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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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Datum:	2020
Hauptverfasser:	Dehtiarov, Maksym O., Dziuba, Anatolii P., Avramov, Konstantin V., Sirenko, Volodymyr M.
Format:	Artikel
Sprache:	Englisch Russisch
Veröffentlicht:	Інститут енергетичних машин і систем ім. А. М. Підгорного Національної академії наук України 2020
Schlagworte:	launch vehicle tail section material consumption stress-strain state UDC 539.3
Online Zugang:	https://journals.uran.ua/jme/article/view/213127
Tags:	Tag hinzufügen Keine Tags, Fügen Sie den ersten Tag hinzu!
Назва журналу:	Journal of Mechanical Engineering

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Journal of Mechanical Engineering

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