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The first 3U CubeSat to study satellite re-entry

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EntrySat testing activities

D 14 November 2014    

In June 2014, EntrySat thermal and mechanical models we re tested in thermal vaccum Chamber at IRAP, and ICA vibration falicity.

EntrySat thermal model tested in thermal vaccum chamber at IRAP laboratory.

EntrySat mechanical model tested in vibrations at DMSM/ICA vibration facility.

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EntrySat description The Low Earth Orbit is getting more and more crowded with space debris. Objects at LEO experience a natural decay (...)

Friday 14 November 2014