| Autor: |
Bobylev, A. V., Dyad'kin, A. A., Kobzev, V. I., Poedinok, V. M., Reshetin, A. G., Suprunenko, S. N., Jaroshevskii, V. A. |
| Předmět: |
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| Zdroj: |
Cosmic Research; Jan2008, Vol. 46 Issue 1, p74-89, 16p, 2 Diagrams, 2 Charts, 13 Graphs |
| Abstrakt: |
We consider the problems of control of the angular and trajectory motion of the Kliper re-entry vehicle. This spacecraft with a moderate hypersonic lift-to-drag ratio is designed according to the load-carrying frame scheme. Gas-dynamic engines, a split balancing flap, and an air brake are used as mounting devices of control. [ABSTRACT FROM AUTHOR] |
| Databáze: |
Complementary Index |
| Externí odkaz: |
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