row_type stringclasses 2
values | standard_number stringclasses 2
values | document_title stringclasses 2
values | approval_date stringdate 2020-08-15 00:00:00 2023-06-12 00:00:00 | standard_name stringclasses 1
value | doc_edition stringclasses 2
values | source_url stringclasses 1
value | document_hash stringclasses 2
values | chunk_id stringlengths 0 28 | chunk_index int32 0 4 | chunk_text stringlengths 0 391 | token_count int32 0 97 | tokenizer_name stringclasses 1
value | chunk_size int32 1.02k 1.02k | overlap int32 128 128 | page_start int32 -1 -1 | page_end int32 -1 -1 | section_path stringclasses 1
value | question_id stringlengths 0 36 | question_text stringclasses 6
values | parent_chunk_id stringlengths 0 28 |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
chunk | NASA/SP-2016-6105-Rev2 | FRANGIBILITY AND IMPACT LIMIT REQUIREMENTS | 2023-06-12 | Rev A | 0e0271d3865aab1641fc3cfc6414ae681c3ff1d31d8a30ff40f5e73bb8fa9009 | NASA/SP-2016-6105-Rev2:00000 | 0 | Process review review spaceflight heritage weldment manufacturing article parameter weldment powder flight additive manufacturing spaceflight fracture safety verification. Process fracture traceability porosity component inspection flight review verification component weldment verification microstructure additive weldment spaceflight. | 84 | o200k_base | 1,024 | 128 | -1 | -1 | ||||||
question | NASA/SP-2016-6105-Rev2 | FRANGIBILITY AND IMPACT LIMIT REQUIREMENTS | 2023-06-12 | Rev A | 0e0271d3865aab1641fc3cfc6414ae681c3ff1d31d8a30ff40f5e73bb8fa9009 | 0 | 0 | o200k_base | 1,024 | 128 | -1 | -1 | Q-NASA/SP-2016-6105-Rev2-00000-00-00 | Which requirement applies to fracture control under this standard? | NASA/SP-2016-6105-Rev2:00000 | |||||
question | NASA/SP-2016-6105-Rev2 | FRANGIBILITY AND IMPACT LIMIT REQUIREMENTS | 2023-06-12 | Rev A | 0e0271d3865aab1641fc3cfc6414ae681c3ff1d31d8a30ff40f5e73bb8fa9009 | 0 | 0 | o200k_base | 1,024 | 128 | -1 | -1 | Q-NASA/SP-2016-6105-Rev2-00000-00-01 | Which requirement applies to acceptance testing under this standard? | NASA/SP-2016-6105-Rev2:00000 | |||||
chunk | NASA/SP-2016-6105-Rev2 | FRANGIBILITY AND IMPACT LIMIT REQUIREMENTS | 2023-06-12 | Rev A | 0e0271d3865aab1641fc3cfc6414ae681c3ff1d31d8a30ff40f5e73bb8fa9009 | NASA/SP-2016-6105-Rev2:00001 | 1 | Acceptance parameter manufacturing safety article weldment manufacturing parameter fracture parameter inspection component verification flight microstructure process additive weldment. Qualification additive verification qualification qualification porosity verification manufacturing process additive additive traceability fracture flammability microstructure safety. | 92 | o200k_base | 1,024 | 128 | -1 | -1 | ||||||
question | NASA/SP-2016-6105-Rev2 | FRANGIBILITY AND IMPACT LIMIT REQUIREMENTS | 2023-06-12 | Rev A | 0e0271d3865aab1641fc3cfc6414ae681c3ff1d31d8a30ff40f5e73bb8fa9009 | 1 | 0 | o200k_base | 1,024 | 128 | -1 | -1 | Q-NASA/SP-2016-6105-Rev2-00001-00-00 | Which requirement applies to process qualification under this standard? | NASA/SP-2016-6105-Rev2:00001 | |||||
question | NASA/SP-2016-6105-Rev2 | FRANGIBILITY AND IMPACT LIMIT REQUIREMENTS | 2023-06-12 | Rev A | 0e0271d3865aab1641fc3cfc6414ae681c3ff1d31d8a30ff40f5e73bb8fa9009 | 1 | 0 | o200k_base | 1,024 | 128 | -1 | -1 | Q-NASA/SP-2016-6105-Rev2-00001-00-01 | Which requirement applies to porosity limits under this standard? | NASA/SP-2016-6105-Rev2:00001 | |||||
chunk | NASA/SP-2016-6105-Rev2 | FRANGIBILITY AND IMPACT LIMIT REQUIREMENTS | 2023-06-12 | Rev A | 0e0271d3865aab1641fc3cfc6414ae681c3ff1d31d8a30ff40f5e73bb8fa9009 | NASA/SP-2016-6105-Rev2:00002 | 2 | Microstructure spaceflight fracture inspection inspection heritage additive porosity article nonconformance process manufacturing microstructure porosity powder powder porosity article. Article inspection spaceflight component porosity microstructure manufacturing fracture manufacturing flight safety additive article safety qualification process. | 87 | o200k_base | 1,024 | 128 | -1 | -1 | ||||||
question | NASA/SP-2016-6105-Rev2 | FRANGIBILITY AND IMPACT LIMIT REQUIREMENTS | 2023-06-12 | Rev A | 0e0271d3865aab1641fc3cfc6414ae681c3ff1d31d8a30ff40f5e73bb8fa9009 | 2 | 0 | o200k_base | 1,024 | 128 | -1 | -1 | Q-NASA/SP-2016-6105-Rev2-00002-00-00 | Which requirement applies to powder handling under this standard? | NASA/SP-2016-6105-Rev2:00002 | |||||
question | NASA/SP-2016-6105-Rev2 | FRANGIBILITY AND IMPACT LIMIT REQUIREMENTS | 2023-06-12 | Rev A | 0e0271d3865aab1641fc3cfc6414ae681c3ff1d31d8a30ff40f5e73bb8fa9009 | 2 | 0 | o200k_base | 1,024 | 128 | -1 | -1 | Q-NASA/SP-2016-6105-Rev2-00002-00-01 | Which requirement applies to powder handling under this standard? | NASA/SP-2016-6105-Rev2:00002 | |||||
chunk | NASA/SP-2016-6105-Rev2 | FRANGIBILITY AND IMPACT LIMIT REQUIREMENTS | 2023-06-12 | Rev A | 0e0271d3865aab1641fc3cfc6414ae681c3ff1d31d8a30ff40f5e73bb8fa9009 | NASA/SP-2016-6105-Rev2:00003 | 3 | Inspection manufacturing parameter verification system system flight qualification system safety inspection manufacturing qualification article fracture spaceflight flight acceptance. Acceptance inspection parameter weldment flight process porosity flammability flight traceability heritage article spaceflight acceptance fracture review. | 84 | o200k_base | 1,024 | 128 | -1 | -1 | ||||||
question | NASA/SP-2016-6105-Rev2 | FRANGIBILITY AND IMPACT LIMIT REQUIREMENTS | 2023-06-12 | Rev A | 0e0271d3865aab1641fc3cfc6414ae681c3ff1d31d8a30ff40f5e73bb8fa9009 | 3 | 0 | o200k_base | 1,024 | 128 | -1 | -1 | Q-NASA/SP-2016-6105-Rev2-00003-00-00 | Which requirement applies to fracture control under this standard? | NASA/SP-2016-6105-Rev2:00003 | |||||
question | NASA/SP-2016-6105-Rev2 | FRANGIBILITY AND IMPACT LIMIT REQUIREMENTS | 2023-06-12 | Rev A | 0e0271d3865aab1641fc3cfc6414ae681c3ff1d31d8a30ff40f5e73bb8fa9009 | 3 | 0 | o200k_base | 1,024 | 128 | -1 | -1 | Q-NASA/SP-2016-6105-Rev2-00003-00-01 | Which requirement applies to acceptance testing under this standard? | NASA/SP-2016-6105-Rev2:00003 | |||||
chunk | NASA/SP-2016-6105-Rev2 | FRANGIBILITY AND IMPACT LIMIT REQUIREMENTS | 2023-06-12 | Rev A | 0e0271d3865aab1641fc3cfc6414ae681c3ff1d31d8a30ff40f5e73bb8fa9009 | NASA/SP-2016-6105-Rev2:00004 | 4 | Parameter inspection spaceflight traceability heritage manufacturing verification microstructure flammability article porosity component additive powder fracture heritage parameter article. System safety additive flight spaceflight additive porosity process acceptance flammability fracture flight microstructure powder spaceflight manufacturing. | 86 | o200k_base | 1,024 | 128 | -1 | -1 | ||||||
question | NASA/SP-2016-6105-Rev2 | FRANGIBILITY AND IMPACT LIMIT REQUIREMENTS | 2023-06-12 | Rev A | 0e0271d3865aab1641fc3cfc6414ae681c3ff1d31d8a30ff40f5e73bb8fa9009 | 4 | 0 | o200k_base | 1,024 | 128 | -1 | -1 | Q-NASA/SP-2016-6105-Rev2-00004-00-00 | Which requirement applies to process qualification under this standard? | NASA/SP-2016-6105-Rev2:00004 | |||||
question | NASA/SP-2016-6105-Rev2 | FRANGIBILITY AND IMPACT LIMIT REQUIREMENTS | 2023-06-12 | Rev A | 0e0271d3865aab1641fc3cfc6414ae681c3ff1d31d8a30ff40f5e73bb8fa9009 | 4 | 0 | o200k_base | 1,024 | 128 | -1 | -1 | Q-NASA/SP-2016-6105-Rev2-00004-00-01 | Which requirement applies to porosity limits under this standard? | NASA/SP-2016-6105-Rev2:00004 | |||||
chunk | NPR-8705.2C | MATERIALS AND PROCESSES REQUIREMENTS FOR SPACECRAFT | 2020-08-15 | Rev B | 3b12db8bb249e991dd42549d35ac8d9f61c6903df34c62f6e6b0863aff26f95b | NPR-8705.2C:00000 | 0 | Process qualification fracture safety traceability traceability verification traceability acceptance component additive qualification nonconformance system acceptance powder nonconformance flammability. Article process parameter component parameter porosity heritage fracture parameter system traceability process manufacturing microstructure powder fracture. | 89 | o200k_base | 1,024 | 128 | -1 | -1 | ||||||
question | NPR-8705.2C | MATERIALS AND PROCESSES REQUIREMENTS FOR SPACECRAFT | 2020-08-15 | Rev B | 3b12db8bb249e991dd42549d35ac8d9f61c6903df34c62f6e6b0863aff26f95b | 0 | 0 | o200k_base | 1,024 | 128 | -1 | -1 | Q-NPR-8705.2C-00000-01-00 | Which requirement applies to acceptance testing under this standard? | NPR-8705.2C:00000 | |||||
question | NPR-8705.2C | MATERIALS AND PROCESSES REQUIREMENTS FOR SPACECRAFT | 2020-08-15 | Rev B | 3b12db8bb249e991dd42549d35ac8d9f61c6903df34c62f6e6b0863aff26f95b | 0 | 0 | o200k_base | 1,024 | 128 | -1 | -1 | Q-NPR-8705.2C-00000-01-01 | Which requirement applies to acceptance testing under this standard? | NPR-8705.2C:00000 | |||||
chunk | NPR-8705.2C | MATERIALS AND PROCESSES REQUIREMENTS FOR SPACECRAFT | 2020-08-15 | Rev B | 3b12db8bb249e991dd42549d35ac8d9f61c6903df34c62f6e6b0863aff26f95b | NPR-8705.2C:00001 | 1 | Acceptance flammability nonconformance porosity additive parameter qualification inspection parameter nonconformance spaceflight weldment additive porosity parameter safety spaceflight process. Porosity system porosity fracture parameter nonconformance microstructure acceptance additive component weldment powder flight manufacturing spaceflight acceptance. | 89 | o200k_base | 1,024 | 128 | -1 | -1 | ||||||
question | NPR-8705.2C | MATERIALS AND PROCESSES REQUIREMENTS FOR SPACECRAFT | 2020-08-15 | Rev B | 3b12db8bb249e991dd42549d35ac8d9f61c6903df34c62f6e6b0863aff26f95b | 1 | 0 | o200k_base | 1,024 | 128 | -1 | -1 | Q-NPR-8705.2C-00001-01-00 | Which requirement applies to fracture control under this standard? | NPR-8705.2C:00001 | |||||
question | NPR-8705.2C | MATERIALS AND PROCESSES REQUIREMENTS FOR SPACECRAFT | 2020-08-15 | Rev B | 3b12db8bb249e991dd42549d35ac8d9f61c6903df34c62f6e6b0863aff26f95b | 1 | 0 | o200k_base | 1,024 | 128 | -1 | -1 | Q-NPR-8705.2C-00001-01-01 | Which requirement applies to porosity limits under this standard? | NPR-8705.2C:00001 | |||||
chunk | NPR-8705.2C | MATERIALS AND PROCESSES REQUIREMENTS FOR SPACECRAFT | 2020-08-15 | Rev B | 3b12db8bb249e991dd42549d35ac8d9f61c6903df34c62f6e6b0863aff26f95b | NPR-8705.2C:00002 | 2 | Article spaceflight safety inspection flammability article verification spaceflight porosity safety parameter weldment review additive traceability article verification manufacturing. Inspection safety powder qualification process additive additive weldment parameter verification porosity nonconformance traceability nonconformance qualification microstructure. | 90 | o200k_base | 1,024 | 128 | -1 | -1 | ||||||
question | NPR-8705.2C | MATERIALS AND PROCESSES REQUIREMENTS FOR SPACECRAFT | 2020-08-15 | Rev B | 3b12db8bb249e991dd42549d35ac8d9f61c6903df34c62f6e6b0863aff26f95b | 2 | 0 | o200k_base | 1,024 | 128 | -1 | -1 | Q-NPR-8705.2C-00002-01-00 | Which requirement applies to porosity limits under this standard? | NPR-8705.2C:00002 | |||||
question | NPR-8705.2C | MATERIALS AND PROCESSES REQUIREMENTS FOR SPACECRAFT | 2020-08-15 | Rev B | 3b12db8bb249e991dd42549d35ac8d9f61c6903df34c62f6e6b0863aff26f95b | 2 | 0 | o200k_base | 1,024 | 128 | -1 | -1 | Q-NPR-8705.2C-00002-01-01 | Which requirement applies to process qualification under this standard? | NPR-8705.2C:00002 | |||||
chunk | NPR-8705.2C | MATERIALS AND PROCESSES REQUIREMENTS FOR SPACECRAFT | 2020-08-15 | Rev B | 3b12db8bb249e991dd42549d35ac8d9f61c6903df34c62f6e6b0863aff26f95b | NPR-8705.2C:00003 | 3 | Powder safety nonconformance powder microstructure powder system article nonconformance porosity acceptance safety inspection spaceflight acceptance process qualification porosity. Flight microstructure review flammability heritage inspection flight powder microstructure weldment article additive powder traceability verification review. | 84 | o200k_base | 1,024 | 128 | -1 | -1 | ||||||
question | NPR-8705.2C | MATERIALS AND PROCESSES REQUIREMENTS FOR SPACECRAFT | 2020-08-15 | Rev B | 3b12db8bb249e991dd42549d35ac8d9f61c6903df34c62f6e6b0863aff26f95b | 3 | 0 | o200k_base | 1,024 | 128 | -1 | -1 | Q-NPR-8705.2C-00003-01-00 | Which requirement applies to fracture control under this standard? | NPR-8705.2C:00003 | |||||
question | NPR-8705.2C | MATERIALS AND PROCESSES REQUIREMENTS FOR SPACECRAFT | 2020-08-15 | Rev B | 3b12db8bb249e991dd42549d35ac8d9f61c6903df34c62f6e6b0863aff26f95b | 3 | 0 | o200k_base | 1,024 | 128 | -1 | -1 | Q-NPR-8705.2C-00003-01-01 | Which requirement applies to fracture control under this standard? | NPR-8705.2C:00003 | |||||
chunk | NPR-8705.2C | MATERIALS AND PROCESSES REQUIREMENTS FOR SPACECRAFT | 2020-08-15 | Rev B | 3b12db8bb249e991dd42549d35ac8d9f61c6903df34c62f6e6b0863aff26f95b | NPR-8705.2C:00004 | 4 | Verification manufacturing weldment manufacturing parameter porosity manufacturing article qualification verification fracture qualification porosity article parameter fracture powder acceptance. Microstructure flight additive microstructure fracture porosity nonconformance verification heritage nonconformance nonconformance inspection traceability verification microstructure spaceflight. | 97 | o200k_base | 1,024 | 128 | -1 | -1 | ||||||
question | NPR-8705.2C | MATERIALS AND PROCESSES REQUIREMENTS FOR SPACECRAFT | 2020-08-15 | Rev B | 3b12db8bb249e991dd42549d35ac8d9f61c6903df34c62f6e6b0863aff26f95b | 4 | 0 | o200k_base | 1,024 | 128 | -1 | -1 | Q-NPR-8705.2C-00004-01-00 | Which requirement applies to powder handling under this standard? | NPR-8705.2C:00004 | |||||
question | NPR-8705.2C | MATERIALS AND PROCESSES REQUIREMENTS FOR SPACECRAFT | 2020-08-15 | Rev B | 3b12db8bb249e991dd42549d35ac8d9f61c6903df34c62f6e6b0863aff26f95b | 4 | 0 | o200k_base | 1,024 | 128 | -1 | -1 | Q-NPR-8705.2C-00004-01-01 | Which requirement applies to fracture control under this standard? | NPR-8705.2C:00004 |
README.md exists but content is empty.
- Downloads last month
- 6