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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| Date: | 2020 |
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| Main Authors: | , , , |
| Format: | Article |
| Language: | English Russian |
| Published: |
Інститут енергетичних машин і систем ім. А. М. Підгорного Національної академії наук України
2020
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| Subjects: | |
| Online Access: | https://journals.uran.ua/jme/article/view/213127 |
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| Journal Title: | Journal of Mechanical Engineering |