3 Quality assurance 㸦 ရ㉁ಖド㸧
3.2 Quality requirements 㸦ရ㉁せồ㡯㸧
3.2.1 Request for HVI testing of materials㸦㉸㧗㏿⾪✺ヨ㦂ࡢᮦᩱ࠾ࡅࡿせồ㸧
The customer shall issue a request to a hypervelocity impact facilities to test the materials. The request for testing of materials shall specify :
㢳ᐈࡣ㸪ᮦᩱࢆヨ㦂ࡍࡿࡓࡵ㉸㧗㏿⾪✺タせồࢆฟࡍࡶࡢࡍࡿ㸬ᮦᩱヨ㦂࠾ࡅࡿせồࡣ௨ୗࢆ‶
ࡓࡍࡶࡢࡍࡿ㸬
- objective of the test activity,
- background and justification to the test activity, - material to be investigated,
- description of test activity - deliverables.
- ヨ㦂άືࡢ┠ⓗ
- ヨ㦂άືࡢ⫼ᬒព⩏
- ◊✲ࡉࢀࡿᮦᩱ
- ヨ㦂άືࡢㄝ᫂
- ᥦฟ᭩㢮
3.2.2 Work proposal for HVI testing of materials㸦㉸㧗㏿⾪✺ヨ㦂ࡢᮦᩱ࠾ࡅࡿ◊✲ᥦ㸧 The test facility shall issue a work proposal for testing of materials. The work proposal shall specify : ヨ㦂タࡣ㸪ᮦᩱヨ㦂࠾ࡅࡿ◊✲ᥦࢆฟࡍࡶࡢࡍࡿ㸬◊✲ᥦࡣ௨ୗࢆ‶ࡓࡍࡶࡢࡍࡿ㸬
- test objective,
- test method and reference to test standards, - material,
- description of proposed test procedure, - deliverables,
- work breakdown structure, - planning and time schedule, - itemized cost list and payment.
- ᐇ㦂┠ⓗ
- ᐇ㦂᪉ἲヨ㦂つ᱁ࡢᣦ♧
- ᮦᩱ
- ᥦࡉࢀࡓᐇ㦂ᡭ㡰ࡢㄝ᫂
- ᥦฟ᭩㢮
- సᴗᵓᡂ᫂⣽
[II-1]
䛂㻵㻿㻻㻌㻝㻝㻞㻞㻣㻌㻿㼜㼍㼏㼑㻌㼟㼥㼟㼠㼑㼙㼟㻌̿㻌㼀㼑㼟㼠㻌㼜㼞㼛㼏㼑㼐㼡㼞㼑㻌㼠㼛㻌㼑㼢㼍㼘㼡㼍㼠㼑㻌㼟㼜㼍㼏㼑㼏㼞㼍㼒㼠㻌㼙㼍㼠㼑㼞㼕㼍㼘㻌㼑㼖㼑㼏㼠㼍㻌㼡㼜㼛㼚㻌㼔㼥㼜㼑㼞㼢㼑㼘㼛㼏㼕㼠㼥㻌㼕㼙㼜㼍㼏㼠 䠄Ᏹᐂ䝅䝇䝔䝮̿㉸㧗㏿ᗘ⾪✺䛻㉳ᅉ䛩䜛Ᏹᐂᶵᮦᩱ䜲䝆䜵䜽䝍ホ౯䛾䛯䜑䛾ヨ㦂ᡭ㡰䠅䛃
䛻ᇶ䛵䛟ヨ㦂⨨㍑ṇཬ䜃㼑㼖㼑㼏㼠㼍ホ౯ヨ㦂
㻣㻝
[ϩ-1]
- ィ⏬ࢱ࣒ࢫࢣࢪ࣮ࣗࣝ
- 㡯┠ู⤒㈝ࣜࢫࢺᨭᡶ࠸
3.2.3 Calibration㸦㍑ṇヨ㦂㸧
In addition to the calibration test specified in Clause 5, the test facility shall carry out and maintain calibration of test equipment throughout the duration of the test activity. Calibration records shall be readily accessible and retrievable for the entire duration of the test activity on customer request.
