| Name | ECE3SAT |
|---|---|
| Type | CubeSat |
| Units or mass | 1U |
| Status | cancelled |
| Organisation | ECE Paris |
| Institution | University |
| Entity | 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
Detailed ECE3SAT entry in the Database
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Created by Erik Kulu
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