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CHEOPS SIGNED

Consortium for Hall Effect Orbital Propulsion System

Total Cost €

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EC-Contrib. €

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Partnership

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 CHEOPS project word cloud

Explore the words cloud of the CHEOPS project. It provides you a very rough idea of what is the project "CHEOPS" about.

electric    mode    cheops    propulsion    dual    performances    het    eps    thruster    power    satellite   

Project "CHEOPS" data sheet

The following table provides information about the project.

Coordinator
SAFRAN AIRCRAFT ENGINES 

Organization address
address: BVD DU GENERAL MARTIAL VALIN 2
city: PARIS
postcode: 75015
website: www.safran-aircraft-engines.com

contact info
title: n.a.
name: n.a.
surname: n.a.
function: n.a.
email: n.a.
telephone: n.a.
fax: n.a.

 Coordinator Country France [FR]
 Total cost 14˙817˙142 €
 EC max contribution 10˙960˙028 € (74%)
 Programme 1. H2020-EU.2.1.6.2. (Enabling advances in space technology)
2. H2020-EU.2.1.6.1.1. (Safeguard and further develop a competitive, sustainable and entrepreneurial space industry and research community and strengthen European non-dependence in space systems)
 Code Call H2020-COMPET-2016
 Funding Scheme /IA
 Starting year 2016
 Duration (year-month-day) from 2016-11-01   to  2020-04-30

 Partnership

Take a look of project's partnership.

# participants  country  role  EC contrib. [€] 
1    SAFRAN AIRCRAFT ENGINES FR (PARIS) coordinator 4˙340˙875.00
2    SITAEL SPA IT (MOLA DI BARI) participant 2˙089˙806.00
3    BRADFORD ENGINEERING BV NL (HEERLE) participant 1˙052˙205.00
4    CENTRE NATIONAL DE LA RECHERCHE SCIENTIFIQUE CNRS FR (PARIS) participant 956˙513.00
5    AST ADVANCED SPACE TECHNOLOGIES GMBH DE (STUHR) participant 651˙931.00
6    THALES ALENIA SPACE BELGIUM S.A. BE (MONT SUR MARCHIENNE) participant 600˙071.00
7    UNIVERSIDAD CARLOS III DE MADRID ES (GETAFE (MADRID)) participant 360˙001.00
8    CHALMERS TEKNISKA HOEGSKOLA AB SE (GOETEBORG) participant 332˙012.00
9    DEUTSCHES ZENTRUM FUER LUFT - UND RAUMFAHRT EV DE (KOELN) participant 175˙696.00
10    SME4SPACE VZW BE (HEVERLEE) participant 135˙874.00
11    OHB SYSTEM AG DE (BREMEN) participant 94˙705.00
12    AIRBUS DEFENCE AND SPACE SAS FR (TOULOUSE CEDEX) participant 92˙750.00
13    THALES ALENIA SPACE FRANCE FR (TOULOUSE) participant 77˙585.00

Mappa

 Project objective

CHEOPS proposes to develop three different Hall Effect Thruster electric propulsion systems: a dual mode EPS for GEO applications, a low power for LEO applications and a >20 kW high thrust EPS for exploration applications. Each of these will be developed according to market needs and drivers applying incremental technology changes to existing EPS products. The development approach will follow the ESA ECSS approach and the dual mode and low power are targeting a System PDR review with 42 months from the project start. Development will cover the following elements: thruster, cathode, PPU and FMS. The project is perfectly aligned to the SRC guidelines published with the call. Through a detailed development plan the project will demonstrate their ability to achieve by the end of CHEOPS Phase II (2023) the following: a) TRL7-8 for dual mode and low power b) high power HET EPS TRL6. Common transverse activities will include advanced numerical design tools for electric propulsion which will further the understanding of the observable behaviour and interactions with the satellite platform and predict performances of a given design. This includes alternative propellants and the ability to estimate the system lifetime. Finally significant progress will be made in establishing a HET performances measurement standard and developing advanced non-intrusive tests for measuring thruster erosion. The CHEOPS consortium is led by SNECMA and is comprised of representatives of the biggest European Prime satellite makers, the full EPS supply chain and supported by academia.

 Work performed, outcomes and results:  advancements report(s) 

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