| Name | MiTEE-2 (MiTEE-B, Miniature Tether Electrodynamics Experiment) |
|---|---|
| Type | CubeSat |
| Units or mass | 3U |
| Status | not launched, expected in 2020 |
| Organisation | University |
| Organisation | University of Michigan |
| Nation | US |
| Oneliner | Assess the feasibility of using miniature electrodynamic (ED) tethers in space as means to provide “propellantless”. |
| Keywords | Tether, Propulsion |
Last modified: 2020-01-06
Detailed MiTEE-2 entry in the Database
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