Abstract
Interplanetary missions with ion propulsion are simulated and evaluated, using a general approach, that has been presented at the 14th ISTS. Specific problems, such as the power generation and the optimization of the specific impulse are discussed.
| Original language | English |
|---|---|
| Pages | 333-337 |
| Number of pages | 5 |
| State | Published - 1984 |
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