L. Manzolillo , M. Bartalim, F. Avanzi, L.Sestini, F. Dini, F. Cannelli, U. Cesari, and F. Marconcini – AEROSPAZIO Tecnologie Srl F. Paganucci, G. Becatti, M.M. Saravia, G. Giammarinaro, and C. Guidi – University o
Publicado en: 39th International Electric Propulsion Conference Imperial College London, London, United Kingdom, 14-19 September 2025
Editor: Researchgate

Electric Propulsion Activities at the University of Pisa

Autores: Fabrizio Paganucci and Mariano Andrenucci
Publicado en: 38th International Electric Propulsion Conference, 2024
Editor: ERPS

Fused Filament Fabrication of Alumina Components for Hall Thrusters

Autores: Guido Giammarinaro, Francesco Marconcini and Carla Guidi
Publicado en: 38th International Electric Propulsion Conference, 2024
Editor: ERPS

Other (1)

Characterisation of a 20 kW Dual Channel Hall Thruster in the Framework of the ESA TANDEM Project

Autores: S. Scaranzin, F.Scortecci, E. Bonelli, L. Sestini, M. Bartali and F. Avanzi – AEROSPAZIO Tecnologie Srl U. Cesari, F. Dini and F. Cannelli – AEROSPAZIO Tecnologie Srl G. Giammarinaro, F. Marconcini, F. Paganucci, M. Saravia and G. Becatti – University o
Publicado en: 8th International Electric Propulsion Conference (IEPC 2024), Toulouse, France, June 2024
Editor: Researchgate