Methods to Reduce Material Intensity of Tail Sections of Launch Vehicles

• Дата: 2020
• Автори: Dehtiarov, Maksym O., Dziuba, Anatolii P., Avramov, Konstantin V., Sirenko, Volodymyr M.
• Формат: Стаття
• Мова: English; Russian
• Опубліковано: Journal of Mechanical Engineering 2020
• Теми: launch vehicle; tail section; material consumption; stress-strain state; UDC 539.3; ракета-носій; хвостовий відсік; матеріаломісткість; напружено-деформований стан; УДК 539.3; ракета-носитель; хвостовой отсек; материалоемкость; напряженно-деформированное состояние
• Онлайн доступ: https://journals.uran.ua/jme/article/view/213127
• Назва журналу: Journal of Mechanical Engineering

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...