Methods to Reduce Material Intensity of Tail Sections of Launch Vehicles
Saved in:
| Date: | 2020 |
|---|---|
| Main Authors: | M. O. Dehtiarov, A. P. Dziuba, K. V. Avramov, V. M. Sirenko |
| Format: | Article |
| Language: | English |
| Published: |
2020
|
| Series: | Journal of mechanical engineering |
| Online Access: | http://jnas.nbuv.gov.ua/article/UJRN-0001159852 |
| Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
| Journal Title: | Library portal of National Academy of Sciences of Ukraine | LibNAS |
Institution
Library portal of National Academy of Sciences of Ukraine | LibNASSimilar Items
-
Methods to Reduce Material Intensity of Tail Sections of Launch Vehicles
by: Dehtiarov, Maksym O., et al.
Published: (2020) -
Methods to Reduce Material Intensity of Tail Sections of Launch Vehicles
by: Dehtiarov, Maksym O., et al.
Published: (2020) -
Flexural-flexural-longitudinal transients of launch vehicle
by: K. V. Avramov, et al.
Published: (2011) -
Strength of Composite Transport and Launch Container for Rocket Launch
by: K. V. Avramov, et al.
Published: (2023) -
Flexural-flexural-longitudinal transients of launch vehicle
by: Аврамов, К. В., et al.
Published: (2016)