Abstract
Cracks of all types are extremely dangerous for structures; this fact is critically unacceptable in the rocket and space industry. Aluminum-lithium alloys have a perfect set of mechanical, operational and corrosion characteristics that allow them to compete with traditional alloys and even polymer composite materials. The main focus of scientific research was the analysis of crack formation when combining two successive methods of heating samples of the promising rocket and space industry alloy 1420: discrete isothermal scanning and continuous program heating. The relationship between such factors as the average elongation of cracks in the sample, the number of cracks in the sample, changes in the area of the sample relative to the degree of compression of the material, the heating temperature of the sample, the exposure time in the furnace, the number of rolling passes, and rolling speed were revealed in the paper.
Sign-in/Register to access full text options 
Talk to us
Join us for a 30 min session where you can share your feedback and ask us any queries you have
Schedule a callMore From: IOP Conference Series: Materials Science and Engineering
Disclaimer: All third-party content on this website/platform is and will remain the property of their respective owners and is provided on "as is" basis without any warranties, express or implied. Use of third-party content does not indicate any affiliation, sponsorship with or endorsement by them. Any references to third-party content is to identify the corresponding services and shall be considered fair use under The CopyrightLaw.
