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Guidance On Strength, Fatigue, and Fracture Control Requirements for Additively Manufactured Spaceflight Hardware

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Organization that Developed the Standard
Organization that Developed the Standard
NASA Standard
Document Identifiers
Document Number
NASA-HDBK-5026
Version
Baseline
Change Number
0
Document Date
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ACTIVE
NASA Organization and Technical Discipline
Responsible NASA Organization
NASA HQ, Office, Facility or Division
NASA HQ Office, Facility or Division
OCE - Office of the Chief Engineer
Technical Discipline Category
5000 - Structures/Mechanical Systems, Fluid Dynamics, Thermal, Propulsion, Aerodynamics
Endorsed Standard
Endorsement Details
NASA Core Standard
No
NASA Endorsed Standard Status
Not NASA Endorsed
Mandatory Standard
NASA Mandatory Standard
Not a NASA Mandatory Standard
Document Scope
Document Scope
This NASA Technical Handbook provides guidance on implementation of NASA requirements for Additively Manufactured (AM) spaceflight hardware in the areas of strength, fatigue, and fracture control. AM hardware owners should consider all requirements in these areas contained in NASA-STD-5001, Structural Design and Test Factors of Safety for Spaceflight Hardware, NASA-STD-5009, Nondestructive Evaluation Requirements for Fracture Critical (FC) Metallic Components, NASA-STD-5012, Strength and Life Assessment Requirements for Liquid-Fueled Space Propulsion System Engines, and NASA-STD-5019, Fracture Control Requirements for Spaceflight Hardware.
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NASA-HDBK-5026-Final-8-12-2024.pdf (3.13 MB)
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