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Miniature free-space electrostatic ion thrusters
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Hartley, Frank T. Stephens, James B. |
| Copyright Year | 2006 |
| Description | A miniature electrostatic ion thruster is proposed for maneuvering small spacecraft. In a thruster based on this concept, one or more propellant gases would be introduced into an ionizer based on the same principles as those of the device described in an earlier article, "Miniature Bipolar Electrostatic Ion Thruster". On the front side, positive ions leaving an ionizer element would be accelerated to high momentum by an electric field between the ionizer and an accelerator grid around the periphery of the concave laminate structure. On the front side, electrons leaving an ionizer element would be ejected into free space by a smaller accelerating field. The equality of the ion and electron currents would eliminate the need for an additional electron- or ion-emitting device to keep the spacecraft charge-neutral. In a thruster design consisting of multiple membrane ionizers in a thin laminate structure with a peripheral accelerator grid, the direction of thrust could then be controlled (without need for moving parts in the thruster) by regulating the supply of gas to specific ionizer. |
| File Size | 64634 |
| Page Count | 1 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_20110014141 |
| Archival Resource Key | ark:/13960/t2s51n20b |
| Language | English |
| Publisher Date | 2006-11-01 |
| Access Restriction | Open |
| Subject Keyword | Spacecraft Propulsion And Power Ion Engines Ionizers Microsatellites Thrustors Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
