NAVY MIL-I-60508 A-1989 INITIATOR CARTRIDGE ACTUATED DELAY M6A1 M26 M33 M44 METAL PARTS ASSEMBLY《M6A1 M26 M33 M44 火药驱动起始延迟装置金属零件》.pdf

1、MIL-I-bOSO8A 13 = 99999Ob 0338730 O W , 5-3747, INCH-POUN D MIL-I-60508A 3 January 1989 SUPERSEDING 26 May 1966 and 15 July 1986 MI L-l-60508( MU) MILITARY SPECIFICATION AMENDMENT 1 INITIATOR, CARTRIDGE ACTUATED, DELAY, M6A1, M26, M33, M44, METAL PARTS ASSEMBLY This specification is approved for use

2、 by all Departments and AQenCiB of the Department of Defense 1. SCOPE 1.1 Scope. This specification covers the requirements for the Cartridge Actuated Initiators M6A1, M26, M33, M44, Metal Parts Assembly (see 6.1). 2. APPLICABLE DOCUMENTS 2.1 Government documents. 2.1.1 Specifications, standards and

3、 handbooks. The following specifications, standards and handbooks form a part of this document to the extent specified herein. Unless otherwise specified, the issues of these documents are those listed in the issue of the Department of Defense Index of Specifications and Standards (DoDISS) and suppl

4、ement thereto, cited in the solicitation (see 6.2). SPECIFICATIONS MILITARY MIL-A-2550 Ammunition, General Specification For STANDARDS MILITARY MI L-STD-105 Sampling Procedures and Tables for Inspection by Attributes MIL-STD-109 Quality Assurance Terms and Definitions MI L-STD-413 Visual Inspection

5、Guide for Elastomeric O-rings (Unless otherwise indicated, copies of federal and military specifications, standards, and handbooks are available from the Naval Publications and Forms Center, (Attn: NPODS), 5801 Tabor Avenue, Philadelphia, PA 19120-5099.) Beneficial comments (recommendations, additio

6、ns, deletions) and any pertinent data which may be of use in improving this document should be addressed to: Commanding Officer, Naval Ordnance Station, Standardization Branch (Sa), Indian Head, MD 20640-5000, by using the self-addressed Standardization Document Improvement Proposal (DD Form 1426) a

7、ppearing at the end of this document or by letter. AMSC NIA FSC 1377 DISTRIBUTION STATEMENT A. Approved for public release; distribution is unlimited. e ,- THIS DOCUMENT CONTAINS !y PAGES. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,- MIL-I-6050A

8、13 U 7777906 337312 . i MIL-I-60508A 2.1.2 Other Government documents, drawings, and publications. The following other Government documents, drawings, and publications form a patt of this document to the extent specified herein. Unless otherwise specified, the issues are those cited in the solicitat

9、ion. DRAW I NGS NAVAL ORDNANCE STATION, INDIAN HEAD, MD (CAGE Code 19200 and 19203) 8593315 Initiator, Cartridge Actuated, Delay, Metal Parts Assembly 8796826 Box, Fiberboard (Inner) Packing, Ammunition for Initiators, Cartridge Actuated, Delay, M4A1, MMl, M12A1, M26, M33, M44, M45Al or M49A1 879682

10、7 Box, Packing, Ammunition, for Initiator, Cartridge Actuated, Delay, M4A1, MW1, M12A1, M26, M33, M44, M45A1 or M49A1, in Fiber Container, M375 9216824 Box, Fiberboard (Outer) Alternative, Packing Ammunition, for Initiators, Car- tridge Actuated, Delay, M4A1, M6A1, M12A1, M26, M33, M44, M45A1, or M4

11、9A1 US, AIR FORCE TPO 00-845-1058 Initiator, Cartridge Actuated, M26 (Amdication for copies should be addressed to: Cornmanding Officer, Naval Ordnance Station, Data Control Branch - (Code 3720), Indian Head, MD 20640-5000.) 2.2 Order of mecedence. In the event of a conflict between the text of this

12、 document and the references cited herein the text oi this document takes precedence. Nothing in this document, however, supersedes applicable laws and regulations unless a specific exemption has been obtained. 3. REQUIREMENTS 3.1 First article. When specified in the contract or purchase order (see

13、6.2), a sample shall be subjected to first article inspection (see 4.4 and 6.4). 3.2 Materials. All materials used in the manufacture of the initiators shall conform strictly to the specifications referred to on the respective drawings unless specific approval in writing covering a departure therefr

14、om has been obtained from the cognizant Navy design activity prior to manufacture. When alternate materials or methods of manufacture are specified on the drawings, the bidders selections shall be clearly stated in the proposal. 3.3 Raw material. The contractor shall be responsible for selecting fro

