CHEOPS Very High-Power Building Blocks

Informacje na temat projektu

CHEOPS-VHP-BB

Identyfikator umowy o grant: 101082532

DOI

10.3030/101082532

Projekt został zamknięty

Data podpisania przez KE 25 Listopada 2022

Data rozpoczęcia 1 Stycznia 2023

Data zakończenia 31 Marca 2026

Finansowanie w ramach

• Digital, Industry and Space

Koszt całkowity

€ 1 971 131,25

Wkład UE

€ 1 499 853,00

Koordynowany przez

SAFRAN ELECTRONICS & DEFENSE
France

CORDIS oferuje możliwość skorzystania z odnośników do publicznie dostępnych publikacji i rezultatów projektów realizowanych w ramach programów ramowych HORYZONT.

Odnośniki do rezultatów i publikacji związanych z poszczególnymi projektami 7PR, a także odnośniki do niektórych konkretnych kategorii wyników, takich jak zbiory danych i oprogramowanie, są dynamicznie pobierane z systemu OpenAIRE .

Rezultaty

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.

Publikacje

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

Autorzy: 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
Opublikowane w: 39th International Electric Propulsion Conference, Imperial College London, London, United Kingdom 14-19 September 2025
Wydawca: Researchgate

Technology Demonstration testing of the PPS20k Thruster

Autorzy: 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
Opublikowane w: 39th International Electric Propulsion Conference Imperial College London, London, United Kingdom, 14-19 September 2025
Wydawca: Researchgate

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

Autorzy: Guidi, F. Marconcini, G. Giammarinaro
Opublikowane w: Space Propulsion 2024, 2024
Wydawca: 3AF

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

Autorzy: 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
Opublikowane w: 39th International Electric Propulsion Conference Imperial College London, London, United Kingdom, 14-19 September 2025
Wydawca: Researchgate

Electric Propulsion Activities at the University of Pisa

Autorzy: Fabrizio Paganucci and Mariano Andrenucci
Opublikowane w: 38th International Electric Propulsion Conference, 2024
Wydawca: ERPS

Fused Filament Fabrication of Alumina Components for Hall Thrusters

Autorzy: Guido Giammarinaro, Francesco Marconcini and Carla Guidi
Opublikowane w: 38th International Electric Propulsion Conference, 2024
Wydawca: ERPS

Other (1)

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

Autorzy: 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
Opublikowane w: 8th International Electric Propulsion Conference (IEPC 2024), Toulouse, France, June 2024
Wydawca: Researchgate