NASA MSFC STD 3716 : 2017
Current
The latest, up-to-date edition.
STANDARD FOR ADDITIVELY MANUFACTURED SPACEFLIGHT HARDWARE BY LASER POWDER BED FUSION IN METALS
Hardcopy , PDF
English
18-10-2017
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1. SCOPE
2. APPLICABLE DOCUMENTS
3. ACRONYMS, ABBREVIATIONS, SYMBOLS, AND DEFINITIONS
4. GENERAL REQUIREMENTS
5. FOUNDATIONAL PROCESS CONTROL REQUIREMENTS
6. PART DESIGN AND PRODUCTION CONTROL REQUIREMENTS
7. ESTABLISHING L-PBF MATERIAL PROPERTY DESIGN VALUES
APPENDICES
A - PART PRODUCTION PLAN CONTENT
B - EXTENDED COMMENTARY
C - DEVELOPMENT AND USE OF THE MPS AND PCRD
D - THE CRYPTOGRAPHIC HASH
E - REFERENCE DOCUMENTS
F - REQUIREMENTS SUMMARY TABLE
This MSFC Technical Standard provides a framework for the implementation of Laser-Powder Bed Fusion (L-PBF) Additive Manufacturing (AM) parts into spaceflight applications requiring high reliability.
| DocumentType |
Standard
|
| Pages |
93
|
| PublisherName |
National Aeronautics and Space Administration
|
| Status |
Current
|
| NASA MSFC SPEC 3717 : 2017 | SPECIFICATION FOR CONTROL AND QUALIFICATION OF LASER POWDER BED FUSION METALLURGICAL PROCESSES |
| SAE AS 9102 : 2014 | AEROSPACE FIRST ARTICLE INSPECTION REQUIREMENT |
| SAE AMS 2175 : 2010 | CASTINGS, CLASSIFICATION AND INSPECTION OF |
| NASA MSFC SPEC 3717 : 2017 | SPECIFICATION FOR CONTROL AND QUALIFICATION OF LASER POWDER BED FUSION METALLURGICAL PROCESSES |
| ISO/ASTM 52921:2013 | Standard terminology for additive manufacturing — Coordinate systems and test methodologies |
| ASTM E 466 : 2015 : REDLINE | Standard Practice for Conducting Force Controlled Constant Amplitude Axial Fatigue Tests of Metallic Materials |
| NASA STD 5001 : 2014 | STRUCTURAL DESIGN AND TEST FACTORS OF SAFETY FOR SPACEFLIGHT HARDWARE |
| NASA JSC 65828 : 2011 | STRUCTURAL DESIGN REQUIREMENTS AND FACTORS OF SAFETY FOR SPACEFLIGHT HARDWARE |
| ASTM E 606/E606M : 2012 : REDLINE | Standard Test Method for Strain-Controlled Fatigue Testing |
| NASA STD 5017 : 2015 | DESIGN AND DEVELOPMENT REQUIREMENTS FOR MECHANISMS |
| SAE AS 9100D : 2016 | QUALITY MANAGEMENT SYSTEMS - REQUIREMENTS FOR AVIATION, SPACE AND DEFENSE ORGANIZATIONS |
| ASTM E 2281 : 2015 : REDLINE | Standard Practice for Process Capability and Performance Measurement |
| ASTM E 2587 : 2016 : REDLINE | Standard Practice for Use of Control Charts in Statistical Process Control |
| NASA STD 5019 : 2016 | FRACTURE CONTROL REQUIREMENTS FOR SPACEFLIGHT HARDWARE |
| IEST STD CC1246 : 2013 | PRODUCT CLEANLINESS LEVELS - APPLICATIONS, REQUIREMENTS, AND DETERMINATION |
| NASA STD 5012 : 2016 | STRENGTH AND LIFE ASSESSMENT REQUIREMENTS FOR LIQUID-FUELED SPACE PROPULSION SYSTEM ENGINES |
| NASA STD 6016 : 2016 | STANDARD MATERIALS AND PROCESSES REQUIREMENTS FOR SPACECRAFT |
| FIPS PUB 180 : 2002 | SECURE HASH STANDARD |
| NASA MSFC SPEC 164 : 2010 | CLEANLINESS OF COMPONENTS FOR USE IN OXYGEN, FUEL, AND PNEUMATIC SYSTEMS, SPECIFICATION FOR |
| ASTM E 8/E8M : 2016-09 | TEST METHODS FOR TENSION TESTING OF METALLIC MATERIALS |
| NASA STD 5009 : 2008 | NONDESTRUCTIVE EVALUATION REQUIREMENTS FOR FRACTURE-CRITICAL METALLIC COMPONENTS - MEASUREMENT SYSTEM IDENTIFICATION: METRIC (INCH-POUND) |
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