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Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
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STANDARD MATERIALS AND PROCESSES REQUIREMENTS FOR SPACECRAFT
Published date
01-01-2016
Superseded date
06-15-2020
Superseded by
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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Superseded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 |
| 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 |
| 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 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 |
| ASTM G 63 : 2015 : REDLINE | Standard Guide for Evaluating Nonmetallic Materials for Oxygen Service |
| SAE AMS2773E | Heat Treatment Cast Nickel Alloy and Cobalt Alloy Parts |
| 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 |
| 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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