13.5

7. DESCRIPTION/USE: MUAs shall be submitted for all materials and processes that are technically acceptable but do not meet the technical requirements of NASA-STD-6016A, as implemented by the approved Materials and Processes Selection, Control, and Implementation Plan. [The use of materials and processes that do not comply with the technical requirements of this standard may be technically acceptable if hardware reliability and vehicle safety are not affected.]
8. DISTRIBUTION: As determined by the Contracting Officer.
9. INITIAL SUBMISSION: PDR.
10. SUBMISSION FREQUENCY: At PDR and as the need for new MUAs is identified during the detailed design process. MUAs shall be revised and resubmitted whenever design modifications affect the part numbers or the environment or loads change to more severe than identified on the MUA or the MUA rationale.
11. REMARKS:
12. INTERRELATIONSHIP: Parent SOW Paragraph: XXXX
13. DATA PREPARATION INFORMATION:

13.5

MAINTENANCE: Contractor updates to the Category I and Category II MUAs shall be submitted to NASA for approval. Complete reissue of the MUA is required.

7. DESCRIPTION/USE: The MIUL is an electronic searchable parts list or separate electronic searchable materials identification and usage list. The MIUL identifies all Materials and Processes (M&P) usages contained in the end item, excluding piece part electronics and materials in sealed containers (maximum leak rate less than 1 x 10-4 cm3/sec), for evaluation of the acceptability of M&P selected and utilized.
8. DISTRIBUTION: As determined by the Contracting Officer.
9. INITIAL SUBMISSION: PDR
10. SUBMISSION FREQUENCY: As-designed MIUL – at Hardware Acceptance Review As-built MIUL updates – prior to FRR
11. REMARKS:
12. INTERRELATIONSHIP: Parent SOW Paragraph: XXXX
13. DATA PREPARATION INFORMATION:

13.1

• SCOPE: Materials and processes usage shall be documented in an electronic searchable parts list or separate electronic searchable Materials Identification and Usage List (MIUL). The procedures and formats for documentation of materials and processes usage will depend upon specific hardware but shall cover the as-built hardware. The system used shall be an integral part of the engineering configuration control/release system. A copy of the stored data shall be provided to NASA in a form compatible with the Materials and Processes Technical Information System (MAPTIS).

Wire, cable, and exposed surfaces of connectors shall be reported on the MIUL. All other standard and nonstandard electrical, electronic, and electromechanical (EEE) parts are exempt from reporting on the MIUL. Materials used in hermetically sealed electronic containers (maximum leak rate less than 1 x 10-4 cm3/sec) are also exempt from inclusion in the MIUL.

13.5

MAINTENANCE: Contractor updates to the MIUL shall be submitted to NASA for approval. Complete reissue of the document is not required.

13.5

MAINTENANCE: Changes to the document proposed by the contractor shall be submitted to NASA for approval. Complete reissue of the document is required.

7. DESCRIPTION/USE:

• The Nondestructive Evaluation (NDE) Plan shall address the NDE requirements necessary to assure the health and integrity of the spaceflight hardware throughout its life cycle. This Plan shall identify all Nondestructive Evaluation (NDE) standards employed in the inspection of materials.

8. DISTRIBUTION: As determined by the Contracting Officer.
9. INITIAL SUBMISSION: PDR
10. SUBMISSION FREQUENCY: The contractor may submit updates/revisions at any time.
11. REMARKS:
12. INTERRELATIONSHIP:
13. DATA PREPARATION INFORMATION:

13.5

MAINTENANCE: Changes to the document proposed by the contractor shall be submitted to NASA for approval. Complete reissue of the document is required.

sampling requirements and acceptance criteria; thermal processing; first article evaluations and re-sampling periods; build orientation, platform material, and layout; special cleaning requirements; repair allowance; inspection requirements; critical dimensions; any other factors that affect physical/mechanical properties.

c. Development of process controls on metallurgical process constituents, including the assembled part build file; feedstock controls; chemistry; powder feedstock (including recycled powder); fusion process controls (machine type and operating parameters:
laser power, speed, layer thickness, hatch width, etc.); chamber atmosphere; chamber contamination control; and thermal processing controls.

d. Controls on AM-related equipment, including addressing updates to improve machine performance.

13.4 FORMAT: Electronic, Word®-compatible document or Adobe® PDF.

13.5 MAINTENANCE: Changes to the document proposed by the contractor shall be submitted to NASA for approval. Complete reissue of the document is required.

13.5

MAINTENANCE: Changes to the document proposed by the contractor shall be submitted to NASA for approval. Complete reissue of the document is required.

NASA-TM-86556 (1985) (Reference section 4.2.3.4): Unnamed: 1=Lubrication Handbook for the Space Industry, Part A: Solid Lubricants, Part B: Liquid Lubricants ANSI/AIAA G-095 (Reference section 4.2.6.4): Unnamed: 1=Guide to Safety of Hydrogen and Hydrogen Systems AWS G2.4/G2.4M (Reference section 4.2.4.6.1): Unnamed: 1=Guide for the Fusion Welding of Titanium and Titanium Alloys SAE AMS2453 (Reference section 4.2.2.2.1): Unnamed: 1=Low Stress Grinding of Steel Parts Heat Treated to 180 ksi or Over, and Low Stress Grinding of Chrome Plating Applied to Steel Parts Heat Treated to 180 ksi or Over