ARMY MIL-P-64005-1985 PROJECTILE 155MM GB2 M687 METAL PARTS ASSEMBLY WITH LOADED OGIVE《带装药弧头部的M687式155毫米GB2射弹用金属件组件》.pdf
《ARMY MIL-P-64005-1985 PROJECTILE 155MM GB2 M687 METAL PARTS ASSEMBLY WITH LOADED OGIVE《带装药弧头部的M687式155毫米GB2射弹用金属件组件》.pdf》由会员分享,可在线阅读,更多相关《ARMY MIL-P-64005-1985 PROJECTILE 155MM GB2 M687 METAL PARTS ASSEMBLY WITH LOADED OGIVE《带装药弧头部的M687式155毫米GB2射弹用金属件组件》.pdf(23页珍藏版)》请在麦多课文档分享上搜索。
1、CI- MIL-P-64005 13 m 7997906 0352825 4 m Approved for public release; distribution is unlimited . THIS DOCUMENT CONTAINS PAGES. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-P-bLIOOS 13 W 7449706 O352826 h li MIL-P-64005 (AR) 2.1.2 Other Govern
2、ment documents, drawinqs and publications. The following other Government documents, drawings and publications form a part of this specification to the extent specified herein. DRAWINGS US ARMY ARMAMENT RESEARCH AND DEVELOPMENT CENTER (ARDC) PRODUCT AND PACKAGING DRAWINGS 11751156 - Projectile, 155M
3、M, GB2, M687 Ogive 9357729 - Projectile, 155ME9, GB2, M687 Marking 9349367 - Projectile, 155MM, GB2, M687, Metal Diagram Parts Assembly with Loaded Ogive US ARMY CHEMICAL RESEARCH AND DEVELOPMENT CENTER (CRDC) PRODUCT AND PACKAGING DRAWINGS E15-12-321 -Pallet, Side Loading for 155MM, M687 Projectile
4、 (Copies of specifications, standards, handbooks, drawings, and publications required by manufacturers in connection with specific acquisition functions should be obtained from the contracting activity or as directed by the contracting officer). 2.1.3 Order of precedence. In the event of a conflict
5、between the text of this specification and the references cited herein, the text of this specification shall take precedence. 3. REQUIREMENTS 3.1 Materials. Materials and parts shall be in accordance 3.2 Loaded ogive. The loaded ogive shall comply with all the with applicable drawings and specificat
6、ions. requirements specified on dwg. 9349367 and meet the requirements specified in applicable specifications. 3.3 Clean explosive scrap. Clean explosive scrap resulting from normal production operations may be re-melted and used provided that it complies with the requirements for high explosive (in
7、cluding grade) as specified on dwg. 9349367 with the exception that it does not have to meet the material form requirement called for in MIL-0-60371. Scraps from the floor, ventilation and suction apparatus (other than from machining operations specifically controlled to prevent contamination of exp
8、losive) shall not be used (see 6.8) . 2 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-P-64005 13 m 7797706 0352827 8 m MIL-P-64005 (AR) 3.4 Cavitation in high explosive charqe. 3.4.1 General. Cracks and cavities within an explosive e charge sha
9、ll not exceed the requirements specified in Table I when determined as specified in 4.5.1. Cavities having a maximum (max) projected length of 1/16 inch shall be disregarded provided that they are separated by 1/2 inch or more of solid explosivel. TABLE I. Cavitation requirements Sum of projected ar
10、eas of the cavities, 1/4 NA excluding pipes, cracks and annular %: rings, square inch (sq. in.). P t Projected length of any cavity, excluding 1/2 1/2 NA pipes, cracks, and annular rings (in.). Piping cavities, maximum (max.) projected 1/8 1/4 NA area (sq. in.). Piping cavities, max. projected width
11、 (in.) 1/8 1/4 NA Citacks, max. projected width (in.). 1/32 1/32 NA Annular rings, max. projected width (in.) . O 1/16 NA (Segments, See Figure 1) Piping cavitation is defined as cavitation located on or near the vertical center line of the ogive with the longitudinal axis (length) at least three ti
12、mes or greater than the width. An annular ring is defined as cavitation that takes the form of a ring or portion thereof around the periphery of the cast. * Void permitted in Segment C. 3.4.2 Cracked charges. There shall be no more than three transverse cracks in any total charge, and not more than
13、one traverse crack shall be permitted in Segment A. 3.4.3 Porosity. Porous areas shall be treated as cavities and shall be subject to the restrictions placed upon cavities, except that 80 percent of the projected length and 80 percent of the projected area shall be considered for acceptance purposes
14、. 3 - . Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-P-69005 13 a 7779706 0352828 T II MIL-P-64005 (AR) 3.4.4 Base separation. The maximum allowable base separation between the base of the ogive cavity and the cast shall be .O15 of an inch whe
15、n determined in accordance with 4.5.3. 3.4.5 Surface cavitation. Voids or cracks in segment C of Figure 1 shall not be cause for rejection. Cavities in the base of the fuzewell (top of segment B) shall not be cause for rejection provided the sum of the areas of the cavities is not greater than 80 pe
16、rcent of the top of segment B. No point may extend above the flat surface on which the liner will rest. Cavities having a maximum dimension of 1/32 inch.or less shall be disregarded in surface cavitation computations. 3.5 Loading of high explosive. 4 B 3.5.1 Loading. The ogive shall be loaded in acc
17、ordance with dwg. 9349367. -i 3.5.2 Mating surfaces. The mating surfaces of threads shall be free of caked explosives and all threads shall be free of foreign material. If a chemical cleaner is required, acetone or methylene chloride shall be used. Care shall be taken to prevent the chemical cleaner
18、 from coming into contact with the charge and becoming entrapped in the ogive. 3.5.3 Solid explosives. Solid explosives shall not be in the ogive before loading or added to the ogive during initial pouring or cooling. ogive prior to loading shall be free from foreign matter. 3.5.4 Ogive interior cav
19、ity. The interior cavity of the 3.5.5 Fuze well. The fuze well including threads shall be free from any foreign matter or loose explosive prior to assembly of the liner. 3.5.6 Exterior surfaces. There shall be no explosive on any exterior ,surfaces of the projectile after loading. 3.5.7 Ogive cavity
20、. The ogive cavity shall be free of scales, fins, burrs, draw marks, laminations, embedded foreign matter, folds, pits and sharp edges. 3.6 Liftinq plug. The projectile metal parts assembly with loaded ogive and with lifting plug assembled shall meet the disassembly torques specified n dwg. 9349367.
21、 4 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-P-b4005 13 W 777770b 0352827 1 W MIL-P-64005 (AR) 3.7 Provinq qround. 3.7.1 Metal parts assembly with inert ogive“. There shall be 0 no evidence of metal parts failure when tested at excess press
22、ure. Metal parts failure shall be: a. Loss or breakup of metal part components in bore or in b. Shear of the rotating band as evidenced by complete * Applicable only when ballistic test is used to qualify both flight (except obturator). lack of engraving. metal parts and ogive loading. * a T 3.7.2 M
23、etal parts assembly with loaded oqive. -.There shall be no evidence of metal parts assembly with loaded ogive failure when tested for excess pressure or at zone 3. Failure of this configuration shall be: a. Premature burst of the oxamide explosive composition in b. Partial or incomplete functioning
24、upon impact. c. Any metal parts separation in bore or in flight. bore or in flight. 3.8 First article inspection. This specification contains technical provisions for first article inspection. Requirements for the submission of first article samples by the contractor shall be as specified in the con
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