SRC – In-Space electrical propulsion and station keeping

Call: 
SPACE 2018-2020
Referencia: 
SPACE-13-TEC-2019

disruptive electric propulsion technology is a technology that disrupts a status quo in the space sector. It could replace the dominant technology by providing radical improvements in performance or costs which are perceived as valuable by a customer or part of the market, or it opens up new opportunities not possible with the incumbent technology. Emerging technologies that are potentially ‘disruptive’ often underperform compared to the dominant technology in early development phases – the underlying physics may not be fully understood for example and more R&D is required to properly ascertain performance attributes. Examples can be: disruptive improvement of performances, enabling of new operational scenarios, reducing costs of the full system etc.

Proposals shall cover one of the following two subtopics:

  • Thruster concepts or technologies for disruptive electric propulsion systems such as Helicon Plasma Thrusters (HPT), Electron Cyclotron Resonance plasma thrusters (ECR), Magneto Plasma Dynamic thrusters (MPD), Pulsed Plasma Thrusters (PPT), micro-propulsion electric thrusters, or any other innovative electric thruster concepts and relevant technologies for disruptive electric propulsion systems.
  • Transversal concepts and technologies for disruptive electric propulsion systems, such as power condition electronics, direct drive, magnetic nozzles, alternative propellants, testing techniques, materials.

Proposals may target any part of the technology readiness levels (TRL) scale, in particular:

  • Breakthrough technologies starting at low or very low TRL (<4), aiming to promote promising and potentially disruptive thrusters concepts in the field of Electric Propulsion. This should allow increasing of the current TRL, which in the long term could change the Electric Propulsion landscape.
  • Promising technologies starting at higher TRL (≥4) in the field of Electric Propulsion, enabling significant improvements of Electric Propulsion system performances, cost and fit to the market. The objective here is to allow to efficiently and effectively increase the TRL. Proposal for higher TRL should include the best possible combination of a market analysis and an application impact analysis.

Proposals shall include a market analysis detailing the targeted applications and the specific key advantages of the proposed technology. Every disruptive effect shall be specifically correlated with its final application

 

 

Deadline: 
12/03/2019


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