NASA STD 5019 : 2016
Withdrawn
Withdrawn
A Withdrawn Standard is one, which is removed from sale, and its unique number can no longer be used. The Standard can be withdrawn and not replaced, or it can be withdrawn and replaced by a Standard with a different number.
FRACTURE CONTROL REQUIREMENTS FOR SPACEFLIGHT HARDWARE
Withdrawn date
17-10-2019
Published date
01-02-2016
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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
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| Status |
Withdrawn
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| 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 |
| NASM85604:2012 | BOLT, NICKEL ALLOY 718, TENSION, HIGH STRENGTH, 125 KSI FSU AND 220 KSI FTU, HIGH TEMPERATURE, SPLINE DRIVE |
| 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 |
| NASM1312-11:2017 | FASTENER TEST METHODS METHOD 11 TENSION FATIGUE |
| 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 |
| NA 0271 : REV 2 | PROCUREMENT SPECIFICATION, METRIC FASTENERS, CRES 300 SERIES, EXTERNALLY THREADED, MJ THREAD, 500 MPA FTU AND 700 MPA FTU |
| 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 |
| NA 0026 : REV 3 | PROCUREMENT SPECIFICATION, METRIC FASTENERS, A-286 CRES EXTERNALLY THREADED, 1100 MPA TENSILE, 660 MPA SHEAR |
| NAM 1312/111 : REV 1 | FASTENER TEST METHODS, METRIC METHOD 111 TENSION FATIGUE |
| API 579-1 : 2016 | FITNESS-FOR-SERVICE |
| MIL-HDBK-6870 Revision B:2012 | NONDESTRUCTIVE INSPECTION PROGRAM REQUIREMENTS FOR AIRCRAFT AND MISSILE MATERIALS AND PARTS |
| NAS 4003 : 2003 | FASTENER, A286 CORROSION RESISTANT ALLOY, EXTERNALLY THREADED, 160 KSI FTU, 95 KSI FSU, 1000 DEGREES F |
| 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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