ECE3SAT
Spacecraft name ECE3SAT
Type CubeSat
Units or mass 1U
Status cancelled
Organisation ECE Paris
Institution University
Entity type Academic / Education
Nation France
Oneliner

Verify a physical theory permitting a fast deorbiting.

Sources [1]
Photo sources [1]
Keywords De-orbit device

Last modified: 2023-06-08

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Created by Erik Kulu

Email: erik.kulu@nanosats.eu
LinkedIn: linkedin.com/in/erikkulu

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