Explore the words cloud of the MINOTOR project. It provides you a very rough idea of what is the project "MINOTOR" about.
The following table provides information about the project.
Coordinator |
OFFICE NATIONAL D'ETUDES ET DE RECHERCHES AEROSPATIALES
Organization address contact info |
Coordinator Country | France [FR] |
Project website | http://www.minotor-project.eu |
Total cost | 1˙485˙809 € |
EC max contribution | 1˙485˙809 € (100%) |
Programme |
1. H2020-EU.2.1.6.1. (Enabling European competitiveness, non-dependence and innovation of the European space sector) 2. H2020-EU.2.1.6.2. (Enabling advances in space technology) 3. H2020-EU.2.1.6.1.1. (Safeguard and further develop a competitive, sustainable and entrepreneurial space industry and research community and strengthen European non-dependence in space systems) |
Code Call | H2020-COMPET-2016 |
Funding Scheme | RIA |
Starting year | 2017 |
Duration (year-month-day) | from 2017-01-01 to 2020-04-30 |
Take a look of project's partnership.
# | ||||
---|---|---|---|---|
1 | OFFICE NATIONAL D'ETUDES ET DE RECHERCHES AEROSPATIALES | FR (PALAISEAU) | coordinator | 599˙065.00 |
2 | UNIVERSIDAD CARLOS III DE MADRID | ES (GETAFE (MADRID)) | participant | 310˙481.00 |
3 | JUSTUS-LIEBIG-UNIVERSITAET GIESSEN | DE (GIESSEN) | participant | 153˙750.00 |
4 | THALES MICROELECTRONICS SAS | FR (ETRELLES) | participant | 150˙271.00 |
5 | THALES ALENIA SPACE BELGIUM S.A. | BE (MONT SUR MARCHIENNE) | participant | 115˙058.00 |
6 | L - UP SAS | FR (PARIS) | participant | 86˙907.00 |
7 | SAFRAN AIRCRAFT ENGINES | FR (PARIS) | participant | 70˙276.00 |
MINOTOR’s strategic objective is to demonstrate the feasibility of the ECRA technology as a disruptive game-changer in electric propulsion, and to prepare roadmaps paving the way for the 2nd EPIC call, in close alignment with the overall SRC-EPIC strategy. Based on electron cyclotron resonance (ECR) as the sole ionization and acceleration process, ECRA is a cathodeless thruster with magnetic nozzle, allowing thrust vectoring. It has a considerable advantage in terms of global system cost, where a reduction of at least a factor of 2 is expected, and reliability compared to mature technologies. It is also scalable and can potentially be considered for all electric propulsion applications, from microsatellites to space tugs. Although the first results obtained with ECRA have been encouraging, the complexity of the physics at play has been an obstacle for the understanding and development of the technology. Thus an in-depth numerical and experimental investigation plan has been devised for the project, in order to bring the technology from TRL3 to TRL5. The strong consortium is composed of academic experts to perform the research activities on ECRA, including alternative propellants, along with experienced industrial partners to quantify its disruptive advantages on the propulsion subsystem and its market positioning. ECRA’s advantages as an electric thruster technology can be a disruptive force in a mostly cost-driven satellite market. It would increase European competitiveness, help develop low-cost satellite missions such as constellations, provide end-of-life propulsion, and pave the way for future emerging electric propulsion technologies. The 36 months MINOTOR project requests a total EC grant of 1 485 809 M€ for an experienced consortium of 7 partners from 4 countries: ONERA (FR, Coordinator), industries Thales Alenia Space (BE), Thales Microelectronics (FR), SNECMA (FR), Universities Carlos III (ES) and Giessen (GE), and SME L-up (FR).
year | authors and title | journal | last update |
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2017 |
T. Vialis, J. Jarrige, D. Packan Geometry optimization and effect of gas propellant in an electron cyclotron resonance plasma thruster published pages: , ISSN: , DOI: |
The 35th International Electric Propulsion Conference IEPC-2017-378, 08/10/2017 | 2020-01-20 |
2017 |
J. Jarrige; S. Correyero, PQ. Elias, D. Packan Investigation on the ion velocity distribution in the magnetic nozzle of an ECR plasma thruster using LIF measurements published pages: , ISSN: , DOI: |
The 35th International Electric Propulsion Conference IEPC-2017-382, 08/10/2017 | 2020-01-20 |
2017 |
S. Correyero, J. Jarrige, D. Packan, E. Ahedo Measurement of anisotropic plasma properties along the magnetic nozzle expansion of an Electron Cyclotron Resonance Thruster published pages: , ISSN: , DOI: |
The 35th International Electric Propulsion Conference IEPC-2017-437, 08/10/2017 | 2020-01-20 |
2017 |
PQ. Elias Advances in the kinetic simulation of microwave absorption in an ECR thruster published pages: , ISSN: , DOI: |
The 35th International Electric Propulsion Conference IEPC-2017-361, 08/10/2017 | 2020-01-20 |
2017 |
Mario Merino, Alvaro Sanchez-Villar, Eduardo Ahedo, Paul Bonoli, Jungpyo Lee, Abhay Ram and John Wright Wave Propagation and Absorption in ECR Plasma thrusters published pages: , ISSN: , DOI: |
The 35th International Electric Propulsion Conference IEPC-2017-105, 09/10/2017 | 2020-01-20 |
2017 |
M.Wijnen, S.Correyero-Plaza, N.Aguera-Lopez, D.Perez-Grande Innovative Electric Propulsion trends, concurrent mission design and enabling technologies for a bold CubeSat Lunar Positioning published pages: , ISSN: , DOI: |
The 35th International Electric Propulsion Conference Winner of Young Visionary paper | 2020-01-20 |
2017 |
G. Sanchez-Arriaga, J. Zhou, E. Ahedo, M. MartÃnez-Sánchez, J.J. Ramos One-dimensional Direct Vlasov Simulations of Non-stationary Plasma Expansion in Magnetic Nozzle published pages: , ISSN: , DOI: |
The 35th International Electric Propulsion Conference IEPC-2017-106 (partial funding) | 2020-01-20 |
2017 |
D, Packan The “MINOTOR†H2020 project for ECR thruster development published pages: , ISSN: , DOI: |
The 35th International Electric Propulsion Conference IEPC-2017-547, 08/10/2017 | 2020-01-20 |
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