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Opendata, web and dolomites

MHT

Development of an innovative Mini Helicon Thruster (MHT) thruster suitable for small satellites

Total Cost €

EC-Contrib. €

Partnership

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Outcomes and
results

MHT project word cloud

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

contact market performances deeper satellites identification strategy checking definition customer platform micro realized platforms showing evaluation ten thrust thruster continued risk disruptive contingency outcome environment overview plan protection propulsion space cross innovative ip suppliers refinement supply perspective innovation competitors padua chain business mini helicon university proven started small strength industrialization

Project "MHT" data sheet

The following table provides information about the project.

Coordinator	TECHNOLOGY FOR PROPULSION AND INNOVATION SRL Organization address address: VIA ALTINATE 125 city: PADOVA postcode: 35121 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	Italy [IT]
Project website	http://www.t4innovation.com
Total cost	71˙429 €
EC max contribution	50˙000 € (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-1-2016-2017
Funding Scheme	SME-1
Starting year	2017
Duration (year-month-day)	from 2017-08-01 to 2018-01-31

Partnership

Take a look of project's partnership.

#	participants	country	role	EC contrib. [€]
1	TECHNOLOGY FOR PROPULSION AND INNOVATION SRL TECHNOLOGY FOR PROPULSION AND INNOVATION SRL Organization address address: VIA ALTINATE 125 city: PADOVA postcode: 35121 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.	IT (PADOVA)	coordinator	50˙000.00

Map

Project objective

This work presents a phase 1 proposal on the development of an innovative propulsion system specifically studied and developed for mini and micro platform. The mini helicon thruster proposed is the outcome of more than ten years of a research started at University of Padua and continued within Technology for propulsion and innovation. The technology has been proven on a relevant environment with thrust measurements showing performances within the target range of mini and micro platforms. After a wide overview of competitors and market perspective it has been realized that this technology may have a disruptive impact on the future space market of small satellites. In this proposal a refinement of the business plan is proposed through the following key activities: better identification of market requirements by detailed contact with potential customer, deeper evaluation of competitors’ strength cross checking their performances with customer needs, identification of supply chain, definition of development plan, suppliers, industrialization plan, risk assessment and contingency plan, development of market plan and IP protection strategy.

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The information about "MHT" are provided by the European Opendata Portal: CORDIS opendata.