NASA STD 6016 : 2016
Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by
STANDARD MATERIALS AND PROCESSES REQUIREMENTS FOR SPACECRAFT
Superseded date
15-06-2020
Superseded by
Published date
01-01-2016
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DOCUMENT HISTORY LOG
FOREWORD
1. SCOPE
2. APPLICABLE DOCUMENTS
3. ACRONYMS AND DEFINITIONS
4. REQUIREMENTS
APPENDIX
A - Standard Materials and Processes Requirements for
Spacecraft - Requirements Compliance Matrix with
Requirements Justifications
B - Typical MUA Form
C - Retired Category III MUA Rationale Codes
D - Recommended Data Requirements Documents
E - References
Describes materials and processes (M&P) used in the design, fabrication, and testing of space program flight hardware for NASA, including but not limited to crewed, uncrewed, robotic, launch vehicle, lander, in-space and surface systems, and spacecraft program/project hardware elements.
| DevelopmentNote |
Supersedes NASA STD 6016(INT). (07/2008)
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| DocumentType |
Standard
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| PublisherName |
National Aeronautics and Space Administration
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| Status |
Superseded
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| SupersededBy | |
| Supersedes |
| NASA STD 5001 : 2014 | STRUCTURAL DESIGN AND TEST FACTORS OF SAFETY FOR SPACEFLIGHT HARDWARE |
| NASA STD 5018 : 2011 | STRENGTH DESIGN AND VERIFICATION CRITERIA FOR GLASS, CERAMICS, AND WINDOWS IN HUMAN SPACE FLIGHT APPLICATIONS |
| NASA STD 4003 : 2013 | ELECTRICAL BONDING FOR NASA LAUNCH VEHICLES, SPACECRAFT, PAYLOADS, AND FLIGHT EQUIPMENT |
| NASA JSC 65828 : 2011 | STRUCTURAL DESIGN REQUIREMENTS AND FACTORS OF SAFETY FOR SPACEFLIGHT HARDWARE |
| NASA KSC KTI 5210 : 2012 | MATERIAL SELECTION LIST FOR OXYGEN SERVICE |
| 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 3659 : 2012 | PROCESS SPECIFICATION FOR ELECTRICAL BONDING |
| NASA MSFC SPEC 3635 : 2012 | PYROTECHNIC SYSTEM SPECIFICATION |
| NASA STD 8739.6 : 2016 | IMPLEMENTATION REQUIREMENTS FOR NASA WORKMANSHIP STANDARDS |
| NASA PRC 0015 : 2016 | PROCESS SPECIFICATION FOR AUTOMATIC AND MACHINE ARC WELDING OF TITANIUM AND TITANIUM ALLOY HARDWARE |
| NASA STD 5019 : 2016 | FRACTURE CONTROL REQUIREMENTS FOR SPACEFLIGHT HARDWARE |
| NASA JSC 08080-2 : 2015 | JSC DESIGN AND PROCEDURAL STANDARDS |
| NASA STD 6001 : 2011 | FLAMMABILITY, OFFGASSING, AND COMPATIBILITY REQUIREMENTS AND TEST PROCEDURES |
| NASA MSFC STD 3012 : 2012 | ELECTRICAL, ELECTRONIC, AND ELECTROMECHANICAL (EEE) PARTS MANAGEMENT AND CONTROL REQUIREMENTS FOR MSFC SPACE FLIGHT HARDWARE |
| NASA STD 5020 : 2012 | REQUIREMENTS FOR THREADED FASTENING SYSTEMS IN SPACEFLIGHT HARDWARE |
| NASA STD 5017 : 2015 | DESIGN AND DEVELOPMENT REQUIREMENTS FOR MECHANISMS |
| NASA STD 5006 : 2015 | GENERAL FUSION WELDING REQUIREMENTS FOR AEROSPACE MATERIALS |
| NASA STD 8739.10 : 2017 | ELECTRICAL, ELECTRONIC, AND ELECTROMECHANICAL (EEE) PARTS ASSURANCE STANDARD |
