The citations below refer to the sections in this NASA Technical Standard.
ASTM B689-97 (Reapproved 2013) (Cited in section 4.2.4.10): ASTM International (ASTM).1=Standard Specification for Electroplated Engineering Nickel Coatings ASTM B733-15 (Cited in sections 4.2.4.10 and 4.2.6.3): ASTM International (ASTM).1=Standard Specification for Autocatalytic (Electroless) Nickel-Phosphorus Coatings on Metal
NOTE: Per section 4.1.6: The use of M&P that do not comply with the requirements of this NASA Technical Standard may be acceptable in the actual hardware applications. MUAs are required for all M&P that are technically acceptable but do not meet the requirements of this NASA Technical Standard, as implemented by the approved Materials and Processes Selection, Control, and Implementation Plan.
NASA-STD-6016B
ASTM E1548 (2009) (Cited in section 4.2.6.7): 1=Standard Practice for Preparation of Aerospace Contamination Control Plans AWS C3.2M/C3.2 (2008) (Cited in section 4.2.4.7): 1=Standard Method for Evaluating the Strength of Brazed Joints AWS C3.3 (2008) (Cited in section 4.2.4.7): 1=Recommended Practices for Design, Manufacture, and Examination of Critical Brazed Components AWS C3.4M/C3.4 (2016) (Cited in section 4.2.4.7): 1=Specification for Torch Brazing AWS C3.5M/C3.5 (2016) (Cited in section 4.2.4.7): 1=Specification for Induction Brazing AWS C3.6M/C3.6 (2016) (Cited in section 4.2.4.7): 1=Specification for Furnace Brazing AWS C3.7M/C3.7 (2011) (Cited in section 4.2.4.7): 1=Specification for Aluminum Brazing AWS C7.4/C7.4M (2008) (Cited in section 4.2.4.6.1): 1=Process Specification and Operator Qualification for Laser Beam Welding AWS D17.1/D17.1M (2010) AMD1 (2012) (Cited in section 4.2.4.6.1): 1=Specification for Fusion Welding for Aerospace Applications AWS D17.2/D17.2M (2013) (Cited in section 4.2.4.6.2): 1=Specification for Resistance Welding for Aerospace Applications AWS D17.3/D17.3M (2016) (Cited in section 4.2.4.6.3): 1=Specification for Friction Stir Welding of Aluminum Alloys for Aerospace Applications NOTE: Per section 4.1.6: The use of M&P that do not comply with the requirements of this NASA Technical Standard may be acceptable in the actual hardware applications. MUAs are required for all M&P that are technically acceptable but do not meet the requirements of this NASA Technical Standard, as implemented by the approved Materials and Processes Selection, Control, and Implementation Plan.
NASA-STD-6016B Battelle Memorial Institute
MMPDS-10 (2015) (Cited in section 4.1.8.1, 4.1.8.2, and 4.2.4.1): 1=Metallic Materials Properties Development and Standardization (MMPDS) GEIA-STD-0005-1A (2012) (Cited in section 4.2.2.11): Government Electronics and Information Technology Association (GEIA) (SAE International).1=Performance Standard for Aerospace and High Performance Electronic Systems Containing Lead-Free Solder GEIA-STD-0005-2A (2012) (Cited in section 4.2.2.11): Government Electronics and Information Technology Association (GEIA) (SAE International).1=Standard for Mitigating the Effects of Tin Whiskers in Aerospace and High Performance Electronic Systems NAS 410, Revision 4 (2014) (Cited in section 4.2.5.1): Government Electronics and Information Technology Association (GEIA) (SAE International).1=NAS Certification and Qualification of Nondestructive Test Personnel NAS 412, Revision 1 (2013) (Cited in section 4.2.6.7): Government Electronics and Information Technology Association (GEIA) (SAE International).1=Foreign Object Damage/Foreign Object Debris (FOD) Prevention SAE AMS2175A (2010) (Cited in section 4.2.4.3): Government Electronics and Information Technology Association (GEIA) (SAE International).1=Castings, Classification and Inspection of SAE AMS2375D (2007, Reaffirmed 2012) (Cited in section 4.2.4.2): Government Electronics and Information Technology Association (GEIA) (SAE International).1=Control of Forgings Requiring First Article Approval SAE AMS2403N (2015) (Cited in section 4.2.4.10): Government Electronics and Information Technology Association (GEIA) (SAE International).1=Plating, Nickel General Purpose SAE AMS2404G (2013) (Cited in section 4.2.4.10 and 4.2.6.3): Government Electronics and Information Technology Association (GEIA) (SAE International).1=Plating, Electroless Nickel SAE AMS2423E (2015) (Cited in section 4.2.4.10): Government Electronics and Information Technology Association (GEIA) (SAE International).1=Plating, Nickel Hard Deposit NOTE: Per section 4.1.6: The use of M&P that do not comply with the requirements of this NASA Technical Standard may be acceptable in the actual hardware applications. MUAs are required for all M&P that are technically acceptable but do not meet the requirements of this NASA Technical Standard, as implemented by the approved Materials and Processes Selection, Control, and Implementation Plan.
