Methods to Reduce Material Intensity of Tail Sections of Launch Vehicles

• 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
• 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...