The documents in these paragraphs are applicable to the extent specified. The citations below refer to the sections in this NASA Technical Standard.
National Aeronautics and Space Administration (NASA)
NASA-STD-5006A with Change 1 (2016) (Cited in section 4.2.4.6): 1=General Welding Requirements for Aerospace Materials NASA-STD-5009 (2008) (Cited in section 4.2.5.1): 1=Nondestructive Evaluation Requirements for Fracture-Critical Metallic Components NASA-STD-5020 (2012) (Cited in section 4.2.6.6.1): 1=Requirements for Threaded Fastening Systems in Spaceflight Hardware NASA-STD-6001B (2011) with Change 2 (2016) (Cited in sections 4.2.1, 4.2.1.1, 4.2.1.2, 4.2.1.4, and 4.2.1.5): 1=Flammability, Offgassing, and Compatibility Requirements and Test Procedures NASA-STD-6012 (2012) (Cited in section 4.2.6.3): 1=Corrosion Protection for Space Flight Hardware JSC 20584 (2008) (Cited in section 4.2.1.2): 1=Spacecraft Maximum Allowable Concentrations for Airborne Contaminants Materials and Processes Technical Information System (MAPTIS) (Cited in section 4.2.1.2): 1=Materials Selection List for Space Hardware Systems 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.
| 1 | |
|---|---|
| NPR 7120.5 (Cited in section 1.3) | NASA Space Flight Program and Project Management Requirements |
| NPR 7120.8 (Cited in section 1.3) | NASA Research and Technology Program and Project Management Requirements |
| NASA-STD-5006A with Change 1 (2016) (Cited in section 4.2.4.6) | General Welding Requirements for Aerospace Materials |
| NASA-STD-5009 (2008) (Cited in section 4.2.5.1) | Nondestructive Evaluation Requirements for Fracture-Critical Metallic Components |
| NASA-STD-5020 (2012) (Cited in section 4.2.6.6.1) | Requirements for Threaded Fastening Systems in Spaceflight Hardware |
| NASA-STD-6001B (2011) with Change 2 (2016) (Cited in sections 4.2.1, 4.2.1.1, 4.2.1.2, 4.2.1.4, and 4.2.1.5) | Flammability, Offgassing, and Compatibility Requirements and Test Procedures |
| NASA-STD-6012 (2012) (Cited in section 4.2.6.3) | Corrosion Protection for Space Flight Hardware |
| JSC 20584 (2008) (Cited in section 4.2.1.2) | Spacecraft Maximum Allowable Concentrations for Airborne Contaminants |
| JSC 29353 (Cited in section 4.2.1.1) | Flammability Configuration Analysis for Spacecraft Applications |
| Materials and Processes Technical Information System (MAPTIS) (Cited in section 4.2.1.2) | Materials Selection List for Space Hardware Systems |
| MSFC-SPEC-445A (1990) (Cited in section 4.2.4.5) | Adhesive Bonding, Process and Inspection, Requirements for |
| MSFC-STD-3029A (2005) (Cited in section 4.2.2) | Guidelines for the Selection of Metallic Materials for Stress Corrosion Cracking Resistance in Sodium Chloride Environments |
| Department of Defense | Department of Defense |
| MIL-STD-810G (2008), with Change 1 (2014) (Cited in section 4.2.3.8) | Department of Defense Test Method Standard for Environmental Engineering Considerations and Laboratory Tests |
| MIL-STD-1252 (1975) (Cited in section 4.2.4.6.4) (Inactive for New Design effective 3/11/1998 but determined by NASA to be the best existing standard for use) | Inertia Friction Welding Process, Procedure and Performance Qualification |
| MIL-HDBK-454B (Cited in section 4.2.3.8) | General Guidelines for Electronic Equipment |
| MIL-HDBK-6870B (2012) (Cited in section 4.2.5.1) | Nondestructive Inspection Program Requirements for Aircraft and Missile Materials and Parts |
| ASTM E595-15 (Cited in section 4.2.3.6) | Standard Test Method for Total Mass Loss and Collected Volatile Condensable Materials from Outgassing in a Vacuum Environment |
| ASTM E1548 (2009) (Cited in section 4.2.6.7) | Standard Practice for Preparation of Aerospace Contamination Control Plans |
| American Welding Society (AWS) | American Welding Society (AWS) |
| AWS C3.2M/C3.2 (2008) (Cited in section 4.2.4.7) | Standard Method for Evaluating the Strength of Brazed Joints |
| AWS C3.3 (2008) (Cited in section 4.2.4.7) | Recommended Practices for Design, Manufacture, and Examination of Critical Brazed Components |
| AWS C3.4M/C3.4 (2016) (Cited in section 4.2.4.7) | Specification for Torch Brazing |
| AWS C3.5M/C3.5 (2016) (Cited in section 4.2.4.7) | Specification for Induction Brazing |
| AWS C3.6M/C3.6 (2016) (Cited in section 4.2.4.7) | Specification for Furnace Brazing |
| AWS C3.7M/C3.7 (2011) (Cited in section 4.2.4.7) | Specification for Aluminum Brazing |
| AWS C7.4/C7.4M (2008) (Cited in section 4.2.4.6.1) | 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) | Specification for Fusion Welding for Aerospace Applications |
| AWS D17.2/D17.2M (2013) (Cited in section 4.2.4.6.2) | Specification for Resistance Welding for Aerospace Applications |
| AWS D17.3/D17.3M (2016) (Cited in section 4.2.4.6.3) | Specification for Friction Stir Welding of Aluminum Alloys for Aerospace Applications |
| MMPDS-10 (2015) (Cited in section 4.1.8.1, 4.1.8.2, and 4.2.4.1) | Metallic Materials Properties Development and Standardization (MMPDS) |
| SAE AMS2488D (2000, Reaffirmed 2011) (Cited in section 4.2.2.3.2) | Anodic Treatment - Titanium and Titanium Alloys Solution, pH 13 or Higher |
| SAE AMS2491F (2015) (Cited in section 4.2.3.10) | Surface Treatment of Polytetrafluoroethylene, Preparation for Bonding |
| SAE AMS2680C (2001, Reaffirmed 2010) (Cited in section 4.2.4.6.1) | Electron-Beam Welding for Fatigue Critical Applications |
| SAE AMS2759E (2008, Reaffirmed 2014) (Cited in section 4.2.4.1) | Heat Treatment of Steel Parts, General Requirements |
| SAE AMS2759/9D (2009) (Cited in sections 4.2.6.4) | Hydrogen Embrittlement Relief (Baking) of Steel Parts |
| SAE AMS2770N (2015) (Cited in section 4.2.4.1) | Heat Treatment of Wrought Aluminum Alloy Parts |
| SAE AMS2771E (2013) (Cited in section 4.2.4.1) | Heat Treatment of Aluminum Alloy Castings |
| SAE AMS2772G (2016) (Cited in section 4.2.4.1) | Heat Treatment of Aluminum Alloy Raw Materials |
| SAE AMS2773E (2013) (Cited in section 4.2.4.1) | Heat Treatment, Cast Nickel Alloy and Cobalt Alloy Parts |
| SAE AMS2774E (2016) (Cited in section 4.2.4.1) | 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) | Heat Treatment of Titanium Alloy Parts |
| SAE AMS-H-6875B (2010) (Cited in 4.2.4.1) | Heat Treatment of Steel Raw Materials |
| SAE AMS-H-81200D (2014) (Cited in sections 4.2.4.1 and 4.2.4.6.1) | Heat Treatment of Titanium and Titanium Alloys |
| SAE AMS-STD-401 (1999) (Cited in section 4.2.6.2) | Sandwich Constructions and Core Materials: General Test Methods |
| SAE AS22759C (2014) (Cited in section 4.2.1.5) | Wire, Electrical, Fluoropolymer-Insulated, Copper or Copper Alloy |
| SAE CMH-17-1G (2012) (Cited in section 4.1.8.1) | 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) | Composite Materials Handbook Volume 2 - Polymer Matrix Composites Materials Properties |
| SAE CMH-17-3G (2012) (Cited in section 4.1.8.1) | 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) | 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) | Composite Materials Handbook Volume 5 - Ceramic Matrix Composites |
| SAE CMH-17-6 (2013) (Cited in section 4.1.8.1) | Composite Materials Handbook Volume 6 – Structural Sandwich Composites |