| NASA MSFC STD 246 : 2011 | STANDARD DESIGN AND OPERATIONAL CRITERIA FOR CONTROLLED ENVIRONMENTAL AREAS |
| NASA STD 6012 : 2012 | CORROSION PROTECTION FOR SPACE FLIGHT HARDWARE |
| 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 MSFC STD 557 : 2012 | THREADED FASTENERS, TITANIUM ALLOYS, USAGE CRITERIA FOR LAUNCH VEHICLES AND SPACECRAFT APPLICATIONS |
| NASA JSC 27301 : 2009 | MATERIALS AND PROCESSES SELECTION, CONTROL, AND IMPLEMENTATION PLAN FOR JSC FLIGHT HARDWARE |
| 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 |
| MIL HDBK 17-5 : 0 | COMPOSITE MATERIALS HANDBOOK - VOLUME 5: CERAMIC MATRIX COMPOSITES |
| SAE AMS2801B | Heat Treatment of Titanium Alloy Parts |
| SAE AMS2404G | Plating, Electroless Nickel |
| ASTM B 733 : 2015 : REDLINE | Standard Specification for Autocatalytic (Electroless) Nickel-Phosphorus Coatings on Metal |
| NASA STD 5020 : 2012 | REQUIREMENTS FOR THREADED FASTENING SYSTEMS IN SPACEFLIGHT HARDWARE |
| SAE AMS 2488 : 2000 | ANODIC TREATMENT - TITANIUM AND TITANIUM ALLOYS SOLUTION PH 13 OR HIGHER |
| SAE AMS 2175 : 2010 | CASTINGS, CLASSIFICATION AND INSPECTION OF |
| AWS D17.3/D17.3M : 2016 | SPECIFICATION FOR FRICTION STIR WELDING OF ALUMINUM ALLOYS FOR AEROSPACE APPLICATIONS |
| NASA STD 6001 : 2011 | FLAMMABILITY, OFFGASSING, AND COMPATIBILITY REQUIREMENTS AND TEST PROCEDURES |
| MIL-STD-810 Revision G:2008 | ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS |
| SAE AMS2770M | Heat Treatment of Wrought Aluminum Alloy Parts |
| AWS C3.7M/C3.7 : 2011 | SPECIFICATION FOR ALUMINUM BRAZING |
| NASA STD 6012 : 2012 | CORROSION PROTECTION FOR SPACE FLIGHT HARDWARE |
| AWS C3.6M/C3.6 : 2016 | SPECIFICATION FOR FURNACE BRAZING |
| NAS410:2003 | NAS CERTIFICATION & QUALIFICATION OF NONDESTRUCTIVE TEST PERSONNEL |
| ASTM G 88 : 2013 : REDLINE | Standard Guide for Designing Systems for Oxygen Service |
| ASTM E 595 : 2015 : REDLINE | Standard Test Method for Total Mass Loss and Collected Volatile Condensable Materials from Outgassing in a Vacuum Environment |
| AWS G2.4/G2.4M : 2007 | GUIDE FOR THE FUSION WELDING OF TITANIUM AND TITANIUM ALLOYS |
| AWS C3.3 : 2008 | RECOMMENDED PRACTICES FOR THE DESIGN, MANUFACTURE, AND EXAMINATION OF CRITICAL BRAZED COMPONENTS |
| SAE AMS2759E | Heat Treatment of Steel Parts General Requirements |
| AWS C3.5M/C3.5 : 2016 | SPECIFICATION FOR INDUCTION BRAZING |
| MIL-STD-1252 Base Document:1975 | INERTIA FRICTION WELDING PROCESS, PROCEDURE AND PERFORMANCE QUALIFICATION |
| MIL-HDBK-454 Revision B:2007 | GENERAL GUIDELINES FOR ELECTRONIC EQUIPMENT |
| AWS D17.2/D17.2M : 2013 | SPECIFICATION FOR RESISTANCE WELDING FOR AEROSPACE APPLICATIONS |
| AWS C3.4M/C3.4 : 2016 | SPECIFICATION FOR TORCH BRAZING |
| AWS C3.2M/C3.2 : 2008 | STANDARD METHOD FOR EVALUATING THE STRENGTH OF BRAZED JOINTS |
| SAE AS22759C | Wire, Electrical, Fluoropolymer-Insulated, Copper or Copper Alloy |
| SAE AMS2491F | Surface Treatment of Polytetrafluoroethylene (PTFE) Preparation for Bonding |
| SAE AMS2423E | Plating, Nickel Hard Deposit |
