The documents listed in this section contain provisions that constitute requirements of this NASA Technical Standard as cited in the text.
2.1.1
[MPR 4] The latest issuances of cited documents shall apply unless specific versions are designated.
2.1.2
[MPR 5] Non-use of specifically designated versions shall be approved by the responsible Technical Authority.
The applicable documents are accessible at https://standards.nasa.gov, may be obtained directly from the Standards Developing Body or other document distributors, or information for obtaining the document is provided.
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
MSFC-SPEC-445A (1990) (Cited in section 4.2.4.5): 1=Adhesive Bonding, Process and Inspection, Requirements for MSFC-STD-3029A (2005) (Cited in section 4.2.2): 1=Guidelines for the Selection of Metallic Materials for Stress Corrosion Cracking Resistance in Sodium Chloride Environments MIL-STD-810G (2008), with Change 1 (2014) (Cited in section 4.2.3.8): 1=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): 1=Inertia Friction Welding Process, Procedure and Performance Qualification MIL-HDBK-6870B (2012) (Cited in section 4.2.5.1): 1=Nondestructive Inspection Program Requirements for Aircraft and Missile Materials and Parts