Name | E.T.PACK DMM & EEM (Electrodynamic Tether technology for PAssive Consumable-less deorbit Kit, E.T.PACK-F) |
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Type | CubeSat |
Units or mass | 12U |
Status | not launched, expected in 2025 |
Organisation | Universidad Carlos III de Madrid |
Institution | University |
Entity | Academic / Education |
Nation | Spain |
Manufacturer | AIVT by ? |
Operator | ? |
Costs | €5.5M |
Oneliner |
Develop a deorbit device based on 500m electrodynamic tether. |
Description |
The E.T.PACK deorbit device has been designed to fit into a standard 12U envelope, with a maximum mass of 24 kg. It is composed of two modules: the Deployment Mechanism Module (DMM), with an approximated dimension of 2U x 2U x 1.5U, and the Electron Emitter Module (EEM), with 2U x 2U x 2.5U of rough size, see Figure |
Sources | [1] [2] |
Photo Sources | [1] |
Keywords | Propulsion |
Last modified: 2022-12-29
Detailed E.T.PACK DMM & EEM entry in the Database
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