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...
| Main Authors: | , , , |
|---|---|
| Format: | Article |
| Language: | English |
| Published: |
NAS of Ukraine, A. Pidhornyi Institute of Mechanical Engineering Problems
2020-09-01
|
| Series: | Journal of Mechanical Engineering |
| Subjects: | |
| Online Access: | https://journal-me.com/wp-content/uploads/2020/10/2020_3_3_eng.pdf |