| Article ID | Journal | Published Year | Pages | File Type |
|---|---|---|---|---|
| 1717379 | Acta Astronautica | 2006 | 9 Pages |
Abstract
As third part, in order to test the model and its analysis and synthesis capabilities, we implement a software tool that helps the designer in the rapid tuning of the fundamental quantities for the optimization of the performance: the proposed model shows an optimum agreement with the results of the simulations.
Related Topics
Physical Sciences and Engineering
Engineering
Aerospace Engineering
Authors
Guido Sterbini,