NAVY MIL-P-85723 (1)-1991 PROJECTILE 20 MILLIMETER SEMI-ARMOR PIERCING HIGH EXPLOSIVE INCENDIARY PGU-28 B《PGU-28 B型20毫安半精确位置高爆炸指示器射弹》.pdf
《NAVY MIL-P-85723 (1)-1991 PROJECTILE 20 MILLIMETER SEMI-ARMOR PIERCING HIGH EXPLOSIVE INCENDIARY PGU-28 B《PGU-28 B型20毫安半精确位置高爆炸指示器射弹》.pdf》由会员分享,可在线阅读,更多相关《NAVY MIL-P-85723 (1)-1991 PROJECTILE 20 MILLIMETER SEMI-ARMOR PIERCING HIGH EXPLOSIVE INCENDIARY PGU-28 B《PGU-28 B型20毫安半精确位置高爆炸指示器射弹》.pdf(8页珍藏版)》请在麦多课文档分享上搜索。
1、- I I I l l I l 1 I I I I I I I I l I l l l I I l l I 1 I i I t I I l l l I t I I I I I I I I I l I 1 I MIL-P-85723 (1) 13 W 99999Ob OYb78b8 5 = I I NCH-POUND MIL-P-85723(AS) AMENDMENT 1 31 January 1991 MILITARY SPECIFICATION PROJECTILE, 20 MILLIMETER, SEMI-ARMOR PIERCING, HIGH EXPLOSIVE INCENDIARY,
2、 PGU-28/B This amendment forms a part of MIL-P-85723(AS), dated 12 August 1986, and is approved for use by the Naval Air Systems Command, Department of the Navy and is of the Department of Defense. 6.2.11.“ available for use by all Departments and Agencies PAGE 2 t 2.1.1, last line, after “solicitat
3、ion,“ add “(see 2.1 1 , under “MIL-STD-1235“ add “(Un1 ess otherwi se i ndi cated. coDi es of federa and mi 1 i tary specif cations, standards, and handbooks are available from the Standardization Documents Order Desk, Building 4D, 700 Robbins Avenue, Philadelphia, PA 19111-5094.)“ PAGE 3 2.1.2, und
4、er “1575AS109“ add “(Copies of Naval Air Systems Command drawings are available from the Naval Air Technical Services Facility (NATSF) (Code 3121, 700 Robbins Avenue, Philadelphia, PA 191 11-5097.)“ 2.1.2, under “Cepartment of the Army,“ delete “DI1075203“ and substitute “Dl 1075203. II and add “Dl
5、1075245 Production Check Standards (Copies are available from the Department of the Army, U.S. Army Information System Command (ASQNC-APP OPP-P), Picatinny Arsenal, NJ 07806-5000.) 2.1.2, under “US Army Material Command,“below “AMCR 715-505,“delete “(Copies of specifications, standards, drawings, pu
6、bl ications, and other Government documents required by contractors in connection with specific acquisition functions should be obtained from the contracting activity or as directed by the contracting activity.)“ and substitute “(Copies are available from the Commander, USAISC-Letter Kenny, Attn: AS
7、Q-NC-DL-OIP, Chambersburg, PA 17201-4186. I AMSC N/A 1 of 8 FSC 1305 DISTRIBUTION STATEMENT A. Approved for publ ic release; distri bution is un1 imi ted. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-P-85723(AS) AMENDMENT 1 1 PAGE 4 Delete exi
8、sting paragraph 2.2 in its entirety and substitute “2.2 Non-Government publ i cations. The fol lowing document(s1 form a part of this Unless otherwise specified, the issues of documents not listed document to the extent specified herein. Unless otherwise specified, the issues of the documents which
9、are DoD adopted are those listed in the issue of the DODISS cited in the solicitation. in the DODISS are the issues of the documents cited in the solicitation (see 6.2.11.“ 2.2, under “AMERICAN SOCIETY FOR TESTING AND MATERIALS (ASTM)“ delete “ASTM B117-64“ and “ASTM E18-67“ and substi tute “ASTM 81
10、17“ and “ASTM E18“ respectively. 2.2, below “(Application for copies should be addressed to the American Society for Testing and Materials, 1916 Race Street, Philadelphia, PA 19103.)“ add Below “ASTM El 8, II add “ASTM F519 Testing for Hydrogen Embri ttlement Re1 ief .II 1, “(Non-Government standard