15、m the classification list contained in the raw material specification the surface and physical condition of the raw material intended for use in manufacture. 3.4 Physical properties. Physical properties required by the drawing shall be uniform throughout the part within specified tolerances. Require

16、ments for all alloy steel parts shall be achieved by quenching and tempering. 36 Hydrostatic pressure. The initiator chamber and cap shall withstand a hydrostatic pressure of 5500 to 6500 pounds per square inch (psi) for 15 seconds, minimum, without deformation or mechanical failure (see 65.1). 3.6

17、Shear pin strength. The shear pin, after application of protective finish, shall shear when a load of 41 f 5 pounds is applied at the steady rate of 0.125 inch per minute. 2 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-I-6050BA 23 W 7779706 03

18、38732 4 MIL-I-60508A 3.7 Metal parts assembly. Parts shall be combined to produce an assembly which conforms to the requirements 3.8 Protective finish. Protective finish shall be in accordance with the applicable specifications and shall apply 3.9 Residual magnetism. The metal parts assembly shall n

19、ot deflect the indicator of the compass more than of the metal parts assembly drawing. All threaded joints shall be assembled handtight. to all surfaces of the component regardless of contour configuration. five degrees in either direction using procedures in 4.6.5. / 3.10 Workmanship. The requireme

20、nts for workmanship are as specified on the applicable drawings, referenced specifications and the following;. 3.10.1 Metal defects. All components shall be free from cracks, splits, cold shuts, inclusions, porosity or any similar defect. - 3.10.2 Burr. No part shall have a burr which might interfer

21、e with the assembly or function of the item or which might be injurious-to personnel handling the item. 3.10.3 Foreign matter. No part or assembly shall contain chips, dirt, grease, rust, corrosion or other foreign matter. 4. QUALITY ASSURANCE PROVISIONS 4.1 Responsibility for inspection. Unless oth

22、erwise specified in the contract or purchase order (see 6.2), the contractor is responsible for the performance of all inspection requirements (examinations and tests) as specified herein. Except as otherwise specified in the contract or purchase order, the contractor may use his own or any other fa

23、cilities suitable for the performance of the inspection requirements specified herein, unless disapproved by the Government. The Government reserves the right to perform any of the inspections set forth in the specification where such inspections are deemed necessary to ensure supplies and services

24、conform to prescribed requirements. 4.1.1 Responsibility for compliance. All items shall meet all requirements of sections 3 and 5. The inspection set forth in this specification shall become a part of the contractors overall inspection system or quality program. The absence of any inspection requir

25、ements in the specification shall not relieve the contractor of the responsibility of ensuring that all products or supplies submitted to the Government for acceptance comply with all requirements of the contract. Sampling inspection, as part of manufacturing operations, is an acceptable practice to

26、 ascertain conformance to requirements; however, this does not authorize submission of known defective material, either indicated or actual, nor does it commit the Government to accept defective material. 4.1.2 Quality assurance terms and definitions. Reference shall be made to MIL-STD-109 to define

27、 the quality assurance terms used. 4.1.3 Inspection. Inspection shall be in accordance with MIL-A-2550. 4.2 Classification of inspections. The inspection requirements specified herein are classified as follows: a. First article inspection (see 4.4) b. Quality conformance inspection (see 45). 4.3 Ins

28、pection conditions. Unless otherwise specified, all inspections shall be performed under the following conditions: a. Temperature: Room ambient 68O to 77OF b. Aititude: Sea level c. Humidity: 50 percent relative, maximum d. Atmospheric pressure: 14.7 psia 3 Provided by IHSNot for ResaleNo reproducti

29、on or networking permitted without license from IHS-,-,-MIL-I-bO5OA 13 M 7999906 0338733 b W MIL-I-60508A 4.4 First article inspection. At the beginning of regular production, the contractor shall submit an initial production sample to a Government approved facility for evaluation. The sample shall

30、consist of 5 metal parts assemblies, 9 sets of unassembled parts, 1 set of unassembled parts without plating or final protective finish and 50 shear pins from the same lot of shear pins tested by the contractor. The sample shall be manufactured in the same manner, using the same materials, equipment

31、, processes and procedures as used in regular production. All parts and materials, including packaging and packing, must be the same as will be used for regular production and shall be obtained from the same source of supply. After inspection and provisional acceptance at source, the first article s

32、ample shall be inspected for all requirements of the drawings and specifications. The Government reserves the right to require new first article samples until such time as an acceptable sample is submitted (see 6.4). 4.5 Quality conformance inspection. 4.5.1 Lot. 4.5.1.1 Submission of product. Unles

33、s otherwise specified by the contracting activity, formation and identification of Ids shall be in accordance with MIL-STD-105, 4.5.1.2 Size of lot. For the purpose of identification and shipment, the shipping lots of metal parts assemblies shall consist of 1200 assemblies, maximum, provided the hom

