NASA STD 5019 : 2016
Withdrawn
Withdrawn
FRACTURE CONTROL REQUIREMENTS FOR SPACEFLIGHT HARDWARE
Published date
02-01-2016
Withdrawn date
10-17-2019
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DOCUMENT HISTORY LOG
FOREWORD
1. SCOPE
2. APPLICABLE DOCUMENTS
3. ACRONYMS AND DEFINITIONS
4. GENERAL REQUIREMENTS
5. EXEMPT PARTS
6. ASSESSMENT OF NON-FRACTURE CRITICAL PARTS
7. ASSESSMENT OF FRACTURE CRITICAL PARTS
8. FLAW SCREENING, TRACEABILITY, AND MATERIAL
SELECTION
9. FRACTURE CONTROL DOCUMENTATION AND VERIFICATION
10. ALTERNATIVES
APPENDIX
A - Requirements Compliance Matrix
B - Reference Documents
The purpose of this NASA Technical Standard is to establish the fracture control requirements for National Aeronautics and Space Administration (NASA) human-rated spaceflight hardware.
| DevelopmentNote |
Supersedes NASA STD 5019(INT) & NASA STD 5007. (02/2008)
|
| DocumentType |
Standard
|
| PublisherName |
National Aeronautics and Space Administration
|
| Status |
Withdrawn
|
| Supersedes |
| NASA SP 3421 : 2011 | PROBABILISTIC RISK ASSESSMENT PROCEDURES GUIDE FOR NASA MANAGERS AND PRACTITIONERS |
| NASA JSC 65828 : 2011 | STRUCTURAL DESIGN REQUIREMENTS AND FACTORS OF SAFETY FOR SPACEFLIGHT HARDWARE |
| NASA MSFC SPEC 3679 : 2012 | PROCESS SPECIFICATION - WELDING AEROSPACE HARDWARE |
| NASA SPEC 5022:2015 | NASA MANUFACTURING AND TEST REQUIREMENTS FOR NORMALLY CLOSED PYROVALVES FOR HAZARDOUS FLIGHT SYSTEMS APPLICATIONS |
| NASA MSFC SPEC 3635 : 2012 | PYROTECHNIC SYSTEM SPECIFICATION |
| NASA PRC 6510 : 2011 | PROCESS SPECIFICATION FOR ULTRASONIC INSPECTION OF WELDS |
| NASA PRC 6509 : 2011 | PROCESS SPECIFICATION FOR EDDY CURRENT INSPECTION |
| NASA STD 6008 : 2008 CHANGE 1 2013 | NASA FASTENER PROCUREMENT, RECEIVING INSPECTION, AND STORAGE PRACTICES FOR SPACEFLIGHT HARDWARE |
| NASA PRC 6506 : 2011 | PROCESS SPECIFICATION FOR LIQUID PENETRANT INSPECTION |
| NASA PRC 6505 : 2011 | PROCESS SPECIFICATION FOR MAGNETIC PARTICLE INSPECTION |
| NASA STD 6016 : 2016 | STANDARD MATERIALS AND PROCESSES REQUIREMENTS FOR SPACECRAFT |
| NASA STD 8719.24 : 2011 | NASA EXPENDABLE LAUNCH VEHICLE PAYLOAD SAFETY REQUIREMENTS |
| NASA STD 5020 : 2012 | REQUIREMENTS FOR THREADED FASTENING SYSTEMS IN SPACEFLIGHT HARDWARE |
| NASA STD 5006 : 2015 | GENERAL FUSION WELDING REQUIREMENTS FOR AEROSPACE MATERIALS |
| NASA JSC 20793 : 2017 | CREWED SPACE VEHICLE BATTERY SAFETY REQUIREMENTS |
| NASA PRC 6503 : 2011 | PROCESS SPECIFICATION FOR RADIOGRAPHIC INSPECTION |
| NASA MSFC STD 3716 : 2017 | STANDARD FOR ADDITIVELY MANUFACTURED SPACEFLIGHT HARDWARE BY LASER POWDER BED FUSION IN METALS |
| NASA MSFC STD 3598 : 2015 | STANDARD FOR FOREIGN OBJECT DAMAGE/FOREIGN OBJECT DEBRIS (FOD) PREVENTION |
| NASA GSFC STD 7000 : 2013 | GENERAL ENVIRONMENTAL VERIFICATION STANDARD (GEVS) FOR GSFC FLIGHT PROGRAMS AND PROJECTS |
