NASA-HDBK-5026:2024
Current
Current
The latest, up-to-date edition.
GUIDANCE ON STRENGTH, FATIGUE, AND FRACTURE CONTROL REQUIREMENTS FOR ADDITIVELY MANUFACTURED SPACEFLIGHT HARDWARE
Available format(s)
Hardcopy , PDF
Language(s)
English
Published date
12-08-2024
Important note : Users cannot be edited or removed once added to your Multi user PDF.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 |
| 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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