• NASA STD 6016 : 2016

    Superseded A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.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

    Available format(s): 

    Superseded date:  06-15-2020

    Language(s): 

    Published date:  01-01-2016

    Publisher:  National Aeronautics and Space Administration

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    Table of Contents - (Show below) - (Hide below)

    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

    Abstract - (Show below) - (Hide below)

    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.

    General Product Information - (Show below) - (Hide below)

    Development Note Supersedes NASA STD 6016(INT). (07/2008)
    Document Type Standard
    Publisher National Aeronautics and Space Administration
    Status Superseded
    Superseded By
    Supersedes

    Standards Referenced By This Book - (Show below) - (Hide below)

    NASA JSC 25863 : 2009 FRACTURE CONTROL PLAN FOR JSC SPACE-FLIGHT HARDWARE
    NASA STD 5012 : 2016 STRENGTH AND LIFE ASSESSMENT REQUIREMENTS FOR LIQUID-FUELED SPACE PROPULSION SYSTEM ENGINES
    NASA STD 5001 : 2014 STRUCTURAL DESIGN AND TEST FACTORS OF SAFETY FOR SPACEFLIGHT HARDWARE
    NASA KSC KTI 5210 : 2012 MATERIAL SELECTION LIST FOR OXYGEN SERVICE
    NASA STD 5018 : 2011 STRENGTH DESIGN AND VERIFICATION CRITERIA FOR GLASS, CERAMICS, AND WINDOWS IN HUMAN SPACE FLIGHT APPLICATIONS
    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 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

    Standards Referencing This Book - (Show below) - (Hide below)

    MIL HDBK 17-5 : 0 COMPOSITE MATERIALS HANDBOOK - VOLUME 5: CERAMIC MATRIX COMPOSITES
    SAE AMS 2801 : 2014 HEAT TREATMENT OF TITANIUM ALLOY PARTS
    SAE AMS 2404 : 2013 PLATING, ELECTROLESS NICKEL
    ASTM B 733 : 2015 : REDLINE Standard Specification for Autocatalytic (Electroless) Nickel-Phosphorus Coatings on Metal
    SAE AMS STD 401 : 1999 SANDWICH CONSTRUCTIONS AND CORE MATERIALS - GENERAL TEST METHODS
    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 : G ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS
    SAE AMS 2770 : 2015 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
    NAS 410 : 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 AMS 2759 : 2014 HEAT TREATMENT OF STEEL PARTS, GENERAL REQUIREMENTS
    AWS C3.5M/C3.5 : 2016 SPECIFICATION FOR INDUCTION BRAZING
    MIL STD 1252 : 0 INERTIA FRICTION WELDING PROCESS, PROCEDURE AND PERFORMANCE QUALIFICATION
    MIL HDBK 454 : B 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 AS 22759 : 2014 WIRE, ELECTRICAL, FLUOROPOLYMER-INSULATED, COPPER OR COPPER ALLOY
    SAE AMS 2491 : 2015 SURFACE TREATMENT OF POLYTETRAFLUOROETHYLENE (PTFE), PREPARATION FOR BONDING
    SAE AMS 2423 : 2015 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: STRUCTURAL SANDWICH COMPOSITES
    SAE AMS 2772 : 2016 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 AMS H 81200 : 2014 HEAT TREATMENT OF TITANIUM AND TITANIUM ALLOYS
    SAE AMS 2759/9 : 2009 HYDROGEN EMBRITTLEMENT RELIEF (BAKING) OF STEEL PARTS
    NASA MSFC SPEC 445 : 1990 ADHESIVE BONDING, PROCESS AND INSPECTION, REQUIREMENTS FOR
    SAE AMS 2774 : 2016 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 AMS 2403 : 2015 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 2375 : 2017-07 CONTROL OF FORGINGS REQUIRING FIRST ARTICLE APPROVAL
    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 AMS 2773 : 2013 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 : B 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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