NASA-HDBK-5026:2024
Current
GUIDANCE ON STRENGTH, FATIGUE, AND FRACTURE CONTROL REQUIREMENTS FOR ADDITIVELY MANUFACTURED SPACEFLIGHT HARDWARE
English
08-12-2024
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.
| DocumentType |
Handbook
|
| Pages |
108
|
| PublisherName |
National Aeronautics and Space Administration
|
| Status |
Current
|
| AIAA S 080 : A2018 | SPACE SYSTEMS - METALLIC PRESSURE VESSELS, PRESSURIZED STRUCTURES, AND PRESSURE COMPONENTS |
| MIL-HDBK-1823 Revision A:2009 | Nondestructive Evaluation System Reliability Assessment |
| ASTM E 3166 : 2020 : EDT 1 | Standard Guide for Nondestructive Examination of Metal Additively Manufactured Aerospace Parts After Build |
| ASTM E 399 : 2023 | Standard Test Method for Linear-Elastic Plane-Strain Fracture Toughness of Metallic Materials |
| ASTM E 1820 : 2024 | Standard Test Method for Measurement of Fracture Toughness |
| ISO/ASTM 52900:2015 | Additive manufacturing — General principles — Terminology |
| ASTM E 1681 : 2023 | Standard Test Method for Determining Threshold Stress Intensity Factor for Environment-Assisted Cracking of Metallic Materials |
| ASTM E 1823 : 2024 : REV C | Standard Terminology Relating to Fatigue and Fracture Testing |
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