5 ❶࡛ᣦᐃࡉࢀࡓ㍑ṇヨ㦂ຍ࠼࡚㸪ヨ㦂タࡣ㸪ヨ㦂άືᮇ㛫୰ࡢᐇ㦂ᶵᮦࡢ㍑ṇࢆ⾜࠸㸪⥔ᣢࡍࡿࡶࡢ
ࡍࡿ㸬㍑ṇࡢグ㘓ࡣ㸪㢳ᐈࡢせồᛂࡌ࡚ヨ㦂άືࡢᮇ㛫࠾࠸࡚ࡍࡄ⏝ࡋࡸࡍࡃ㸪᳨⣴࡛ࡁࡿࡶ
ࡢࡍࡿ㸬
3.2.4 Testing, evaluation and reporting㸦ヨ㦂㸪ホ౯㸪ሗ࿌㸧
The test facility shall provide evidence that the test activity, evaluation and reporting is carried out in accordance with the requirements listed in Clauses 5, 6 and 7, respectively.
ヨ㦂タࡣ㸪ヨ㦂άື㸪ホ౯ሗ࿌ࡀ㸪5㸪6㸪7 ❶ࡑࢀࡒࢀ࡛グ㍕ࡉࢀࡓせ௳ࡋࡓࡀࡗ࡚⾜ࢃࢀࡿ࠸࠺
ドᣐࢆ࠼ࡿࡶࡢࡍࡿ㸬
3.2.5 Traceability and records㸦ࢺ࣮ࣞࢧࣅࣜࢸグ㘓㸧
Materials shall be durably marked to unequivocally identify manufacturer’s code, batch number, material standard designation.
Specimens shall be durably marked to unequivocally identify individual specimens.
The test facility shall maintain test records for the entire duration of the contract.
Test records shall be accessible and retrievable on customer request.
Storage of materials and specimens by the test facility shall be agreed with the customer.
Disposal of materials and specimens shall be authorized by the customer.
ᮦᩱࡣ㸪〇㐀ࢥ࣮ࢻ㸪ࣂࢵࢳࢼࣥࣂ࣮㸪ᮦᩱつ᱁ࡢグྕࢆࡣࡗࡁࡾ☜ㄆࡍࡿࡓࡵỌ⥆ⓗ࣐࣮ࢡࢆࡅ
ࡽࢀࡿࡶࡢࡍࡿ㸬
ヨᩱࡣ㸪ಶࠎࡢヨᩱࢆࡣࡗࡁࡾ☜ㄆࡍࡿࡓࡵỌ⥆ⓗ࣐࣮ࢡࢆࡅࡽࢀࡿࡶࡢࡍࡿ㸬 ヨ㦂タࡣ㸪ዎ⣙ᮇ㛫୰࠾ࡅࡿᐇ㦂グ㘓ࢆ⥔ᣢࡍࡿࡶࡢࡍࡿ㸬
