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2006-02-06
Active Space Technologies acts as consultant for ESA's Education Office YES2 project

The Center of Expertise of the University of Patras, Greece (CoE Patras) is in charge of the mechanical and thermal subsystems of YES2. Active Space Technologies is consultant in the definition of the thermal interfaces with the Russian Foton M3, and in the thermal modelling and analysis.

The 2nd Young Engineers Satellite (YES2) is a project of the ESA Educational Office, where students from all over Europe develop an innovative re-entry technology by using space tethers instead of conventional propulsion methods. The YES2 Spacemail is trying to demonstrate a brand new method for payload transportation from Space to Earth and more specifically from the International Space Station (ISS) to Earth. The mission is planned to be launched in 2007 with the Russian scientific spacecraft FOTON-M3.

The goals of the project are:
  • to give students a motivating technological & educational experience;
  • to demonstrate SpaceMail: return a small capsule from space to Earth, using:
     • a 30 km 5 kg wire (tether) rather than a rocket engine, helping to open the way for new, advanced space        applications;
     • an ultra-light re-entry capsule demonstrating novel heatshield technologies and entering a new regime of        in-flight aerothermodynamics study.

The Russian Foton spacecraft was created as an interface for 0G experiments. It was designed and built by the Central Specialised Design Bureau of the State Research and Production Space Rocket Centre (TsSKB-Progress) and was first launched by a Soyuz-U launcher in 1985. The Foton spacecraft consists of the descent module, a battery pack, and an attitude and orbit control module.
The definition of the Foton-YES2 thermal interface and consequent thermal analysis are of utter importance for the success of the mission. While the design of YES2 spacecraft needs to enable the dissipation of the high heat fluxes during the mission, it has further to withstand ecclipse non-operation phases. At the same time the strict thermal interfaces to Foton and the structural design of YES2 have to be taken into consideration.
The role of
Active Space Technologies is to support YES2 CoE Patras in the trade-off analysis between meeting the interface requirements and delivering an overall good thermal performance of YES2.

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