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COMAP-4S SIGNED

COmponents and MAcrocomponents Packaging For Space

Total Cost €

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EC-Contrib. €

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Partnership

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 COMAP-4S project word cloud

Explore the words cloud of the COMAP-4S project. It provides you a very rough idea of what is the project "COMAP-4S" about.

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Project "COMAP-4S" data sheet

The following table provides information about the project.

Coordinator
SAFRAN ELECTRONICS & DEFENSE 

Organization address
address: 72-76 RUE HENRY FARMAN
city: PARIS
postcode: 75015
website: www.safran-group.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 2˙975˙275 €
 EC max contribution 2˙975˙275 € (100%)
 Programme 1. H2020-EU.2.1.6.1. (Enabling European competitiveness, non-dependence and innovation of the European space sector)
2. H2020-EU.2.1.6.2. (Enabling advances in space technology)
 Code Call H2020-SPACE-2019
 Funding Scheme RIA
 Starting year 2020
 Duration (year-month-day) from 2020-01-01   to  2022-12-31

 Partnership

Take a look of project's partnership.

# participants  country  role  EC contrib. [€] 
1    SAFRAN ELECTRONICS & DEFENSE FR (PARIS) coordinator 1˙710˙556.00
2    TECHNISCHE UNIVERSITAT BERLIN DE (BERLIN) participant 499˙000.00
3    ADVANCED CIRCUIT BOARDS NV BE (DENDERMONDE) participant 442˙026.00
4    NANOXPLORE FR (SEVRES) participant 323˙692.00

Map

 Project objective

Space markets have entered a new age, thanks to new business models but also to the increased use of deeply integrated electronics aboard satellites, either for digital or analog functions. Such miniaturized equipment allows for drastic reductions of the satellite mass, thus enabling larger payloads and more service revenues, and/or lighter satellites, and then cheaper launches. However, despite the deep submicron technologies currently used for manufacturing space components, efficient and competitive packaging of large components remains a roadblock in trying to downsize further these equipment. This is especially true when we have to address dies beyond 300 mm² and/or beyond 625 pins, such integration being made worse with ever increased power dissipation, up to 10 or 20 W per die. Following-up innovative approaches already developed by the Consortium members, such as European rad-hard FPGA (e.g. BRAVE, DAHLIA, OR VEGAS/OPERA projects), System In Package (SIP) technologies and High Density PCB as experienced with ESA contracts, the principal objective of this project is to design and ECSS qualify a “macro-component” Demonstration Model (DM) for space applications, offering unmatched Figures of Merit for space packaging, in terms of Interconnexion density, Die surface, Integration density, together with a cost reduction factor of 3 compared to ceramic CGA, among others. These challenges are made reachable within a 3-phase program, leveraging advanced technologies in organic high density low CTE PCBs, innovative thermal management and SIP integration up to a TRL7 stage, validating the full industrial processes vs. the ECSS Q ST standards. Furthermore, thanks to the close partnership we have in our Consortium, this COMAP-4S Project will set the stage for a true European supply chain serving additional markets beyond rad-hard space equipment, such as embedded macro-components for Defense or Aeronautics, being fully in line with the objectives of SPACE-10-TEC-2019.

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The information about "COMAP-4S" are provided by the European Opendata Portal: CORDIS opendata.

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