ᐇ㦂グ㘓ࡣ㸪㢳ᐈࡢせồᛂࡌ࡚⏝࡛ࡁ㸪᳨⣴࡛ࡁࡿࡶࡢࡍࡿ㸬 ヨ㦂タࡼࡿヨᩱ࠾ࡼࡧᮦᩱࡢಖᏑࡣ㸪㢳ᐈྠពࡉࢀࡿࡶࡢࡍࡿ㸬 ヨᩱ࠾ࡼࡧᮦᩱࡢฎศࡣ㸪㢳ᐈࡼࡗ࡚チྍࡉࢀࡿࡶࡢࡍࡿ㸬
[II-1]
䛂㻵㻿㻻㻌㻝㻝㻞㻞㻣㻌㻿㼜㼍㼏㼑㻌㼟㼥㼟㼠㼑㼙㼟㻌̿㻌㼀㼑㼟㼠㻌㼜㼞㼛㼏㼑㼐㼡㼞㼑㻌㼠㼛㻌㼑㼢㼍㼘㼡㼍㼠㼑㻌㼟㼜㼍㼏㼑㼏㼞㼍㼒㼠㻌㼙㼍㼠㼑㼞㼕㼍㼘㻌㼑㼖㼑㼏㼠㼍㻌㼡㼜㼛㼚㻌㼔㼥㼜㼑㼞㼢㼑㼘㼛㼏㼕㼠㼥㻌㼕㼙㼜㼍㼏㼠 䠄Ᏹᐂ䝅䝇䝔䝮̿㉸㧗㏿ᗘ⾪✺䛻㉳ᅉ䛩䜛Ᏹᐂᶵᮦᩱ䜲䝆䜵䜽䝍ホ౯䛾䛯䜑䛾ヨ㦂ᡭ㡰䠅䛃
䛻ᇶ䛵䛟ヨ㦂⨨㍑ṇཬ䜃㼑㼖㼑㼏㼠㼍ホ౯ヨ㦂
㻣㻟
➨
➨ϩ̿㸰❶
DIS 11227 ἢࡗࡓྛ✀Ᏹᐂ⏝ᮦᩱࡢホ౯ヨ ヨ㦂
Ᏹᐂ⯟✵◊✲㛤Ⓨᶵᵓ◊✲㛤Ⓨ㈨ᩱ䚷㻶㻭㼄㻭㻙㻾㻹㻙㻝㻡㻙㻜㻜㻤 㻣㻠
[ϩ-2]
ᴫ
ᴫ せ せ
ᮏሗ࿌᭩ࡣISO/TC20/SC14/DIS11227‽ᣐࡋ࡚ᐇࡋࡓᕞᕤᴗᏛ㸭Ᏹᐂ⎔ቃᢏ⾡ࣛ࣎ࣛࢺࣜ
࣮ࡢẁᘧ㍍࢞ࢫ㖠࠾ࡅࡿ㸪Ᏹᐂ⏝ᮦᩱࢆ⏝࠸ࡓᐇ㦂ࡢᐇᡭ㡰ᐇ⤖ᯝࢆࡲࡵࡓࡶࡢ࡛࠶ࡿ㸬
ᐇ㦂ࡣDIS11227ࡢ➨6❶ᚑࡗ࡚ᐇࡋ㸪➨㸵❶ᚑࡗ࡚ሗ࿌ࢆࡲࡵࡓ㸬 ⾲ADIS11227ࡢ➨6
❶࡛せồࡉࢀ࡚࠸ࡿᐇ㦂ᐇࣃ࣓࣮ࣛࢱᮏᐇ㦂࡛タᐃࡋࡓࣃ࣓࣮ࣛࢱࡢẚ㍑ࢆ㸪ࡲࡓ⾲BDIS11227 ࡢ➨7❶࡛せồࡉࢀ࡚࠸ࡿヨ㦂ሗ࿌ࡢෆᐜ㸪ࡑࡢෆᐜᑐᛂࡍࡿᮏ᭩࡛ࡢヱᙜ⟠ᡤ㸦㡯┠␒ྕ㸧ࢆ♧
ࡍ㸬࡞࠾, DIS11227ࡢᐇ㦂ࣃ࣓࣮ࣛࢱࡣᚲ㡲㸦shall㸧᮲௳࡛ࡣ࡞࠸ࡀ,ྍ⬟࡞㝈ࡾ㏆࠸ࡇࡀせㄳ㸦͇
should͇㸧ࡉࢀ࡚࠾ࡾ,ᮏᐇ㦂ࡢ᮲௳ࡶDIS11227ྍ⬟࡞㝈ࡾྠ୍ࡋࡓ㸬
2010ᖺᗘᐇ㦂ࢆᐇࡋࡓ⤖ᯝ㸪ᕞᕤᴗᏛ㸭Ᏹᐂ⎔ቃᢏ⾡ࣛ࣎ࣛࢺ࣮ࣜࡢẁᘧ㍍࢞ࢫ㖠࡛
ISO/TC20/SC14/DIS11227‽ᣐࡋࡓᏱᐂ⏝ᮦᩱࢆ⏝࠸ࡓᐇ㦂ࡢᐇࡀྍ⬟࡛࠶ࡿࡇࢆ☜ㄆࡋࡓ㸬
[II-2]
䛂㻵㻿㻻㻌㻝㻝㻞㻞㻣㻌㻿㼜㼍㼏㼑㻌㼟㼥㼟㼠㼑㼙㼟㻌̿㻌㼀㼑㼟㼠㻌㼜㼞㼛㼏㼑㼐㼡㼞㼑㻌㼠㼛㻌㼑㼢㼍㼘㼡㼍㼠㼑㻌㼟㼜㼍㼏㼑㼏㼞㼍㼒㼠㻌㼙㼍㼠㼑㼞㼕㼍㼘㻌㼑㼖㼑㼏㼠㼍㻌㼡㼜㼛㼚㻌㼔㼥㼜㼑㼞㼢㼑㼘㼛㼏㼕㼠㼥㻌㼕㼙㼜㼍㼏㼠 䠄Ᏹᐂ䝅䝇䝔䝮̿㉸㧗㏿ᗘ⾪✺䛻㉳ᅉ䛩䜛Ᏹᐂᶵᮦᩱ䜲䝆䜵䜽䝍ホ౯䛾䛯䜑䛾ヨ㦂ᡭ㡰䠅䛃
䛻ᇶ䛵䛟ヨ㦂⨨㍑ṇཬ䜃㼑㼖㼑㼏㼠㼍ホ౯ヨ㦂
㻣㻡
[ϩ-2]
⾲
⾲A: DIS11227ࡢ➨6❶࡛せồࡉࢀ࡚࠸ࡿヨ㦂ᐇࣃ࣓࣮ࣛࢱᮏᐇ㦂࡛タᐃࡋࡓࣃ࣓࣮ࣛࢱࡢẚ㍑
㻌
㻌
DIS11227 This study
Projectile
Material Aluminum alloy
A2017 or A2024 A2017
Size and shape 1 mm +/- 0.1 mm
diameter sphere Same
