NASA Technical Reports Server (NTRS) 20160008035: Advanced Near Net Shape Technology George C. Marshall Space Flight Center Research And Technology Report 2014 - Info and Reading Options
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"NASA Technical Reports Server (NTRS) 20160008035: Advanced Near Net Shape Technology George C. Marshall Space Flight Center Research And Technology Report 2014" and the language of the book is English.
“NASA Technical Reports Server (NTRS) 20160008035: Advanced Near Net Shape Technology George C. Marshall Space Flight Center Research And Technology Report 2014” Metadata:
- Title: ➤ NASA Technical Reports Server (NTRS) 20160008035: Advanced Near Net Shape Technology George C. Marshall Space Flight Center Research And Technology Report 2014
- Author: ➤ NASA Technical Reports Server (NTRS)
- Language: English
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- Internet Archive ID: NASA_NTRS_Archive_20160008035
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"NASA Technical Reports Server (NTRS) 20160008035: Advanced Near Net Shape Technology George C. Marshall Space Flight Center Research And Technology Report 2014" Description:
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The objective of the Advanced Near Net Shape Technology (ANNST) project is to radically improve near net shape manufacturing methods from the current Technology/ Manufacturing Readiness Levels (TRL/MRL 3-4) to the point where they are viable candidates (TRL/ MRL-6) for shortening the time and cost for insertion of new aluminum alloys and revolutionary manufacturing methods into the development/improvement of space structures. Conventional cyrotank manufacturing processes require fabrication of multiple pieces welded together to form a complete tank. A variety of near net shape manufacturing processes has demonstrated excellent potential for enabling single-piece construction of components such as domes, barrels, and ring frames. Utilization of such processes can dramatically reduce the extent of welding and joining needed to construct cryogenic tanks and other aerospace structures. The specific focus of this project is to successfully mature the integrally stiffened cylinder (ISC) process in which a single-piece cylinder with integral stiffeners is formed in one spin/flow forming process. Structural launch vehicle components, like cryogenic fuel tanks (e.g., space shuttle external tank), are currently fabricated via multipiece assembly of parts produced through subtractive manufacturing techniques. Stiffened structural panels are heavily machined from thick plate, which results in excessive scrap rates. Multipiece construction requires welds to assemble the structure, which increases the risk for defects and catastrophic failures.
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- Added Date: 2021-01-12 19:18:00
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