ELSA

European Levitated Spherical Actuator

 Coordinatore CSEM CENTRE SUISSE D'ELECTRONIQUE ET DE MICROTECHNIQUE SA - RECHERCHE ET DEVELOPPEMENT 

 Organization address address: RUE JAQUET DROZ 1
city: NEUCHATEL
postcode: 2007

contact info
Titolo: Mr.
Nome: Emmanuel
Cognome: Onillon
Email: send email
Telefono: 41327205402
Fax: 41327205950

 Nazionalità Coordinatore Switzerland [CH]
 Sito del progetto http://elsa-project.eu/
 Totale costo 3˙143˙570 €
 EC contributo 1˙966˙305 €
 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   -   2014-11-30

 Partecipanti

# participant  country  role  EC contrib. [€] 
1    CSEM CENTRE SUISSE D'ELECTRONIQUE ET DE MICROTECHNIQUE SA - RECHERCHE ET DEVELOPPEMENT

 Organization address address: RUE JAQUET DROZ 1
city: NEUCHATEL
postcode: 2007

contact info
Titolo: Mr.
Nome: Emmanuel
Cognome: Onillon
Email: send email
Telefono: 41327205402
Fax: 41327205950

CH (NEUCHATEL) coordinator 723˙431.00
2    maxon motor ag

 Organization address city: Sachseln
postcode: 6072

contact info
Titolo: Mr.
Nome: Graziano
Cognome: Santarella
Email: send email
Telefono: +41 41 666 15 94
Fax: +41 41 666 16 50

CH (Sachseln) participant 558˙605.00
3    CENTRUM BADAN KOSMICZNYCH POLSKIEJ AKADEMII NAUK

 Organization address address: BARTYCKA 18 A
city: WARSZAWA
postcode: 00 716

contact info
Titolo: Dr.
Nome: Roman
Cognome: Wawrzaszek
Email: send email
Telefono: 48694385845

PL (WARSZAWA) participant 228˙450.00
4    SOCIETE ANONYME BELGE DE CONSTRUCTIONS AERONAUTIQUES-S.A.B.C.A.

 Organization address address: Chaussee de Haecht 1470
city: BRUXELLES
postcode: 1130

contact info
Titolo: Ms.
Nome: Kathy
Cognome: Vekemans
Email: send email
Telefono: +32 2 7295813
Fax: +32 2 7295893

BE (BRUXELLES) participant 221˙875.00
5    SENER INGENIERIA Y SISTEMAS S.A.

 Organization address address: AVENIDA ZUGAZARTE 56
city: GETXO
postcode: 48930

contact info
Titolo: Mr.
Nome: Juan Manuel
Cognome: Del Cura Velayos
Email: send email
Telefono: +34 918077297

ES (GETXO) participant 156˙635.00
6    REDSHIFT DESIGN AND ENGINEERING BVBA

 Organization address address: MARKT 21A
city: RUMST
postcode: 2840

contact info
Titolo: Mr.
Nome: Tom
Cognome: Beuselink
Email: send email
Telefono: 3237774464

BE (RUMST) participant 77˙309.00

Mappa


 Word cloud

Esplora la "nuvola delle parole (Word Cloud) per avere un'idea di massima del progetto.

sphere    power    actuator    mass    phase    satellites    mission    esa    navigation    allocated    steps    space    performance    reaction    attitude   

 Obiettivo del progetto (Objective)

'The ELSA project has the goal of improving European capacity to independently manufacture commercial and scientific satellites by bringing a new actuator for attitude and orbit control systems to a higher level of maturity. This goal is in line with ESA’s technology strategy and long term plan. Support for initial development activities for this innovative actuator technology was provided within the framework of ESA’s GSTP program. The concept consists of a levitated sphere that can be accelerated about any axis producing a resultant torque in any direction. This system aims at replacing the three (or four) traditional reaction wheels or control moment gyroscopes commonly used in satellites and spacecrafts. It reduces the mass and power supply allocated to theattitude and navigation unit. The mass and power saved can be allocated to the payload. The concept offers performance gain; it provides more momentum for a given system mass in comparison with the current inertial subsystems. It improves the system reliability as no mechanical bearings are present and allows more flexible mission planning. This project, proposed for activity 9.2, 'Strengthening the foundations of Space science and technology', topic SPA.2011.2.1-02, 'Research and development for space exploration', comprises three phases. Phase 1 will define the system specifications, based on an extensive market study of potential user's requirements, and identify a reference mission that will provide requirements in term of attitude and navigation control. Phase 2 will comprise the system design, manufacturing and integration, including a feasibility study of the steps necessary to spatialize the design and increase its technology readiness level. Where possible some of the identified spatialization steps will be implemented as part of this project. The project will conclude with phase 3, which will include system tests and performance assessments to demonstrate the potential of the Reaction Sphere.'

Altri progetti dello stesso programma (FP7-SPACE)

L-µPPT (2011)

Innovative Liquid Micro Pulsed Plasma Thruster system for nanosatellites

Read More  

MIDAS (2010)

Millimetre-wave Integrated Diode and Amplifier Sources

Read More  

SEN3APP (2013)

PROCESSING LINES AND OPERATIONAL SERVICES COMBINING SENTINEL AND IN-SITU DATA FOR TERRESTRIAL CRYOSPHERE AND BOREAL FOREST ZONE

Read More