Impact velocity
5 km/sec㻌(or higher) are
recommended 5 km/sec
Target 1
Material Representative of the material to
be flown on the spacecraft Solar array coupon㻌 Size At least 50 mm × 50 mm 100 mm ×㻌100 mm
Thickness Not defined 25mm
Fixing
Held in place by fixing on the edges only
Rear side left free to allow ejecta collection if perforation or rear
side spall occurs
Supported by aluminum plates cut a circular hole (diameter 40 mm) in the
center
Target 2
Material Representative of the material to be flown on the spacecraft
CFRP aluminum honeycomb Size At least 50 mm × 50 mm 100 mm × 150 mm
Thickness 㻌Not defined 25mm
Fixing
Held in place by fixing on the edges only
Rear side left free to allow ejecta collection if perforation or rear
side spall occurs
Supported by aluminum plates cut a circular hole (diameter 40 mm) in the
center
Target 3
Material Representative of the material to
be flown on the spacecraft Aluminum honeycomb Size At least 50 mm × 50 mm 100 mm × 150 mm
Thickness 㻌Not defined 25mm
[II-2]
Ᏹᐂ⯟✵◊✲㛤Ⓨᶵᵓ◊✲㛤Ⓨ㈨ᩱ䚷㻶㻭㼄㻭㻙㻾㻹㻙㻝㻡㻙㻜㻜㻤 㻣㻢
[ϩ-2]
DIS11227ࡢ➨6❶࡛せồࡉࢀ࡚࠸ࡿヨ㦂ᐇࣃ࣓࣮ࣛࢱᮏᐇ㦂࡛タᐃࡋࡓࣃ࣓࣮ࣛࢱࡢẚ㍑