11、s and other publ i cations are normal ly avai 1 able from the organizations that prepare or distribute the documents. These documents also may be available in or through libraries or other informational services.)“ PAGE 5 3.3.2.2, third line, delete “serrated.“ 3,3.2.4.1, second line, delete “1575AS
12、101“ and substi tute “1575AS105.“ Delete existing paragraph 3.3.2.4.2 in its entirety and substitute “3.3.2.4.2 Paint coating. The paint coating shall be in accordance with the applicable requirements of Drawing 1575AS105. accordance with appl icable requirements of TT-C-490. be indicated by the exp
13、osure of base metal or underlying phosphate in any of the fol lowing conditions. Exterior paint adhesion shall be in Unsatisfactory adhesion shall a. Any area exceeding 0.090 square inch b. More than one area exceeding 0.045 square inch c. More than five areas of 0.021 square inch“ 3.3.2.4.3, third
14、line, after -“salt fog,“ add “for not less than 24 hours.“ Add new paragraph 3.3.2.4.4 as follows. relief of hydrogen embrittlement in accordance with the applicable requirements of TT-C-490. Validation of process shall be in accordance with 4.5.6.1.1.“ “3.3.2,4.4 Hydrogen embri ttlement. All projec
15、tiles shall be processed for 4.1, third line, after “requirements“ add “(examinations and tests).“ 4.1, last line, delete “assure“ and substitute “ensure.“ PAGE 6 4.1.1, first line, delete “must“ and substitute “shall.“ 2 Provided by IHSNot for ResaleNo reproduction or networking permitted without l
16、icense from IHS-,-,-I I l I I 1 1 I l I I I l I I l I l I I I I I I I MIL-P-85723 (1) 13 W 999990b Oqb7870 3 MIL-P-85723(AS) AMENDMENT 1 4.1.1, seventh and eighth 1 i nes, delete “Sampl i ng in qual i ty conformance“ and substitute “Sampling inspection, as part of manufacturing operations, is an acc
17、eptable practice to ascertai n conformance to requirements, however, thi s - - -. II PAGE 9 Delete existing Table II in its entirety and substitute “TABLE II. Body projectile (see Drawing 1575AS107). Categories and defects CRI TICAL: None defined MAJOR: 101 * 102. 103. 104. 105, 106. 107. 108. 109.
18、Di ame t er bourre 1 et mi n i mum Length, mouth to rear of rotating band seat, maximum Overall length, maximum Runout, large HE cavity 2/ Position small I.D. 2/ Large HE cavity inside diameter 21 Small I.D. 2/ Depth rotating band seat, knurl ing, minimum Runout, boat tail MINOR: 201. Lensth to rear
19、 edse of rotatincr band seat, minimum 202. 203. Foreign matter 204. Diameter rotating band seat knurled Width rotating band seat, mi nimum PAGE 10 le thod of i n spec t i on Gage Gage Gage Gage Gage Gage Gage Vi sua1 /Gage L/ Gage Gage Gage l!. Vi suai Gage II Delete existing Table III in its entire
20、ty and substitute 3 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-P-85723 (1) 13 9999906 0467871 5 MI L-P-85723(AS) AMENDMENT 1 “TABLE III. Projectile body assembly (see Drawing 1575AS106). Categories and defects CRITICAL : 1. Ferrous metal dis
21、continuity MAJOR: 101. 102. 103. 104, 105. 106, 107. 108. 109. 110. Length mouth to rear edge of rotating band Diameter, body rear of rotating band, minimum Diameter of rotating band Position rotating band diameter Width rotating band, overall Location crimp groove Profile crimp groove Radius, rear
22、edge of crimp groove, maximum Void at band/body interface Runout, body rear of rotating band MI NOR : 201. Finish qethod of inspectior Soundness Test (see 4.5.5) Gage Gage Gage Gage Gage Gage Gage Gage Vi sual Gage Vi sual In Table IV, under “MAJOR“ below “101 ,II add “102, Diameter, body rear of ro
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