NASA STD 6016(INT) : 2006
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.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
11-07-2008
01-01-2006
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)
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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Superseded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 |
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 |
MIL HDBK 17-5 : 0 | COMPOSITE MATERIALS HANDBOOK - VOLUME 5: CERAMIC MATRIX COMPOSITES |
SAE AMS STD 401 : 1999 | SANDWICH CONSTRUCTIONS AND CORE MATERIALS - GENERAL TEST METHODS |
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 |
SAE AMS 2770 : 2015 | HEAT TREATMENT OF WROUGHT ALUMINUM ALLOY PARTS |
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 |
ASTM E 595 : 2015 : REDLINE | Standard Test Method for Total Mass Loss and Collected Volatile Condensable Materials from Outgassing in a Vacuum Environment |
MIL-STD-2223 Base Document:1992 | TEST METHODS FOR INSULATED ELECTRIC WIRE |
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 |
MIL-HDBK-454 Revision B:2007 | GENERAL GUIDELINES FOR ELECTRONIC EQUIPMENT |
MIL-STD-889 Revision C:2016 | DISSIMILAR METALS |
AWS C3.2M/C3.2 : 2008 | STANDARD METHOD FOR EVALUATING THE STRENGTH OF BRAZED JOINTS |
NASA STD 5009(INT) : 2006 | NONDESTRUCTIVE EVALUATION REQUIREMENTS FOR FRACTURE CRITICAL METALLIC COMPONENTS |
AWS C3.4 : 1999 | SPECIFICATION FOR TORCH BRAZING |
MIL-HDBK-17-3 Revision F:2002 | COMPOSITE MATERIALS HANDBOOK - VOLUME 3: POLYMER MATRIX COMPOSITES MATERIALS USAGE, DESIGN, AND ANALYSIS |
SAE AMS2491F | SURFACE TREATMENT OF POLYTETRAFLUOROETHYLENE (PTFE), PREPARATION FOR BONDING |
NASA STD 6008(INT) : 2006 | NASA FASTENER MANAGEMENT AND CONTROL PRACTICES |
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 |
SAE AMS H 81200 : 2014 | HEAT TREATMENT OF TITANIUM AND TITANIUM ALLOYS |
AWS C3.6 : 1999 | SPECIFICATION FOR FURNACE BRAZING |
SAE AMS 2759/9 : 2009 | HYDROGEN EMBRITTLEMENT RELIEF (BAKING) OF STEEL PARTS |
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 |
SAE AMS H 6875 : 2010 | HEAT TREATMENT OF STEEL RAW MATERIALS |
MIL-HDBK-17-1 Revision F:2002 | COMPOSITE MATERIALS HANDBOOK - VOLUME 1: POLYMER MATRIX COMPOSITES GUIDELINES FOR CHARACTERIZATION OF STRUCTURAL MATERIALS |
AIAA G 095 : 2004 | GUIDE TO SAFETY OF HYDROGEN AND HYDROGEN SYSTEMS |
NAS 412 : 1997 | FOREIGN OBJECT DAMAGE (FOD) PREVENTION GUIDANCE DOCUMENT |
MIL-HDBK-17-2 Revision F:2002 | COMPOSITE MATERIALS HANDBOOK - VOLUME 2: POLYMER MATRIX COMPOSITES MATERIALS PROPERTIES |
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