The thrust generated by a T6 ion engine hollow cathode
The thrust produced by a T6 ion engine main discharge hollow cathode was characterized using different propellants with a target-based measurement system, for discharge current values of 5-25 A and a wide range of mass flow rates. The calculated values of specific impulse are far in excess of those...
| Main Authors: | , , |
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| Format: | Article |
| Language: | English |
| Published: |
2014-09.
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| Subjects: | |
| Online Access: | Get fulltext |