| SAE AMS 2680 : 2001 | ELECTRON-BEAM WELDING, FOR FATIGUE CRITICAL APPLICATIONS |
| GEIA STD 0005-2 : 2012 | MITIGATING THE EFFECTS OF TIN WHISKERS IN AEROSPACE AND HIGH PERFORMANCE ELECTRONIC SYSTEMS |
| ASTM E 2900 : 2012 | Standard Practice for Spacecraft Hardware Thermal Vacuum Bakeout |
| SAE R-427 : 2013 | Composite Materials Handbook Volume 6 - Initial Release |
| SAE AMS2772G | Heat Treatment of Aluminum Alloy Raw Materials |
| NASA STD 5019 : 2016 | FRACTURE CONTROL REQUIREMENTS FOR SPACEFLIGHT HARDWARE |
| NASA MSFC STD 3029 : 2000 | GUIDELINES FOR THE SELECTION OF METALLIC MATERIALS FOR STRESS CORROSION CRACKING RESISTANCE IN SODIUM CHLORIDE ENVIRONMENTS |
| NASA STD 5006 : 2015 | GENERAL FUSION WELDING REQUIREMENTS FOR AEROSPACE MATERIALS |
| NASA JSC 29353 : 2014 | FLAMMABILITY CONFIGURATION ANALYSIS FOR SPACECRAFT APPLICATIONS |
| SAE AMSH81200D | Heat Treatment of Titanium and Titanium Alloys |
| SAE AMS2759/9D | Hydrogen Embrittlement Relief (Baking) of Steel Parts |
| NASA MSFC SPEC 445 : 1990 | ADHESIVE BONDING, PROCESS AND INSPECTION, REQUIREMENTS FOR |
| SAE AMS2774E | Heat Treatment Wrought Nickel Alloy and Cobalt Alloy Parts |
| GEIA STD 0005-1 : 2012 | PERFORMANCE STANDARD FOR AEROSPACE AND HIGH PERFORMANCE ELECTRONIC SYSTEMS CONTAINING LEAD-FREE SOLDER |
| NASA STD 5005 : 2013 | STANDARD FOR THE DESIGN AND FABRICATION OF GROUND SUPPORT EQUIPMENT |
| SAE AMS2403M | Plating, Nickel General Purpose |
| SAE R-424 : 2012 | COMPOSITE MATERIALS HANDBOOK - VOLUME 3 |
| ASTM G 63 : 2015 : REDLINE | Standard Guide for Evaluating Nonmetallic Materials for Oxygen Service |
| SAE AMS 2453 : 2015 | LOW STRESS GRINDING OF STEEL PARTS HEAT TREATED TO 180 KSI OR OVER, AND LOW STRESS GRINDING OF CHROME PLATING APPLIED TO STEEL PARTS HEAT TREATED TO 180 KSI OR OVER |
| SAE AMS2773E | Heat Treatment Cast Nickel Alloy and Cobalt Alloy Parts |
| SAE R-423 : 2012 | COMPOSITE MATERIALS HANDBOOK - VOLUME 2: POLYMER MATRIX COMPOSITES: MATERIALS PROPERTIES |
| SAE R-425 : 2013 | COMPOSITE MATERIALS HANDBOOK - VOLUME 4: METAL MATRIX COMPOSITES |
| MIL-HDBK-6870 Revision B:2012 | NONDESTRUCTIVE INSPECTION PROGRAM REQUIREMENTS FOR AIRCRAFT AND MISSILE MATERIALS AND PARTS |
| SAE R-422 : 2012 | COMPOSITE MATERIALS HANDBOOK - VOLUME 1 |
| SAE AMS H 6875 : 2010 | HEAT TREATMENT OF STEEL RAW MATERIALS |
| NASA STD 5012 : 2016 | STRENGTH AND LIFE ASSESSMENT REQUIREMENTS FOR LIQUID-FUELED SPACE PROPULSION SYSTEM ENGINES |
| AIAA G 095 : 2004 | GUIDE TO SAFETY OF HYDROGEN AND HYDROGEN SYSTEMS |
| NAS 412 : 1997 | FOREIGN OBJECT DAMAGE (FOD) PREVENTION GUIDANCE DOCUMENT |
| AWS D17.1/D17.1M : 2012 | SPECIFICATION FOR FUSION WELDING FOR AEROSPACE APPLICATIONS |
| NASA STD 5009 : 2008 | NONDESTRUCTIVE EVALUATION REQUIREMENTS FOR FRACTURE-CRITICAL METALLIC COMPONENTS - MEASUREMENT SYSTEM IDENTIFICATION: METRIC (INCH-POUND) |
| AWS C7.4/C7.4M : 2008 | PROCESS SPECIFICATION AND OPERATOR QUALIFICATION FOR LASER BEAM WELDING |
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