| Name | MiTEE-2 (MiTEE-B, Miniature Tether Electrodynamics Experiment) |
|---|---|
| Type | CubeSat |
| Units or mass | 3U |
| Mass in kg | 1.7 kg |
| Status | not launched, expected in 2020 |
| Organisation | University of Michigan |
| Institution | University |
| Entity | Academic / Education |
| Nation | US |
| Launch brokerer | NASA CSLI / ELaNa |
| Oneliner | Assess the feasibility of using miniature electrodynamic (ED) tethers in space as means to provide “propellantless”. |
| Sources | Link-1 |
| Keywords | Tether, Propulsion |
Last modified: 2020-03-26
Detailed MiTEE-2 entry in the Database
Full Nanosats Database (much more data)
