NASA STD 5006 : 2015
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
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GENERAL FUSION WELDING REQUIREMENTS FOR AEROSPACE MATERIALS
01-01-2015
16-08-2022
DOCUMENT HISTORY LOG
FOREWORD
1. SCOPE
2. APPLICABLE DOCUMENTS
3. ACRONYMS AND DEFINITIONS
4. REQUIREMENTS
APPENDIX A - GUIDANCE
APPENDIX B - REQUIREMENTS COMPLIANCE MATRIX
Sets up the processing and quality assurance requirements for manual, automatic, machine, and semiautomatic welding for spaceflight applications and special test equipment used for testing flight hardware with the exception of ground-based pressure systems, which are subjected to NASA-STD-8719.17, NASA Requirements for Ground-Based Pressure Vessels and Pressurized Systems (PVS).
| DocumentType |
Standard
|
| PublisherName |
National Aeronautics and Space Administration
|
| Status |
Superseded
|
| SupersededBy | |
| Supersedes |
| NASA MSFC SPEC 3679 : 2012 | PROCESS SPECIFICATION - WELDING AEROSPACE HARDWARE |
| NASA STD 6016(INT) : 2006 | STANDARD MATERIALS AND PROCESSES REQUIREMENTS FOR SPACECRAFT |
| NASA PRC 0015 : 2016 | PROCESS SPECIFICATION FOR AUTOMATIC AND MACHINE ARC WELDING OF TITANIUM AND TITANIUM ALLOY HARDWARE |
| NASA STD 6016 : 2016 | STANDARD MATERIALS AND PROCESSES REQUIREMENTS FOR SPACECRAFT |
| NASA STD 8719.24 : 2011 | NASA EXPENDABLE LAUNCH VEHICLE PAYLOAD SAFETY REQUIREMENTS |
| NASA PRC 0002 : 2012 | PROCESS SPECIFICATION FOR THE MANUAL ARC WELDING OF TITANIUM ALLOY HARDWARE |
| NASA JSC 27301 : 2009 | MATERIALS AND PROCESSES SELECTION, CONTROL, AND IMPLEMENTATION PLAN FOR JSC FLIGHT HARDWARE |
| MIL-HDBK-1823 Revision A:2009 | Nondestructive Evaluation System Reliability Assessment |
| MIL-PRF-27407 Revision D:2014 | Propellant Pressurizing Agent, Helium |
| BB-O-925 Revision A:1961 | Oxygen, Technical, Gas and Liquid (S/S by CGA-G4) |
| SAE AMS2770M | Heat Treatment of Wrought Aluminum Alloy Parts |
| MIL A 18455 : C | ARGON, TECHNICAL |
| NASA STD 5001 : 2014 | STRUCTURAL DESIGN AND TEST FACTORS OF SAFETY FOR SPACEFLIGHT HARDWARE |
| ASME B46.1 : 2009 | SURFACE TEXTURE (SURFACE ROUGHNESS, WAVINESS, AND LAY) |
| BB-H-886 Revision E:2011 | Hydrogen |
| MIL-STD-1537 Revision C:2002 | Electrical Conductivity Test for Verification of Heat Treatment of Aluminum Alloys, Eddy Current Method |
| MIL-STD-2154 Base Document:1982 | Inspection, Ultrasonic, Wrought Metals, Process for (S/S by ASTM-E2375 and SAE-AMS-STD-2154) |
| MIL-STD-2219 Revision A:2005 | Fusion Welding for Aerospace Applications (S/S by AWS-D17.1) |
| NASA STD 5019 : 2016 | FRACTURE CONTROL REQUIREMENTS FOR SPACEFLIGHT HARDWARE |
| BB-C-101 Revision D:2011 | Carbon Dioxide (CO2): Technical and USP |
| NASA-STD-8719.17C:2017 | NASA REQUIREMENTS FOR GROUND-BASED PRESSURE VESSELS AND PRESSURIZED SYSTEMS (PVS) |
| SAE AMSH81200D | Heat Treatment of Titanium and Titanium Alloys |
| ASTM E 2375 : 2016 : REDLINE | Standard Practice for Ultrasonic Testing of Wrought Products |
| MIL-PRF-27401 Revision G:2013 | Propellant Pressurizing Agent, Nitrogen |
| NASA MSFC SPEC 3679 : 2012 | PROCESS SPECIFICATION - WELDING AEROSPACE HARDWARE |
| NASA STD 6016 : 2016 | STANDARD MATERIALS AND PROCESSES REQUIREMENTS FOR SPACECRAFT |
| 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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