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Electrodynamic tether (Document No: 19850025855)
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Roberts, W. T. |
| Copyright Year | 1985 |
| Description | The electrodynamic tether consists of a satellite deployed to a distance of 20 km by an electrically conducting tether. The space station hardware consists of a 12 meter deployment boom, satellite cradle, tether reel and motor, and other tether support systems. The electrodynamic tether will be used to perform a variety of wave experiments by exciting a wide spectrum of low frequency waves in the ionospheric plasma. The system can also be used to artificially generate and study field aligned currents and associated plasma effects. Hydromagnetic waves generated by the passage of the system through the space plasma are of particular interest in space plasma research. |
| File Size | 58481 |
| Page Count | 1 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19850025855 |
| Archival Resource Key | ark:/13960/t52g2m76v |
| Language | English |
| Publisher Date | 1985-01-01 |
| Access Restriction | Open |
| Subject Keyword | Spacecraft Design, Testing And Performance Field Aligned Currents Plasmas Physics Booms Equipment Space Shuttle Payloads Earth Ionosphere Tethered Satellites Electrohydrodynamics Space Stations Solar Observatories Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |