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chunk | NASA-STD-6030 | ADDITIVE MANUFACTURING REQUIREMENTS FOR SPACEFLIGHT SYSTEMS | 2021-04-21 | 5281069358c2b06541ae0d396432906eb066e7933957a77ab913b3851d837588 | 2021-04-21_nasa-std-6030-approveddocx:00000 | 0 |
APPROVED FOR PUBLIC RELEASE—DISTRIBUTION IS UNLIMITED
METRIC/SI (ENGLISH)
NASA TECHNICAL STANDARD
Office of the NASA Chief Engineer
NASA-STD-6030
Approved: 2021-04-21
ADDITIVE MANUFACTURING REQUIREMENTS
FOR SPACEFLIGHT SYSTEMS
NASA-STD-6030
APPROVED FOR PUBLIC REL... | 1,024 | o200k_base | 1,024 | 128 | -1 | -1 | |||||||
chunk | NASA-STD-6030 | ADDITIVE MANUFACTURING REQUIREMENTS FOR SPACEFLIGHT SYSTEMS | 2021-04-21 | 5281069358c2b06541ae0d396432906eb066e7933957a77ab913b3851d837588 | 2021-04-21_nasa-std-6030-approveddocx:00001 | 1 | planned Interruptions ................................................................................................... 47
NASA-STD-6030
APPROVED FOR PUBLIC RELEASE—DISTRIBUTION IS UNLIMITED
5 of 190
TABLE OF CONTENTS (Continued)
SECTION PAGE
4.8 Nondestructive Evaluation (NDE) ....................... | 1,024 | o200k_base | 1,024 | 128 | -1 | -1 | |||||||
chunk | NASA-STD-6030 | ADDITIVE MANUFACTURING REQUIREMENTS FOR SPACEFLIGHT SYSTEMS | 2021-04-21 | 5281069358c2b06541ae0d396432906eb066e7933957a77ab913b3851d837588 | 2021-04-21_nasa-std-6030-approveddocx:00002 | 2 | 8.5 Build Execution .............................................................................................................. 142
8.6 Control of Digital Thread for Part Production ................................................................ 142
NASA-STD-6030
APPROVED FOR PUBLIC RELEASE—DISTRIBUT... | 1,024 | o200k_base | 1,024 | 128 | -1 | -1 | |||||||
chunk | NASA-STD-6030 | ADDITIVE MANUFACTURING REQUIREMENTS FOR SPACEFLIGHT SYSTEMS | 2021-04-21 | 5281069358c2b06541ae0d396432906eb066e7933957a77ab913b3851d837588 | 2021-04-21_nasa-std-6030-approveddocx:00003 | 3 | . This NASA Technical Standard is also intended to cover in-space AM operations;
however, significant tailoring of these requirements is expected.
AM parts used in interfacing ground support equipment (GSE) or test equipment are covered by
the requirements of this NASA Technical Standard only to the extent requi... | 1,024 | o200k_base | 1,024 | 128 | -1 | -1 | |||||||
chunk | NASA-STD-6030 | ADDITIVE MANUFACTURING REQUIREMENTS FOR SPACEFLIGHT SYSTEMS | 2021-04-21 | 5281069358c2b06541ae0d396432906eb066e7933957a77ab913b3851d837588 | 2021-04-21_nasa-std-6030-approveddocx:00004 | 4 | ant engineering organization (CEO)
responsible for development and implementation of the AM parts. The AMCP also defines how
the QMS(s) is(are) integrated throughout the process. Key points of QMS integration are
illustrated with a green triangle symbol in Figure 2. The AMCP and the QMS govern the
engineering and q... | 1,024 | o200k_base | 1,024 | 128 | -1 | -1 | |||||||
question | NASA-STD-6030 | ADDITIVE MANUFACTURING REQUIREMENTS FOR SPACEFLIGHT SYSTEMS | 2021-04-21 | 5281069358c2b06541ae0d396432906eb066e7933957a77ab913b3851d837588 | 0 | 0 | o200k_base | 1,024 | 128 | -1 | -1 | Q-NASA-STD-6030-00000-93456cda | What exact date (YYYY-MM-DD) is listed as the approval date for NASA-STD-6030? | 2021-04-21_nasa-std-6030-approveddocx:00000 | ||||||
question | NASA-STD-6030 | ADDITIVE MANUFACTURING REQUIREMENTS FOR SPACEFLIGHT SYSTEMS | 2021-04-21 | 5281069358c2b06541ae0d396432906eb066e7933957a77ab913b3851d837588 | 1 | 0 | o200k_base | 1,024 | 128 | -1 | -1 | Q-NASA-STD-6030-00001-b23f9300 | What page number marks the beginning of the "MATERIAL PROPERTY SUITE (MPS)" section in this table of contents? | 2021-04-21_nasa-std-6030-approveddocx:00001 | ||||||
question | NASA-STD-6030 | ADDITIVE MANUFACTURING REQUIREMENTS FOR SPACEFLIGHT SYSTEMS | 2021-04-21 | 5281069358c2b06541ae0d396432906eb066e7933957a77ab913b3851d837588 | 2 | 0 | o200k_base | 1,024 | 128 | -1 | -1 | Q-NASA-STD-6030-00002-f926d1ea | Under what specific condition are additive-manufactured parts used on interfacing ground support or test equipment included within the scope of this NASA Technical Standard? | 2021-04-21_nasa-std-6030-approveddocx:00002 | ||||||
question | NASA-STD-6030 | ADDITIVE MANUFACTURING REQUIREMENTS FOR SPACEFLIGHT SYSTEMS | 2021-04-21 | 5281069358c2b06541ae0d396432906eb066e7933957a77ab913b3851d837588 | 3 | 0 | o200k_base | 1,024 | 128 | -1 | -1 | Q-NASA-STD-6030-00003-0102060f | How many verifiable requirement statements—designated “AMR” and indicated by the word “shall”—does this NASA Technical Standard contain? | 2021-04-21_nasa-std-6030-approveddocx:00003 | ||||||
question | NASA-STD-6030 | ADDITIVE MANUFACTURING REQUIREMENTS FOR SPACEFLIGHT SYSTEMS | 2021-04-21 | 5281069358c2b06541ae0d396432906eb066e7933957a77ab913b3851d837588 | 4 | 0 | o200k_base | 1,024 | 128 | -1 | -1 | Q-NASA-STD-6030-00004-d7abc72e | According to the excerpt, the Material Property Suite (MPS) concept is composed of how many distinct entities? | 2021-04-21_nasa-std-6030-approveddocx:00004 |
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