µFCU
Miniaturized Flow Control Unit
| Coordinatore | AST ADVANCED SPACE TECHNOLOGIES GMBH
Organization address
address: ZEPPELINSTRASSE 9B contact info |
| Nazionalità Coordinatore | Germany [DE] |
| Sito del progetto | http://www.microfcu.com/ |
| Totale costo | 2˙059˙936 € |
| EC contributo | 1˙428˙212 € |
| Programma | FP7-SPACE
Specific Programme "Cooperation": Space |
| Code Call | FP7-SPACE-2011-1 |
| Funding Scheme | CP-FP |
| Anno di inizio | 2011 |
| Periodo (anno-mese-giorno) | 2011-12-01 - 2013-09-30 |
Partecipanti
| # | ||||
|---|---|---|---|---|
| 1 |
AST ADVANCED SPACE TECHNOLOGIES GMBH
Organization address
address: ZEPPELINSTRASSE 9B contact info |
DE (STUHR) | coordinator | 567˙485.56 |
| 2 |
STAIGER GMBH & CO KG
Organization address
address: Johannes-Biegstrasse 8 contact info |
DE (Erligheim) | participant | 342˙160.00 |
| 3 |
RHP-TECHNOLOGY GMBH & CO KG
Organization address
address: FORSCHUNGS UND TECHNOLOGIEZENTRUM GEBAUDE CA contact info |
AT (SEIBERSDORF) | participant | 265˙742.00 |
| 4 |
TransMIT Gesellschaft fuer Technologietransfer mbH
Organization address
address: Kerkrader Strasse 3 contact info |
DE (GIESSEN) | participant | 128˙418.00 |
| 5 |
INNOVATIVE SENSOR TECHNOLOGY AG
Organization address
address: INDUSTRIESTRASSE 2 contact info |
CH (WATTWIL) | participant | 124˙406.45 |
Mappa
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Obiettivo del progetto (Objective)
'This proposal is related to FP7 space call 2011 - SPA.2011.2.2-02 (Space critical technologies). The purpose of the proposed work is the development of a miniaturized flow control unit (µFCU) for noble gases like xenon. The proposed technology is relevant to the call as it is listed in the Urgent Action List (ID 13). It is requested by space industry and agencies according ESTER database (e.g. ref. T-8117, T-8119). The new development shall reduce Europe's dependency from other space fairing nations by using only European components.
From a technical point of view, the proposal is also related to SPA.2011.2.2-01 (Space transportation technologies) as it enables electric micropropulsion systems for new mission classes.
The μFCU design is based on a component-of-the-shelf (COTS) approach. The core components and technologies have already been developed for ground applications. They have a high reliability background like medicine, chemical industry or even space. These components will be modified for space applications and for the changed operational and environmental parameter range.
This new development shall outperform existing technologies with respect to mass reduction, leak tightness, drift and long term stability. Furthermore, it shall reduce complexity, driver electronics requirements and AIT effort and therefore will reduce cost. Further cost reduction shall be achieved by modularity, use of COTS and integration of for flow lines controllers into one device.
The design of the µFCU is driven by costumer requirements. Key customer already agreed to join an Advisory Board. The Advisory Board shall support the project by defining reference missions and by reviewing the design.
The Consortium has a strong focus on SMEs with first experiences in space business. Some partners already have a strong and long term involvement in space component and subsystem development.'
Introduzione (Teaser)
Miniaturisation has always been an issue in space technology, since weight reduction is in constant demand. A new miniaturised flow control unit for noble gases like xenon produces electric propulsion for smaller missions.