Opendata, web and dolomites

MSR

Multifunctional Satellite Radiator

Total Cost €

0

EC-Contrib. €

0

Partnership

0

Views

0

 MSR project word cloud

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

honeycombs    advantages    country    boxes    stiffness    isotropic    satellite    mission    structure    integrally    sandwich    spacecraft    structural    share    heavy    milled    panels    business    bearing    hardware    leader    thermal    radiator    easier    orbits    pipes    instruments    definition    performance    panel    foam    space    outer    contact    man    became    securing    located    radiators    radiation    opportunity    full    electronic    lightweight    gap    lack    insert    missions    facesheet    class    made    metallic    grounding    superior    strength    enhanced    honeycomb    medium    sheet    combined    capability    debris    multifunctional    frequently    integral    bond    ratio    conductance    small    conventional    afs    hungarian    plane    assets    sme    adhesives    sheets    good    heat    market    ensures    fill    mechanical    originally    shell    weight    protection    core    provider    thick    manufactured    aluminum    outgassing    esa    degree    cosmic    load   

Project "MSR" data sheet

The following table provides information about the project.

Coordinator
ADMATIS KUTATO, GYARTO ES KERESKEDELMI KORLATOLT FELELOSSEGU TARSASAG 

Organization address
address: PARTOS UTCA 16
city: MISKOLC
postcode: 3535
website: www.admatis.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 Hungary [HU]
 Project website http://www.admatis.com
 Total cost 71˙429 €
 EC max contribution 50˙000 € (70%)
 Programme 1. H2020-EU.2.1.6. (INDUSTRIAL LEADERSHIP - Leadership in enabling and industrial technologies – Space)
2. H2020-EU.2.3.1. (Mainstreaming SME support, especially through a dedicated instrument)
 Code Call H2020-SMEINST-1-2015
 Funding Scheme SME-1
 Starting year 2015
 Duration (year-month-day) from 2015-07-01   to  2015-12-31

 Partnership

Take a look of project's partnership.

# participants  country  role  EC contrib. [€] 
1    ADMATIS KUTATO, GYARTO ES KERESKEDELMI KORLATOLT FELELOSSEGU TARSASAG HU (MISKOLC) coordinator 50˙000.00

Map

 Project objective

Multifunctional Satellite Radiator

Securing space assets against man-made space debris present at frequently used orbits became integral part of space mission definition and overall spacecraft design. Radiator panels as part of the outer shell of spacecraft already provide some degree of protection to the instruments behind them. Overall project objective is to develop a new class of multifunctional structural radiators for small and medium satellite missions where high mechanical and thermal performance shall be combined with improved space debris and cosmic radiation protection characteristics.

Radiator panels manufactured from aluminum foam sandwich (AFS) are able to fill the gap between conventional honeycomb and integrally milled structural radiators. Due to the lightweight core they offer high stiffness-to-weight ratio like honeycombs while the metallic bond between facesheet and core ensures superior load bearing capability and thermal conductance provided by integrally milled radiators. AFS radiators are capable to provide mechanical support for heavy electronic boxes, offer good thermal performance combined with enhanced radiation and debris protection for the hardware located behind the radiator panel. Main advantages of AFS radiators compared to existing honeycomb based radiators are:

• high in plane thermal conductance without heat pipes due to isotropic core structure, • higher insert strength, • better debris protection, • better radiation protection, • originally thick face sheets can be manufactured according to mechanical and thermal needs, • improved outgassing parameters due to lack of adhesives, • easier grounding implementation due to metallic contact between core and face sheet.

As the result of this development Europe will be the leader provider of satellite radiators meaning significant market share. It is also a promising business opportunity for a Hungarian SME whose country is being a full member of ESA.

Are you the coordinator (or a participant) of this project? Plaese send me more information about the "MSR" project.

For instance: the website url (it has not provided by EU-opendata yet), the logo, a more detailed description of the project (in plain text as a rtf file or a word file), some pictures (as picture files, not embedded into any word file), twitter account, linkedin page, etc.

Send me an  email (fabio@fabiodisconzi.com) and I put them in your project's page as son as possible.

Thanks. And then put a link of this page into your project's website.

The information about "MSR" are provided by the European Opendata Portal: CORDIS opendata.

More projects from the same programme (H2020-EU.2.1.6.;H2020-EU.2.3.1.)

ReadyToSail (2016)

ReadyToSail

Read More  

HEART (2018)

HIGH HEAT REJECTION THERMAL CONTROL SYSTEM

Read More  

SPS_TFP_SQ (2015)

TFP Strut Qualification

Read More