MICROTHRUST
MEMS-Based Electric Micropropulsion for Small Spacecraft to Enable Robotic Space Exploration and Space Science
| Coordinatore | ECOLE POLYTECHNIQUE FEDERALE DE LAUSANNE
Organization address
address: BATIMENT CE 3316 STATION 1 contact info |
| Nazionalità Coordinatore | Switzerland [CH] |
| Sito del progetto | http://www.microthrust.net/ |
| Totale costo | 2˙842˙535 € |
| EC contributo | 1˙992˙906 € |
| Programma | FP7-SPACE
Specific Programme "Cooperation": Space |
| Code Call | FP7-SPACE-2010-1 |
| Funding Scheme | CP |
| Anno di inizio | 2010 |
| Periodo (anno-mese-giorno) | 2010-12-01 - 2013-11-30 |
Partecipanti
| # | ||||
|---|---|---|---|---|
| 1 |
ECOLE POLYTECHNIQUE FEDERALE DE LAUSANNE
Organization address
address: BATIMENT CE 3316 STATION 1 contact info |
CH (LAUSANNE) | coordinator | 480˙292.40 |
| 2 |
QUEEN MARY UNIVERSITY OF LONDON
Organization address
address: 327 MILE END ROAD contact info |
UK (LONDON) | participant | 454˙159.60 |
| 3 |
NANOSPACE AB
Organization address
address: SOLNA STRANDVAG 86 contact info |
SE (SOLNA) | participant | 419˙660.00 |
| 4 |
NEDERLANDSE ORGANISATIE VOOR TOEGEPAST NATUURWETENSCHAPPELIJK ONDERZOEK TNO
Organization address
address: Schoemakerstraat 97 contact info |
NL (DEN HAAG) | participant | 320˙048.50 |
| 5 |
SystematIC design bv
Organization address
address: motorenweg 5G contact info |
NL (Delft) | participant | 318˙746.00 |
Mappa
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Obiettivo del progetto (Objective)
'Our MicroThrust proposal addresses the FP7 target for advanced in-space propulsion technologies for solar system exploration. This research provides a key component in facilitating exploration missions: a technology that can substantially reduce the cost of undertaking particular types of robotic exploration. Building on the framework of a successful ESA study, our team of leading academics, research institutions and space companies has developed a conceptual design of a very small, yet highly performant electrical propulsion system. The conceptual design is based upon experimental data already obtained by team members. As a result we are confident that this system can provide the transportation element for taking nano/micro satellites to any location in the Earth-Moon system and will even allow missions to nearby planets and asteroids. The propulsion system will thus permit new exploration mission concepts. These missions due to their size will be developed within a fraction of the time for conventional missions. Their simplicity, perhaps even single instrument spacecraft, will reduce risk for carrying out the mission. Overall this will dramatically reduce cost of individual missions, thus providing more flight opportunities for planetary scientists and planetary exploration. To achieve these goals the propulsion technology has high performance at low mass and low power demand. The propulsion system is a microfabricated colloid thruster having a high degree of subsystem integration. Our work so far has demonstrated the capability of this concept to have a radically reduced part set making substantial progress towards a thruster-on-a-chip. Our experienced team will take the technology through to the significant position of having tested and fully characterized a breadboard model. The design approach is that this is also a proto-flight model such that gaining the final step of a flight test for the hardware is low risk and low development cost.'
Introduzione (Teaser)
Sending a satellite into space and placing it in orbit takes hundreds of thousands of litres of fuel. What if all this propellant wasn't necessary?
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