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NASA STD 6016(INT) : 2006

Superseded

Superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.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

Superseded date

11-07-2008

Published date

01-01-2006

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DOCUMENT HISTORY LOG
FOREWORD
1. SCOPE
   1.1 Purpose
   1.2 Applicability
2. APPLICABLE DOCUMENTS
   2.1 General
   2.2 Government Documents
   2.3 Non-Government Documents
       2.3.1 Voluntary Consensus Standards
   2.4 Order of Precedence
3. ACRONYMS AND DEFINITIONS
   3.1 Acronyms
   3.2 Definitions
4. REQUIREMENTS
   4.1 General Requirements
       4.1.1 Materials and Processes, Selection Control,
             and Implementation Plan
       4.1.2 Materials and Processes Usage Documentation
       4.1.3 Materials Usage Agreement (MUAs)
       4.1.4 Manufacturing Planning
       4.1.5 Materials Certification and Traceability
       4.1.6 Material Design Allowables
   4.2 Detailed Requirements
       4.2.1 Flammability, Offgassing, and Compatibility
             Requirements
       4.2.2 Metals
       4.2.3 Nonmetallic Materials
       4.2.4 Processes
       4.2.5 Material Nondestructive Inspection
       4.2.6 Special Materials Requirements
   4.3 Verification
5. GUIDANCE
   5.1 Reference Documents
Appendix A - MUA Form
Appendix B - Category III MUA Rationale Codes Flammability
             Rationale Codes
Appendix C - Recommended Data Requirements Documents

Defines the minimum requirements for M&P and provides a general control specification for incorporation in NASA program/project hardware procurements and technical programs.

DevelopmentNote
Expires 10 Sept 2007. (10/2006)
DocumentType
Standard
PublisherName
National Aeronautics and Space Administration
Status
Superseded
SupersededBy

NASA STD 6002 : 2008 APPLYING DATA MATRIX IDENTIFICATION SYMBOLS ON AEROSPACE PARTS
NASA STD 6001(INT) : 2009 FLAMMABILITY, OFFGASSING, AND COMPATIBILITY REQUIREMENTS AND TEST PROCEDURES

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SAE AMS 2488 : 2000 ANODIC TREATMENT - TITANIUM AND TITANIUM ALLOYS SOLUTION PH 13 OR HIGHER
SAE AMS 2175 : 2010 CASTINGS, CLASSIFICATION AND INSPECTION OF
NASA STD 6001 : 2011 FLAMMABILITY, OFFGASSING, AND COMPATIBILITY REQUIREMENTS AND TEST PROCEDURES
MIL-STD-810 Revision G:2008 ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS
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AWS C3.7M/C3.7 : 2011 SPECIFICATION FOR ALUMINUM BRAZING
AWS C3.5 : 1999 SPECIFICATION FOR INDUCTION BRAZING
NAS410:2003 NAS CERTIFICATION & QUALIFICATION OF NONDESTRUCTIVE TEST PERSONNEL
ASTM G 88 : 2013 : REDLINE Standard Guide for Designing Systems for Oxygen Service
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MIL-STD-2223 Base Document:1992 TEST METHODS FOR INSULATED ELECTRIC WIRE
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MIL-HDBK-454 Revision B:2007 GENERAL GUIDELINES FOR ELECTRONIC EQUIPMENT
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NASA STD 5009(INT) : 2006 NONDESTRUCTIVE EVALUATION REQUIREMENTS FOR FRACTURE CRITICAL METALLIC COMPONENTS
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SAE AMS 2772 : 2016 HEAT TREATMENT OF ALUMINUM ALLOY RAW MATERIALS
MIL-HDBK-17-4 Revision A:2002 Composite Materials Handbook - Volume 4 Metal Matrix Composites
NASA STD 5006 : 2015 GENERAL FUSION WELDING REQUIREMENTS FOR AEROSPACE MATERIALS
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SAE AMS 2774 : 2016 HEAT TREATMENT, WROUGHT NICKEL ALLOY AND COBALT ALLOY PARTS
ASTM G 63 : 2015 : REDLINE Standard Guide for Evaluating Nonmetallic Materials for Oxygen Service
MIL-HDBK-6870 Revision B:2012 NONDESTRUCTIVE INSPECTION PROGRAM REQUIREMENTS FOR AIRCRAFT AND MISSILE MATERIALS AND PARTS
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NAS 412 : 1997 FOREIGN OBJECT DAMAGE (FOD) PREVENTION GUIDANCE DOCUMENT
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