| NASA STD 5009 : 2008 | NONDESTRUCTIVE EVALUATION REQUIREMENTS FOR FRACTURE-CRITICAL METALLIC COMPONENTS - MEASUREMENT SYSTEM IDENTIFICATION: METRIC (INCH-POUND) |
| NASA STD 5012 : 2016 | STRENGTH AND LIFE ASSESSMENT REQUIREMENTS FOR LIQUID-FUELED SPACE PROPULSION SYSTEM ENGINES |
| NASA JSC 25863 : 2009 | FRACTURE CONTROL PLAN FOR JSC SPACE-FLIGHT HARDWARE |
| ASTM E 2982 : 2014 | Standard Guide for Nondestructive Testing of Thin-Walled Metallic Liners in Filament-Wound Pressure Vessels Used in Aerospace Applications |
| NASA-STD-5009C:2023 | Nondestructive Evaluation Requirements for Fracture Critical Metallic Components |
| ASME PV CODE 8 DIV 2 : 2017 | BOILER AND PRESSURE VESSEL CODE - RULES FOR CONSTRUCTION OF PRESSURE VESSELS DIVISION 2- ALTERNATIVE RULES |
| ASTM E 740/E740M : 2003 | PRACTICE FOR FRACTURE TESTING WITH SURFACE-CRACK TENSION SPECIMENS |
| NASA STD 6008 : 2008 CHANGE 1 2013 | NASA FASTENER PROCUREMENT, RECEIVING INSPECTION, AND STORAGE PRACTICES FOR SPACEFLIGHT HARDWARE |
| NASA STD 5020 : 2012 | REQUIREMENTS FOR THREADED FASTENING SYSTEMS IN SPACEFLIGHT HARDWARE |
| ASME PV CODE 8 DIV 1 : 2017 | BOILER AND PRESSURE VESSEL CODE - RULES FOR CONSTRUCTION OF PRESSURE VESSELS DIVISION 1 |
| NASA PRC 6509 : 2011 | PROCESS SPECIFICATION FOR EDDY CURRENT INSPECTION |
| NASA STD 5001 : 2014 | STRUCTURAL DESIGN AND TEST FACTORS OF SAFETY FOR SPACEFLIGHT HARDWARE |
| NASA STD 5017 : 2015 | DESIGN AND DEVELOPMENT REQUIREMENTS FOR MECHANISMS |
| SAE AS7468B | Bolts, Cobalt-Chromium-Nickel Alloy UNS R30035, Tensile Strength 260 ksi, Procurement Specification |
| ASTM E 1823 : 2013-07 | TERMINOLOGY RELATING TO FATIGUE AND FRACTURE TESTING |
| ASME FFS 1 : 2007 | FITNESS-FOR-SERVICE |
| NASA HDBK 5010 : 0 | FRACTURE CONTROL IMPLEMENTATION HANDBOOK FOR PAYLOADS, EXPERIMENTS, AND SIMILAR HARDWARE |
| NASA MSFC STD 3029 : 2000 | GUIDELINES FOR THE SELECTION OF METALLIC MATERIALS FOR STRESS CORROSION CRACKING RESISTANCE IN SODIUM CHLORIDE ENVIRONMENTS |
| NASA MSFC RQMT 3479 : 2006 | FRACTURE CONTROL REQUIREMENTS FOR COMPOSITE AND BONDED VEHICLE AND PAYLOAD STRUCTURES |
| ASTM E 2899 : 2015 : REDLINE | Standard Test Method for Measurement of Initiation Toughness in Surface Cracks Under Tension and Bending |
| NASA STD 5018 : 2011 | STRENGTH DESIGN AND VERIFICATION CRITERIA FOR GLASS, CERAMICS, AND WINDOWS IN HUMAN SPACE FLIGHT APPLICATIONS |
| API 579-1 : 2016 | FITNESS-FOR-SERVICE |
| MIL-HDBK-6870 Revision B:2012 | Nondestructive Inspection Program Requirements for Aircraft and Missile Materials and Parts |
| NASA STD 6016 : 2016 | STANDARD MATERIALS AND PROCESSES REQUIREMENTS FOR SPACECRAFT |
| NASA STD 5009 : 2008 | NONDESTRUCTIVE EVALUATION REQUIREMENTS FOR FRACTURE-CRITICAL METALLIC COMPONENTS - MEASUREMENT SYSTEM IDENTIFICATION: METRIC (INCH-POUND) |
| NASA JSC 20793 : 2017 | CREWED SPACE VEHICLE BATTERY SAFETY REQUIREMENTS |
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