Methods to Reduce Material Intensity of Tail Sections of Launch Vehicles

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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Bibliographic Details
Date:2020
Main Authors: Dehtiarov, Maksym O., Dziuba, Anatolii P., Avramov, Konstantin V., Sirenko, Volodymyr M.
Format: Article
Language:English
Russian
Published: Інститут енергетичних машин і систем ім. А. М. Підгорного Національної академії наук України 2020
Subjects:
launch vehicle
tail section
material consumption
stress-strain state
UDC 539.3
Online Access:https://journals.uran.ua/jme/article/view/213127
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Journal Title:Journal of Mechanical Engineering

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Journal of Mechanical Engineering

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https://journals.uran.ua/jme/article/view/213127

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