Methods to Reduce Material Intensity of Tail Sections of Launch Vehicles
A technique has been developed for reducing the material intensity of highly stressed tail sections of launch vehicles, taking into account strength and stability constraints as well as technological requirements. A cylindrical longitudinally and transversely ribbed waffle-grid (lattice) shell with...
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| Datum: | 2020 |
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| Hauptverfasser: | , , , |
| Format: | Artikel |
| Sprache: | English Russian |
| Veröffentlicht: |
Інститут енергетичних машин і систем ім. А. М. Підгорного Національної академії наук України
2020
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| Schlagworte: | |
| Online Zugang: | https://journals.uran.ua/jme/article/view/213127 |
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| Назва журналу: | Energy Technologies & Resource Saving |