E.1 Purpose and/or Scope
The purpose of this appendix is to provide reference material for background information only. The referenced sections below refer to this NASA Technical Standard. In case of conflict, refer to paragraph 2.4.
E.2 Reference Documents
DOT/FAA/AR-03/19 (Reference Section 4.1.8.1): 1=Material Qualification and Equivalency for Polymer Matrix Composite Material Systems: Updated Procedure NASA NPR 8020.12 (Reference section 4.2.6.7): 1=Planetary Protection Provisions for Robotic Extraterrestrial Missions NASA-STD-5012 (Reference section 4.1.8.1): 1=Strength and Life Assessment Requirements for Liquid-Fueled Space Propulsion System Engines NASA-STD-5019 (Reference sections 4.1.8.1 and 4.1.8.2): 1=Fracture Control Requirements for Spaceflight Hardware NASA/CR-2005- 213424 (Reference section 4.2.3.4): 1=Lubrication for Space Applications NASA-STD-5005 (Revision D or later) (Reference section 4.0): 1=Standard for the Design and Fabrication of Ground Support Equipment NASA/TM-2007- 213740 (2007) (Reference section 4.2.1.4): 1=Guide for Oxygen Compatibility Assessments on Oxygen Components and Systems
DESCRIPTION/USE:
- The Additively Manufactured Hardware Manufacturing and Qualification Plan shall address the manufacturing process controls and hardware qualification process implemented to ensure repeatable manufacture of additively manufactured (AM) structural hardware with consistent structural properties.
- DISTRIBUTION: As determined by the Contracting Officer.
- INITIAL SUBMISSION: PDR
- SUBMISSION FREQUENCY: The contractor may submit updates/revisions at any time.
- REMARKS:
- INTERRELATIONSHIP:
- DATA PREPARATION INFORMATION: