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NASA-STD-6016 REV B

STANDARD MATERIALS AND PROCESSES REQUIREMENTS FOR SPACECRAFT

active, Most Current
Organization: NASA
Publication Date: 14 May 2020
Status: active
Page Count: 155
scope:

This NASA Technical Standard is directed toward materials and processes (M&P) used in the design, fabrication, and testing of space program flight hardware for NASA, including but not limited to crewed, uncrewed, robotic, launch vehicle, lander, in-space and surface systems, and spacecraft program/project hardware elements. All spaceflight hardware is covered by the M&P requirements of this document, including vendor-designed, off-the-shelf, and vendor-furnished items.

M&P used in interfacing ground support equipment (GSE), test equipment, hardware processing equipment, hardware packaging, and hardware shipment is covered by the M&P requirements of this NASA Technical Standard only to the extent required to prevent damage to or contamination of spaceflight hardware (see Section 4.0). M&P used in NASA aircraft and aircraft operations are not covered by the M&P requirements of this document.

Purpose

The purpose of this NASA Technical Standard is to define the minimum requirements for M&P and to provide a general control specification for incorporation in NASA program/project hardware procurements and technical programs.

Applicability

The controls described here are applicable to all NASA spacecraft programs:

a. [MPR 1] Programs shall apply these controls to program/project hardware. Programs, projects, and elements are responsible for flowing requirements down to contractors, subcontractors, and the lowest component-level suppliers.

b. [MPR 2] Programs shall be responsible for demonstrating compliance with these requirements.

This NASA Technical Standard is approved for use by NASA Headquarters and NASA Centers and Facilities and may be cited in contract, program, and other Agency documents as a technical requirement. It may also apply to the Jet Propulsion Laboratory and other contractors only to the extent specified or referenced in applicable contracts.

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.

Verifiable requirement statements are numbered and indicated by the word "shall" beginning in section 4; this NASA Technical Standard contains 212 requirements. Explanatory or guidance text is indicated in italics beginning in section 4. To facilitate requirements selection and verification by NASA programs and projects, a Requirements Compliance Matrix is provided in Appendix A. This appendix also contains justifications for each verifiable requirement statement.

Tailoring

a. [MPR 3] Tailoring of this NASA Technical Standard's requirements in the Materials and Processes Selection, Control, and Implementation Plan for specific programs/projects shall be formally documented as part of program or project requirements and approved by the responsible program/project NASA M&P organization, the responsible project/program, and the responsible Technical Authority in accordance with NPR 7120.5, NASA Space Flight Program and Project Management Requirements, or NPR 7120.8, NASA Research and Technology Program and Project Management Requirements. These requirements may be tailored simply by constructing a matrix of applicable paragraphs and paragraphs that are not applicable. Tailoring also includes using existing or previously developed contractor processes and standards as a submittal of the various required plans. Otherwise, the tailoring of requirements may be documented in the Materials and Processes Selection, Control, and Implementation Plan by providing the degree of conformance and the method of implementation for each requirement identified here.

b. When a Materials and Processes Selection, Control, and Implementation Plan has been approved by the responsible program/project as an acceptable means of compliance with the technical requirements of this NASA Technical Standard, the Plan may be used for the implementation and verification of M&P requirements on the applicable program/project.

Document History

NASA-STD-6016 REV B
May 14, 2020
STANDARD MATERIALS AND PROCESSES REQUIREMENTS FOR SPACECRAFT
This NASA Technical Standard is directed toward materials and processes (M&P) used in the design, fabrication, and testing of space program flight hardware for NASA, including but not limited to...
November 30, 2016
STANDARD MATERIALS AND PROCESSES REQUIREMENTS FOR SPACECRAFT
This NASA Technical Standard is directed toward materials and processes (M&P) used in the design, fabrication, and testing of space program flight hardware for NASA, including but not limited to...
July 11, 2008
STANDARD MATERIALS AND PROCESSES REQUIREMENTS FOR SPACECRAFT
This document is directed toward materials and processes (M&P) used in the design, fabrication, and testing of flight components for all NASA manned, unmanned, robotic, launch vehicle, lander,...
September 11, 2006
STANDARD MATERIALS AND PROCESSES REQUIREMENTS FOR SPACECRAFT
This document is directed toward Materials and Processes (M&P) used in the design, fabrication, and testing of flight components for all NASA manned, unmanned, robotic, launch vehicle, lander,...

References

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