- Issue
- Journal of Siberian Federal University. Engineering & Technologies. 2016 9 (2)
- Authors
- Moskvichev, Egor V.
- Contact information
- Moskvichev, Egor V.:SDTB “Nauka” ICT SB RAS P.O. box 25515, Krasnoyarsk, 660049, Russia; E-mail:
- Keywords
- spacecraft; filament-wound pressure vessel; composite material; testing; mechanical properties
- Abstract
The results of the assessment of composite mechanical properties in a filament-wound pressure vessel are presented. The cutting diagram, the method of sample preparation and testing procedure are shown. The comparison of the elastic modulus determined on three-point bending tests and tensile tests was carried out
- Pages
- 246-253
- Paper at repository of SibFU
- https://elib.sfu-kras.ru/handle/2311/20229
This work is licensed under a Creative Commons Attribution-NonCommercial 4.0 International License (CC BY-NC 4.0).