ARMY MIL-P-14839-1968 PROJECTILE 105MM SMOKE BE M84E1 METAL PARTS ASSEMBLY《M84E1式105毫米底抛(BE)发烟弹用金属件组件》.pdf
《ARMY MIL-P-14839-1968 PROJECTILE 105MM SMOKE BE M84E1 METAL PARTS ASSEMBLY《M84E1式105毫米底抛(BE)发烟弹用金属件组件》.pdf》由会员分享,可在线阅读,更多相关《ARMY MIL-P-14839-1968 PROJECTILE 105MM SMOKE BE M84E1 METAL PARTS ASSEMBLY《M84E1式105毫米底抛(BE)发烟弹用金属件组件》.pdf(17页珍藏版)》请在麦多课文档分享上搜索。
1、MIL-P- i4839 (MU) 9 February 1968 MILITARY SPECIFrI: CATION PROJECTILE, 105MM : SMOKE, BE, M84E1 METAL PARTS ASSEMBLY 1. SCOPE 1.1 This specification covers Projectile, 105MM: SMOKE, BE, M841, Metal Parts Assembly. 2. APPLICABLE DOCUMENTS 2.1 The following documents of the issue in effect on date of
2、 invitaiAon for bids or request for proposal, form a part of this specification to the extent specified herein. SPECIFICATTONS Military MIL-A- 2550 - Ammunition and Special Weapons, General Specification for STANDARDS Federal Federal Test Method Standard No. i41 - Paint, Varnish, Lacquer and Related
3、 Materials, Method of Inspection, Sampling and Testing. Federal Test Method Standard No. l5l - Metals; Test Methods Military MIL-STD-105 MIL-STD-109 - Quality Assurance Terms and Definit,ions MIL-STD-129 - Sampling Procedures and Tables for Inspection by Attributes - Marking for Shipment and Storage
4、 FSC 1315 . I. THIS DOCUMENT CONTAINS 17 PAGES. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-P-L4837 13 m 7779706 0277362 T m 1-P-14839 (MU) 2.1 (contd) . MIL-STD-1167 - Ammunition Data Card MIL-STD- NIL-STD-i169 MIL-STD-i235 - Lot Numbering o
5、f Ammunition - Packaging, Packing and Marking for Shipment - Single and Multilevel Continuous Sampling of Inert Ammunition Components Procedures and Tables for Inspection by Attributes DRAWINGS Munitions Command Di0542988 E-i0542988 F8837835 D8593429 - Projectile, 105MM, SMOKE, BE, 841, - Inspection
6、 Equipment List for projectile, 105m, - Pallet for Fixed and Semi-Fixed Shell - Band Seating Testing Machine Indentor and Test Metal Parts Assembly SMOKE, BE, M841, Metal Parts Assembly Data PUBLICATIONS MUCOM Frankford Arsenal Operating instructions for use of Detroit Testing Machine for Band Seat
7、Inspection (Copies of specifications, standards , drawings and publications required by suppliers in connection with specific procurement functions should be obtained from the procuring activity or as directed by the contracting officer . ) 2.2 Other Fub1ications.-The following documents form a part
8、 of this specification to the extent specified herein. the issue in effect on date of invitation for bids or request for proposal shall apply. Unless otherwise indicated, ASA-B46.1 - .American Standards Surface Texture, Surface Roughness , Waviness and Lay Technical society and technical association
9、 specifications and standards are generally vailable for reference from libraries. distributed among technical groups and using Federal agencies. They are also 2 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-P-L4B39 13 7979906 0297363 L W 3. RE
10、QUIREMENTS 3.1 General.-Materials, parts and assemblies shall comply with the requirements specified on the applicable drawings, referenced specifications and the following: 3.2 Heat treatment or stress relief.-Heat treatment or stress relief applied to the projectile body shall be uniform throughou
11、t and shall be so conducted as to produce in each projectile body the mechanical properties specified by the applicable drawing. plastic flow without subsequent heat treatment of stress relief is not permitted. Metal forming involving 3.2.1 Hot Forged- Heat treatment method of manufacture.-Projectil
12、e bodies manufactured from forgings shall be subjected to heat treatment to attain the mechanical propertiei specified by the applicable drawing. Heat treatment shall consist of heating above the critical temperature, not to exceed i600 degrees Fahrenheit (OF), followed by an oil quench. quenching,
13、the body forging shall be tempered without delay at a temperature above 750 OF which will produce the required mechanical properties. removal from the tempering furnace, the body forging shall be slowly cooled in air (forced air permitted) to a temperature of not more than 700 OF, after which coolin
14、g may be accelerated by water spray. After After 3.2.2 Cold shaping and hot cup - Cold draw method of manufacture.- Cold working shall be so accomplished as to produce in the projectile body the mechanical properties specified by the applicable drawing. body so formed shall be stress relieved at a t
15、emperature of 700 OF, minimum, following the final forming operation which results in plastic flow. minimum soak time at or above minimum stress relief temperature shall be established which will produce mechanical properties specified by the applicable drawing. anneals prior to the final forming op
16、eration shall be predicated on attainment of required mechanical properties when formed by an approved sequence of operations. The projectile The The temperature and time duration of in process 3.3 Mechanical properties. 3.3.1 Projectile body.-Mechanical properties specified on the applicable drawin
17、g shall apply throughout the projectile body. 3.3.2 the projectile body, the rotating band shall have the following mechanical properties: Rotating band.-After application and subsequent removal from Tensile Strength - 30,000 pounds per square inch (PSI) minimum Elongation - i5 percent minimum in 1
18、inch 3 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-P-( MU) 3.4 Rotating band seating. 3.4.1 Band seat cleanliness.-Prior to banding, the band seat shall be clean and free of oil, dirt, grease, rust or other foreign matter, Shot or sand blasti
19、ng is not permitted for cleaning the band seat after knurling . 3.4.2 Application of band blank.-The rotating band blank shall be pressed into the band seat, after final heat treatment of the projectile body. The band blank shall be applied in such manner as not to distort the projectile body. band
20、seat for a minimum of eight-tenths of the band seat depth measured from the outside surface of the projectile body. There shall be no gap between the band and the band seat sidewalls at %he outside surface of the projectile body after the rotating band has been machined to final dimensions. The band
21、 blank must contact the sidewall of the 3.4.3 Rotating band clearance.-The diametrical clearance between the rotating band and the band seat shall not exceed .o06 inch. 3.5 Meta1defects.-All components shall be free from cracks, seams, splits, cold shuts, inclusions, lamination, porosity or similar
22、defects. 3.6 Protective coating. 3.6.1 Body assembly and base plug.-Requirements relative to paint thickness are not specified except as a guide to performance of tests as indicated by the applicable drawings and specifications. Actual component parts must withstand the specified salt spray exposure
23、 with coating breakdown not greater than that described by the applicable specification. 3.6.2 Baffle plate.-All aspects of surface pretreatment or surface coating are as shown by the applicable specification, and are subject to demonstration of control of process thru salt spray test of panels as i
24、ndicated by the applicable specification. 3 7 Functional 4 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-P-LLl837 13 7797706 0277365 5 3.7.iMetal parts security.-When tested in accordance with 4.4.5. The Metal projectile assembly shall reveal n
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