ECE3SAT

ECE3SAT
Name ECE3SAT
Type CubeSat
Units or mass 1U
Status not launched, expected in 2020
Organisation University
Organisation ECE Paris
Nation France
Oneliner Verify a physical theory permitting a fast deorbiting.
Keywords De-orbit device

Last modified: 2019-07-07
Detailed ECE3SAT entry in the Database
Full Nanosats Database (much more data)

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Created by Erik Kulu

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