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

Informazioni relative al progetto

IFM Micro Thruster

ID dell’accordo di sovvenzione: 779196

DOI 10.3030/779196

Progetto chiuso

Data della firma CE 19 Luglio 2017

Data di avvio 1 Luglio 2017

Data di completamento 31 Dicembre 2019

Finanziato da

• INDUSTRIAL LEADERSHIP - Leadership in enabling and industrial technologies – Space

Costo totale € 1 671 825,00

Contributo UE € 1 170 277,50

Coordinato da

ENPULSION GmbH
Austria

Risultati finali

Websites, patent fillings, videos etc. (1)

Project website

A dedicated page of the Company's website will be dedicated to the project dissemination.

Pubblicazioni

Peer reviewed articles (2)

Direct Thrust and Plume Divergence Measurements of the IFM Nano Thruster

Autori: David Jelem, Alexander Reissner, Bernhard Seifert, Nembo Buldrini, Lissa Wilding, David Krejci
Pubblicato in: Advances in Space Research, 2018, ISSN 0273-1177
Editore: Pergamon Press Ltd.
DOI: 10.1016/j.asr.2018.06.028

Full Performance Mapping of the IFM Nano Thruster including Direct Thrust Measurements

Autori: Krejci, David, Hugonnaud, Valentin, Schönherr, Tony, Little, Bryan, Reissner, Alexander, Seifert, Bernhard, Koch, Quirin, Bosch Borras, Eduard, Gonzalez del Amo, Jose
Pubblicato in: Journal of Small Satellites, Numero No.2, Vol. 8, 2019, Pagina/e 881-893, ISSN 1533-6794
Editore: Journal of Small Satellites

Conference proceedings (8)

Demonstration of the IFM Nano FEEP Thruster in Low Earth Orbit, 4S Symposium 2018

Autori: Krejci, David, Reissner, Alexander, Seifert, Bernhard, Jelem, David, Hörbe, Thomas, Plesescu, Florin, Friedhoff, Pete, Lai, Steve
Pubblicato in: 2018
Editore: ESA Conference Bureau

In-Orbit Demonstration of the Indium-FEEP IFM Nano Thruster, SPC2018-183, 6th Space Propulsion Conference

Autori: Seifert, Bernhard, Buldrini, Nembo, Hörbe, Thomas, Plesescu, Florin, Reissner, Alexander, Krejci, Krejci, David, Friedhoff, Pete, Lai, Steve
Pubblicato in: 2018
Editore: Association Aeronautique et Astronautique de France

The IFM Micro FEEP thruster: a modular design for smallsat propulsion

Autori: Grimaud, Lou, Krejci, David, Reissner, Alexander, Seifert, Bernhard
Pubblicato in: 36th International Electric Propulsion Conference, 2019, Pagina/e IEPC-2019-675
Editore: 36th International Electric Propulsion Conference

Development and Qualification of the IFM Micro Thruster

Autori: Grimaud, Lou, Krejci, David, Reissner, Alexander, Seifert, Bernhard
Pubblicato in: 70th International Astronautical Congress, 2019, Pagina/e IAC-19,C4,B4.5A,13,x52580
Editore: 70th International Astronautical Congress

Recent flight data from IFM Nano Thrusters in a low earth orbit

Autori: Krejci, David, Alexander, Reissner, Schönherr, Tony, , Bernhard, Seifert, Saleem, Zainab, Alejos, Ricardo
Pubblicato in: 36th International Electric Propulsion Conference, 2019, Pagina/e IEPC-2019-724
Editore: 36th International Electric Propulsion Conference

IFM Nano Thruster electric space propulsion: from first Cubesat demonstration to the first 100 thrusters produced

Autori: David Krejci, Alexander Reissner, Dennis Weihrauch
Pubblicato in: 33rd Annual AIAA/USU Conference on Small Satellites, 2019, Pagina/e SSC19-XII-07
Editore: 33rd Annual AIAA/USU Conference on Small Satellites

Thermal Control of High Power Applications on CubeSats

Autori: Janzer, Katja, Killian, Matthias, Langer, Martin, Krejci, David, Reissner, Alexander
Pubblicato in: 69th International Astronautical Congress (IAC), 2018, Pagina/e IAC-18-C2.7.11
Editore: 69th International Astronautical Congress (IAC)

CLIMB Exploration of the Van Allen Belt by CubeSats

Autori: Weimer, Bryan, Scharlemann, Carsten, David; Reissner, Alexander, Seifert, Bernhard
Pubblicato in: 36th International Electric Propulsion Conference, 2019, Pagina/e IEPC-2019-805
Editore: 36th International Electric Propulsion Conference

Monographic books (1)

Propulsion Systems

Autori: Flavia Tata Nardini, Michele Coletti, Alexander Reissner, David Krejci
Pubblicato in: 2017, ISBN 978-1-119-04203-7
Editore: Wiley

Diritti di proprietà intellettuale

Patent (1)

ION THRUSTER FOR THRUST VECTORED PROPULSION OF A SPACECRAFT

Numero candidatura/pubblicazione: 18 187104
Data: 2018-08-02
Candidato/i: ENPULSION GmbH

Trademark (1)

Word mark “ENPULSION”

Numero candidatura/pubblicazione: 018 022930
Data: 2019-06-21
Candidato/i: ENPULSION GmbH

Other (1)

Ionenemitter

Numero candidatura/pubblicazione: PCT AT2018/060159
Data: 2018-07-24
Candidato/i: ENPULSION GmbH

Registered design (1)

Bildmarke – “Raumschiffantrieb im Hexagon”

Numero candidatura/pubblicazione: 017 948516
Data: 2019-02-25
Candidato/i: ENPULSION GmbH