MUAs shall be submitted as described below. Category I MUAs – Category I MUAs are those that involve material/processes usage that could affect the safety of the mission, crew, or vehicle or affect the mission success, but must be used for functional reasons. Approval by the responsible NASA Materials and Processes organization and the NASA Program/Project Office shall be required.
Category II MUAs - Category II MUAs are those that involve material/processes usage that fails a screening of Materials and Processes requirements and is not considered a hazard in its use application but for which no Category III rationale code exists. Approval by the responsible NASA Materials and Processes organization shall be required.
Category III MUAs – Category III MUAs are those that involve materials or processes that have not been shown to meet these requirements but have an approved rationale code
| 1 | 2 | |
|---|---|---|
| 1.0 | PROGRAM: | 2. DRD NO.: XXXX |
| 3.0 | DATA TYPE: 1 (Category I and II MUAs) | 4. DATE REVISED: |
| 2 (Category III MUAs) | 5. PAGE: 1 | |
| 6.0 | TITLE: Materials Usage Agreements (MUAs) | TITLE: Materials Usage Agreements (MUAs) |
NASA-STD-6016B
listed in the hardware developer-approved Materials and Processes Selection, Control, and Implementation Plan. They are evaluated and determined to be acceptable at the configuration/part level. Category III MUAs shall be reported in the Materials Identification and Usage List (MIUL) system or electronic data system utilizing the approved rationale codes in the Materials and Processes Selection, Control, and Implementation Plan. No MUA form is submitted. [Category III MUAs are identified here for completeness but are not required until after PDR.]
13.1
SCOPE:
The Contamination Control Plan shall be generated in accordance with the guidelines of ASTM E1548, Standard Practice for Preparation of Aerospace Contamination Control Plans (as specified by NASA-STD-6016A) and shall include:
- a. A Foreign Object Debris (FOD) Control Plan to prevent damage to spaceflight hardware and injury to the flight crew by FOD during manufacture, assembly, test, transportation, storage, launch site processing, operation, repair, modification, refurbishment, and maintenance. The FOD prevention program shall conform to NAS 412, Foreign Object Damage/Foreign Object Debris (FOD) Prevention, as specified by NASA-STD-6016A.
- b. Definition of cleanliness level acceptance limits and verification methods for fluid systems, and for general spaceflight hardware internal and external surfaces. The Plan shall also contain a list identifying all system fluids, together with the fluid specifications (for procurement or custom mixing) and the required cleanliness levels for the fluid system.
DATA REQUIREMENTS DESCRIPTION (DRD)
PROGRAM:
2. DRD NO.: XXXX
3.
DATA TYPE: 2
4. DATE REVISED:
- PAGE: 1
TITLE: Contamination Control Plan (CCP)
DESCRIPTION/USE: The Contamination Control Plan defines implementation measures to control contamination of spaceflight hardware and fluid systems during manufacturing, assembly, test, transportation, storage, launch site processing, and post-flight refurbishment.
DISTRIBUTION: As determined by the Contracting Officer.
INITIAL SUBMISSION: PDR
SUBMISSION FREQUENCY: The contractor may submit updates/revisions at any time. Final submission shall be at CDR.
REMARKS:
INTERRELATIONSHIP: Parent SOW Paragraph: XXXX
DATA PREPARATION INFORMATION:
13.1
SCOPE:
The Contamination Control Plan shall be generated in accordance with the guidelines of
ASTM E1548, Standard Practice for Preparation of Aerospace Contamination Control
Plans (as specified by NASA-STD-6016A) and shall include:
a. A Foreign Object Debris (FOD) Control Plan to prevent damage to spaceflight hardware and injury to the flight crew by FOD during manufacture, assembly, test, transportation, storage, launch site processing, operation, repair, modification, refurbishment, and maintenance. The FOD prevention program shall conform to NAS 412, Foreign Object Damage/Foreign Object Debris (FOD) Prevention, as specified by NASA-STD-6016A.
b. Definition of cleanliness level acceptance limits and verification methods for fluid systems, and for general spaceflight hardware internal and external surfaces. The Plan shall also contain a list identifying all system fluids, together with the fluid specifications (for procurement or custom mixing) and the required cleanliness levels for the fluid system.
NASA-STD-6016B
13.1
SCOPE:
The NDE Plan shall address the process for establishment, implementation, execution, and control of NDE. The Plan shall meet the intent of MIL-HDBK-6870, Inspection Program Requirements, Nondestructive for Aircraft and Missile Materials and Parts, and the requirements of NASA-STD-5009, Nondestructive Evaluation Requirements for Fracture-Critical Metallic Components as specified by NASA-STD-6016A, Standard Materials and Processes Requirements for Spacecraft.
13.1
SCOPE:
The Additively Manufactured Hardware Manufacturing and Qualification Plan shall address the process for manufacture and verification of materials properties for AM structural hardware.