34、ogeneity requirements of inspection lots have been retained. 4.5.2 Examination. One-hundred percent examination shall be performed for all critical defects. Examination for major and minor defects shall be performed on a defect basis in accordance with the classification of defects, using the sampli

35、ng plan and associated criteria specified in the contract (see 6.2 and 6.3). All nonconforming material shall be rejected. Four power (4X) magnification may be used in performing visual examination for such defects as burr and foreign matter, Inspection for rubber Wings shall be in accordance with M

36、IL-STD415 When compliance with the applicable requirement is in doubt as a result of visual examination, the characteristic shall be measured or gaged to determine acceptability. 4.5.2.1 Retainer, Cartridge, Drawing 8593313, covering a detail of Drawing 8593315. Characteristic Defect Method of Inspe

37、ction Critical 1 Major 1 o1 102 103 104 105 106 107 108 109 110 111 112 113 114 115 116 117 Metering slots in base missing Visual Pitch diameter of thread, rnax Minor diameter of thread, max Concentricity of cavity with pitch diameter of thread Concentricity of counterbore with cavity Perpendiculari

38、ty of pitch diameter of thread with base Symmetry of metering slots in base with body Diameter of cavity, max Depth of cavity Depth to bottom of counterbore Depth of metering slots in base Length of effective thread, min Length of thread, rnax Internal radius at mouth of cavity Total length Width of

39、 metering slots in base Drill point in base, max Number of elongated slots incorrect Gage Gage Gage Gage Gage Gage Gage Gage Gage Gage Gage Gage Gage Measure Measure Measure Visual 4 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-Characteristic 118

40、119 120 12l 122 123 Minor 201 202 203 204 205 206 207 208 209 210 211 212 21 3 214 215 21 6 MIL-I-60508A Defect Thread damaged or not full Metal defective Protective finish inadequate or defective Surface finish on internal radius and base improper Burr Foreign matter present Pitch diameter of threa

41、d, min Diameter of cavity, min Diameter of counterbore Diameter of head Depth of counterbore Diameter of body Length of elongated slots Length of head Width of elongated slots Location of elongated slots Angle between head and body Angular location of metering slots Marking missing, incorrect or ill

42、egible Profile of elongated slots Radius missing or incorrect Surface finish improper, except as otherwise classified Method of Inspection 46.2.2 Chamber, Initiator, Drawing 8593314, covering a detail of Drawing 8593315. Critical None defined Major 1M 102 103 104 1 05 106 107 108 109 110 111 112 113

43、 114 115 116 117 118 Pitch diameter of large thread, min Major diameter of large thread, min Pitch diameter of small thread, min Major diameter of small thread, min Concentricity of counterbore with pitch diameter of large thread Concentricity of datum diameter with small thread Diameter of counterb

44、ore Depth of cavity Thickness of wall, min Location of datum diameter Profile of gas port Thread damaged or not full Chamfer at base of cavity missing or incorrect Metal defective Protective finish inadequate or defective Surface finish at end of gas port improper Burr Foreign matter present Visual

45、Visual Visual Visual Visual Visual Gage Gage Gage Gage Gage Measure Measure Measure Measure Measure Measure Visual Visual Visual Visual Visual Gage Gage Gage Gage Gage Gage Gage Gage Gage Gage Gage Visual Visual Visual Visual Visual Visual Visual 5 Provided by IHSNot for ResaleNo reproduction or net

46、working permitted without license from IHS-,-,-MIL-I-bOSO8A 13 W 777770b 0338735 T MIL-I-60508A Characteristic Defect =? Method of Inspection o Minor 201 202 203 204 205 206 207 208 209 210 211 21 2 21 3 214 215 21 6 Pitch diameter of large thread, max Pitch diameter of small thread, max Diameter of

47、 cavity Diameter of hole Diameter of small thread pilot Diameter of large thread pilot Length of large thread pilot Length of gas port Thickness of wall, max Location of small thread Depth of counterbore Total length Length to end of large thread Marking missing, incorrect or illegible Radius or cha

48、mfer missing or incorrect, except as otherwise classified Surface finish improper, except as otherwise classified 4.5.2.3 Pin, Shear, Drawing 8594745, covering a detail of Drawing 8593315. Critical None defined Major 1 o1 Diameter, max 102 Total length, min 103 Metal defective 104 105 Surface finish

49、 improper 106 Burr 107 Foreign matter present Protective finish inadequate or defective Minor 201 Total length, rnax 202 Profile of end 4.5.2.4 Cap, Drawing 8595254, covering a detail of Drawing 8593315. Critical None defined Major 101 102 103 104 Pitch diameter of thread, max Minor diameter of thread, max Concentricity of pitch diameter of thread with center hole, including perpendicularity with base of cavity Symmetry of flats with pitch diameter of thread Gage Gage Gage Gage Gage