The GIESEPP MP project, co-funded by the European Union under the Horizon 2020 programme, is set to conclude in December 2024.
Continue readingFinal webinar: Mission accomplished on 20.11.2024
The GIESEPP MP consortium, co-funded by the EU Horizon 2020 programme, is hosting its final webinar on November 20 at 17:00 CET via Webex….
Continue readingFinal testing campaign for GIESEPP MP at Aerospazio premises, Italy
The Horizon 2020 project GIESEPP MP has reached a significant milestone with the completion of its final testing phase, known as the EPS…
Continue readingInterview with Javier Torres: An inside look at Airbus Crisa’s role in GIESEPP MP
Javier Torres is technical manager at Airbus Crisa and his main role is to supervise and coordinate all engineering tasks during..
Continue readingPlume diagnostics
In the frame of the GIESEPP MP project the Aerospazio activity will also be aimed at the demonstration and validation of advanced diagnostics, including laser spectroscopy techniques for not intrusive plasma property measurements of the plume of the thrusters.
Continue readingGIESEPP MP tests at Justus Liebig University Giessen, Germany
In February 2024, the Jumbo vacuum test facility at Justus Liebig University Giessen, Germany, hosted the GIESEPP MP measurement campaign..
Continue readingAerospazio test facility
The LVTF-3 is the test facility, located in Italy where Aerospazio will perform the testing activities foreseen in the frame of the GIESEPP-MP project.
Continue readingHorizon 2020 project GIESEPP MP: Brief Results now published on Cordis
Space industry leaders will engage with innovative SMEs and start-ups to establish new collaborations
In an era of extraordinary opportunities within the space sector, the European Union’s Horizon Europe program has opened doors for innovative, forward-thinking businesses, particularly start-ups and SMEs in Europe.
Continue readingElectric Space Propulsion and the RIT technology
Electric propulsion (EP) has become the standard for commercial geostationary satellites due to its high specific thrust, resulting in significant savings in propellant mass.
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