Opendata, web and dolomites

IFM Micro Thruster SIGNED

The unique modular propulsion system suitable for all small satellites from 1 to 500 kg

Total Cost €

0

EC-Contrib. €

0

Partnership

0

Views

0

 IFM Micro Thruster project word cloud

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

time    reliability    manufacturers    several    fires    once    proprietary    life    players    telephone    ranging    re    single    giving    manoeuvres    qualified    needle    version    imaging    commercialization    porous    tungsten    2d    validate    difficult    market    flight    trying    certified    accuracy    limited    tested    sufficient    line    race    commercial    unprecedented    efficiency    suitable    coverage    put    customers    orbits    near    esa    micro    iso    propulsion    deorbiting    engineered    thruster    constellations    shaped    fact    big    rates    array    install    lowering    replacement    propellant    satellites    engineer    2021    ships    9001    amr    space    airplanes    services    difficulties    internet    stability    position    manufacturing    satellite    13    gt    highest    compact    ing    acquire    fit    orbit    2016    monitoring    missions    plasma    small    emitters    modular       graveyard    thrust    investing    global    full    passive    kg    model    constraints    core    worth    cubesats    perfectly    disrupt    500    mass    ifm   

Project "IFM Micro Thruster" data sheet

The following table provides information about the project.

Coordinator
AMR PROPULSION INNOVATIONS GMBH 

Organization address
address: VIKTOR KAPLAN-STRASSE 2
city: WIENER NEUSTADT
postcode: 2700
website: n.a.

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 Austria [AT]
 Project website https://www.enpulsion.com/technology/
 Total cost 1˙671˙825 €
 EC max contribution 1˙170˙277 € (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-2-2016-2017
 Funding Scheme SME-2
 Starting year 2017
 Duration (year-month-day) from 2017-07-01   to  2019-12-31

 Partnership

Take a look of project's partnership.

# participants  country  role  EC contrib. [€] 
1    AMR PROPULSION INNOVATIONS GMBH AT (WIENER NEUSTADT) coordinator 1˙170˙277.00

Map

 Project objective

Several players are investing in Constellations of Satellites to provide customers services as global imaging in near real time, telephone & internet coverage, monitoring of ships, airplanes, fires etc. The global market of this new space race, worth 2.2 B$ in 2016, is expected to increase to 5.3 B$ in 2021. Many manufacturers are trying to disrupt market by lowering manufacturing costs, but the most difficult component to acquire remains the propulsion system: these satellites, in fact, work without a propulsion system, resulting in high replacement rates (once per year), limited orbit manoeuvres, difficulties in flight formation, passive deorbiting not sufficient to put satellites into graveyard orbits at their end of life. AMR propulsion aims to solve these problem with a unique, modular product: the IFM Micro Thruster, a compact, modular propulsion system suitable for all small satellites ranging 1-500 kg, with the highest propellant efficiency, capable of controlling satellites’ position with an unprecedented accuracy, perfectly suitable for single CubeSats as well as for big constellations of satellites (>100). The core, proprietary technology is based on a widely tested (13,000 h) thruster developed for large satellite control in future ESA missions, specifically re-engineered to fit the space and mass constraints of small satellites. The thruster is based on a 2D array of porous tungsten needle-shaped emitters, capable of giving high stability and high reliability to the plasma thrust. During Phase 2 project, AMR will design and engineer the qualified model (i.e. the commercial version) of the IFM Micro Thruster; design and install an ISO-9001 certified production line, and will demonstrate and validate the technology with relevant customers. The overall goal is to reach full commercialization of IFM Micro Thruster at the end of Phase 2.

 Deliverables

List of deliverables.
Project website Websites, patent fillings, videos etc. 2019-07-19 13:52:49

Take a look to the deliverables list in detail:  detailed list of IFM Micro Thruster deliverables.

 Publications

year authors and title journal last update
List of publications.
2019 Grimaud, Lou, Krejci, David, Reissner, Alexander, Seifert, Bernhard
The IFM Micro FEEP thruster: a modular design for smallsat propulsion
published pages: IEPC-2019-675, ISSN: , DOI:
36th International Electric Propulsion Conference 2020-03-11
2019 Grimaud, Lou, Krejci, David, Reissner, Alexander, Seifert, Bernhard
Development and Qualification of the IFM Micro Thruster
published pages: IAC-19,C4,B4.5A,, ISSN: , DOI:
70th International Astronautical Congress 2020-03-11
2019 David Krejci, Alexander Reissner, Dennis Weihrauch
IFM Nano Thruster electric space propulsion: from first Cubesat demonstration to the first 100 thrusters produced
published pages: SSC19-XII-07, ISSN: , DOI:
33rd Annual AIAA/USU Conference on Small Satellites 2020-03-11
2019 Krejci, David, Alexander, Reissner, Schönherr, Tony, , Bernhard, Seifert, Saleem, Zainab, Alejos, Ricardo
Recent flight data from IFM Nano Thrusters in a low earth orbit
published pages: IEPC-2019-724, ISSN: , DOI:
36th International Electric Propulsion Conference 2020-03-11
2019 Weimer, Bryan, Scharlemann, Carsten, David; Reissner, Alexander, Seifert, Bernhard
CLIMB Exploration of the Van Allen Belt by CubeSats
published pages: IEPC-2019-805, ISSN: , DOI:
36th International Electric Propulsion Conference 2020-03-11
2019 Krejci, David, Hugonnaud, Valentin, Schönherr, Tony, Little, Bryan, Reissner, Alexander, Seifert, Bernhard, Koch, Quirin, Bosch Borras, Eduard, Gonzalez del Amo, Jose
Full Performance Mapping of the IFM Nano Thruster including Direct Thrust Measurements
published pages: 881-893, ISSN: 1533-6794, DOI:
Journal of Small Satellites No.2, Vol. 8 2020-03-11
2018 Janzer, Katja, Killian, Matthias, Langer, Martin, Krejci, David, Reissner, Alexander
Thermal Control of High Power Applications on CubeSats
published pages: IAC-18-C2.7.11, ISSN: , DOI:
69th International Astronautical Congress (IAC) 2020-03-11
2018 David Jelem, Alexander Reissner, Bernhard Seifert, Nembo Buldrini, Lissa Wilding, David Krejci
Direct Thrust and Plume Divergence Measurements of the IFM Nano Thruster
published pages: , ISSN: 0273-1177, DOI: 10.1016/j.asr.2018.06.028
Advances in Space Research 2019-07-19
2018 Seifert, Bernhard, Buldrini, Nembo, Hörbe, Thomas, Plesescu, Florin, Reissner, Alexander, Krejci, Krejci, David, Friedhoff, Pete, Lai, Steve
In-Orbit Demonstration of the Indium-FEEP IFM Nano Thruster, SPC2018-183, 6th Space Propulsion Conference
published pages: , ISSN: , DOI:
2019-07-19
2018 Krejci, David, Reissner, Alexander, Seifert, Bernhard, Jelem, David, Hörbe, Thomas, Plesescu, Florin, Friedhoff, Pete, Lai, Steve
Demonstration of the IFM Nano FEEP Thruster in Low Earth Orbit, 4S Symposium 2018
published pages: , ISSN: , DOI:
2019-07-19

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

ASC (2015)

Amorphous Speculative Compression

Read More