SAE AMS2488D (2000, Reaffirmed 2011) (Cited in section 4.2.2.3.2): 1=Anodic Treatment - Titanium and Titanium Alloys Solution, pH 13 or Higher SAE AMS2491F (2015) (Cited in section 4.2.3.10): 1=Surface Treatment of Polytetrafluoroethylene, Preparation for Bonding SAE AMS2680C (2001, Reaffirmed 2010) (Cited in section 4.2.4.6.1): 1=Electron-Beam Welding for Fatigue Critical Applications SAE AMS2759E (2008, Reaffirmed 2014) (Cited in section 4.2.4.1): 1=Heat Treatment of Steel Parts, General Requirements SAE AMS2759/9D (2009) (Cited in sections 4.2.6.4): 1=Hydrogen Embrittlement Relief (Baking) of Steel Parts SAE AMS2770N (2015) (Cited in section 4.2.4.1): 1=Heat Treatment of Wrought Aluminum Alloy Parts SAE AMS2771E (2013) (Cited in section 4.2.4.1): 1=Heat Treatment of Aluminum Alloy Castings SAE AMS2772G (2016) (Cited in section 4.2.4.1): 1=Heat Treatment of Aluminum Alloy Raw Materials SAE AMS2773E (2013) (Cited in section 4.2.4.1): 1=Heat Treatment, Cast Nickel Alloy and Cobalt Alloy Parts SAE AMS2774E (2016) (Cited in section 4.2.4.1): 1=Heat Treatment, Wrought Nickel Alloy and Cobalt Alloy Parts SAE AMS2801B (2003, Reaffirmed 2014) (Cited in section 4.2.4.1 and 4.2.4.6.1): 1=Heat Treatment of Titanium Alloy Parts SAE AMS-H-6875B (2010) (Cited in 4.2.4.1): 1=Heat Treatment of Steel Raw Materials NOTE: Per section 4.1.6: The use of M&P that do not comply with the requirements of this NASA Technical Standard may be acceptable in the actual hardware applications. MUAs are required for all M&P that are technically acceptable but do not meet the requirements of this NASA Technical Standard, as implemented by the approved Materials and Processes Selection, Control, and Implementation Plan.
NASA-STD-6016B
SAE AMS-H-81200D (2014) (Cited in sections 4.2.4.1 and 4.2.4.6.1): 1=Heat Treatment of Titanium and Titanium Alloys SAE AMS-STD-401 (1999) (Cited in section 4.2.6.2): 1=Sandwich Constructions and Core Materials: General Test Methods SAE AS22759C (2014) (Cited in section 4.2.1.5): 1=Wire, Electrical, Fluoropolymer-Insulated, Copper or Copper Alloy SAE CMH-17-1G (2012) (Cited in section 4.1.8.1): 1=Composite Materials Handbook Volume 1 - Polymer Matrix Composites Guidelines for Characterization of Structural Materials SAE CMH-17-2G (2012) (Cited in section 4.1.8.1): 1=Composite Materials Handbook Volume 2 - Polymer Matrix Composites Materials Properties SAE CMH-17-3G (2012) (Cited in section 4.1.8.1): 1=Composite Materials Handbook Volume 3 - Polymer Matrix Composites Materials Usage, Design, and Analysis SAE CMH-17-4B (2013) (Cited in section 4.1.8.1): 1=Composite Materials Handbook Volume 4 - Metal Matrix Composites MIL-HDBK-17-5 (2002) (Reference section 4.1.8.1)— (Use until SAE CMH-17-5 is published, scheduled in 2017): 1=Composite Materials Handbook Volume 5 - Ceramic Matrix Composites SAE CMH-17-6 (2013) (Cited in section 4.1.8.1): 1=Composite Materials Handbook Volume 6 – Structural Sandwich Composites Refer to Appendix E for References.
NOTE: Per section 4.1.6: The use of M&P that do not comply with the requirements of this NASA Technical Standard may be acceptable in the actual hardware applications. MUAs are required for all M&P that are technically acceptable but do not meet the requirements of this NASA Technical Standard, as implemented by the approved Materials and Processes Selection, Control, and Implementation Plan.
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