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Re-Certification and Equivalency Test Results for IM7/8552-1 Following Extended Freezer Storage
In 2015, the Composites for Exploration Upper Stage (CEUS) Project established an equivalency test program to reduce the scope of laminate coupon tests within the project. The material selected was IM7/8552-1, a variant of the IM7/8552 prepreg used to populate a National Center for Advanced Materials Performance (NCAMP) database. The CEUS successor program, Composites Technology for Exploration (CTE), kicked off in 2017 with the remaining CEUS prepreg planned for use. The IM7/8552-1 prepreg was recertified through an in-house defined set of pass/fail criteria then evaluated for equivalency to the NCAMP database. Over the course of recertification and equivalency panel fabrication, the time of freezer storage ranged from 19-23 months. Panels for recertification and equivalency tests were fiber placed at NASA Marshall Space Flight Center (MSFC) and NASA Langley Research Center (LARC).
Forward Considerations in Methodologies for Qualification and Certification of Additively Manufactured Parts
No abstract available
Qualification & Certification of Additively Manufactured Parts for NASA Applications
No abstract available
Analyses of Kennedy Space Center Tropospheric Doppler Radar Wind Profiler Data for Space Launch System Program Certification
No abstract available
A Framework to Establish Additive Manufacturing Certification
No abstract available
Certification Coordination Roadmap
Innovative technology has to prove itself in the context of legacy regulations. The knowledgeable technologist must engage standards process and regulating authorities to understand their roles and to advise the effect of new technology, and with manufacturers to demonstrate technology benefit. A model for Innovative Technology Environment relating NASA to industry, standards and regulation is described. The needs of the standards community of the X-57 are identified, and a NASA standards structure is described. No NASA project works with standards and regulatory organizations like the X-57.
Developments and Challenges Related to Thermal Process Modeling of Metallic Laser Powder Bed Fusion to Advance Certification of Flight Hardware
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Developments and Challenges Related to Thermal Process Modeling of Metallic Laser Powder Bed Fusion to Advance Certification of Flight Hardware
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Thermal Process Modeling of Metallic Laser Powder Bed Fusion to Advance Certification of Flight Hardware
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NASA's Philosophy for the Qualification and Certification of Additively Manufactured Components
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Next Generation Durability and DamageTolerance to Support Certification of Flight Hardware
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NASA Activities and Perspectives on Standardization in the AM Certification Process: NASA-STD-6030 and Beyond
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Computational Materials for Qualification and Certification of Additively
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Qualification and Certification Strategies for Additive Manufactured Parts for Manned Spaceflight
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A Summary of NASA’s Efforts for the Development of and Certification and Qualification of Additively Manufactured Hardware
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Qualification and Certification Strategies for Additive Manufactured Parts for Manned Spaceflight
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