NAVY MIL-DTL-60517 C-2011 INITIATOR CARTRIDGE ACTUATED M27 METAL PARTS ASSEMBLY《M27金属零件组件弹药驱动引爆器》.pdf

1、INCH POUND MIL-DTL-60517C 25 March 2011 SUPERSEDING MIL-DTL-60517B 14 September 2004 DETAIL SPECIFICATION INITIATOR, CARTRIDGE ACTUATED, M27 METAL PARTS ASSEMBLY This specification is approved for use by all Departments and Agencies of the Department of Defense. 1. SCOPE 1.1 Scope. This specificatio

2、n covers the requirements for the M27 Cartridge Actuated Initiator Metal Parts Assembly (see 6.1). 2. APPLICABLE DOCUMENTS 2.1 General. The documents listed in this section are specified in sections 3, 4, or 5 of this specification. This section does not include documents cited in other sections of

3、this specification or recommended for additional information or as examples. While every effort has been made to ensure the completeness of this list, document users are cautioned that they must meet all specified requirements of documents cited in sections 3, 4, or 5 of this specification, whether

4、or not they are listed. 2.2 Government documents. 2.2.1 Specifications, standards, and 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 cited in the solic

5、itation or contract. DEPARTMENT OF DEFENSE SPECIFICATIONS MIL-A-2550 Ammunition, General Specification for (Copies of these documents are available online at https:/assist.daps.dla.mil/ or from the Standardization Document Order Desk, 700 Robbins Avenue, Building 4D, Philadelphia, PA 19111-5094.) Co

6、mments, suggestions, or questions on this document should be addressed to DEPARTMENT OF THE NAVY, Indian Head Division, NSWC, Code E12AP, Document Control, 4123 Artisans Court, Suite 103, Indian Head, Maryland 20640-5085, OFFICIAL BUSINESS, or emailed to amanda.pennnavy.mil. Since contact informatio

7、n can change, you may want to verify the currency of this address information using the ASSIST Online database at https:/assist.daps.dla.mil/. DISTRIBUTION STATEMENT A. Approved for public release; distribution is unlimited. AMSC N/A FSC 1377 Provided by IHSNot for ResaleNo reproduction or networkin

8、g permitted without license from IHS-,-,-MIL-DTL-60517C 22.2.2 Other Government documents, drawings, and publications. The following other Government documents, drawings, and publications form a part of this document to the extent specified herein. Unless otherwise specified, the issues of these doc

9、uments are those cited in the solicitation or contract. DRAWINGS NAVAL ORDNANCE STATION, INDIAN HEAD (GAGE CODE 19200 and 19203) 10520551 Initiator, Cartridge Actuated, M27, Metal Parts Assembly 8830984 Box, Fiberboard (inner) packing, Ammunition for Initiator, Cartridge Actuated M27, M86, M87, M99,

10、 or XM107 8830985 Box, Packing, Ammunition, for Initiator, Cartridge Actuated M27, M86, M87, M98, M99, or XM017 9241155 Box, Fiberboard (Outer) Alternative Packing, Ammunition, for Initiator, Cartridge Actuated M27, M86, M87, M98, M99, or XM107 (Application for copies should be addressed to Commandi

11、ng Officer, Naval Surface Warfare Center, Indian Head, Technical Information Branch (Code 4230), Indian Head, MD 20640.) 2.3 Non-Government publications. The following documents form a part of this document to the extent specified herein. Unless otherwise specified, the issues of these documents are

12、 those cited in the solicitation or contract. AMERICAN SOCIETY FOR QUALITY ASQ A8402 Quality Management and Quality Assurance Vocabulary ASQ Z1.4 Sampling Procedures and Tables for Inspection by Attributes (Application for copies should be addressed to the American Society for Quality Control, PO Bo

13、x 3005, 611 E. Wisconsin Ave., Milwaukee, WI 53201-4606.) INTERNATIONAL ORGANIZATION FOR STANDARDIZATION ISO 3601-3 Fluid power systems O-ring Part 3: Quality acceptance criteria (Application for copies should be addressed to the International Organization for Standardization, 1, ch. de la Voie-Creu

14、se, Case postale 56 CH-1211 Geneva 20, Switzerland) 2.4 Order of precedence. Unless otherwise noted herein or in the contract, in the event of a conflict between the text of this document and the references cited herein, the text of this document takes precedence. Nothing in this document, however,

15、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 6.2), a sample shall be subjected to first article inspection (see 4.4 and 6.3). 3.2 Materials. All materials used in the

16、 manufacture of the initiators shall conform strictly to the specifications referred to on the respective drawings unless specific approval in writing covering a departure there from has been obtained from the cognizant Navy design activity prior to manufacture. Provided by IHSNot for ResaleNo repro

17、duction or networking permitted without license from IHS-,-,-MIL-DTL-60517C 3When alternate materials or methods of manufacture are specified on the drawings, the bidders selections shall be clearly stated in the proposal. 3.2.1 Raw materials. The contractor shall be responsible for selecting from t

18、he classification list contained in the raw material specification the surface and physical condition of the raw material intended for use in manufacture. 3.3 Hardness and other physical properties. Physical properties required by the drawing shall be uniform throughout the part within specified tol

19、erances. Requirements for all alloy steel parts shall be achieved by quenching and tempering. 3.4 Hydrostatic pressure. The initiator chamber and cap shall withstand a hydrostatic pressure of 14,000 to 15,000 pounds per square inch (psi) for 15 seconds, minimum, without deformation or mechanical fai

20、lure (see 6.4.1). 3.5 Firing pin release. The firing pin of the metal parts assembly initiator, less safety pin and cartridge, shall release from the cocked position when the application of an axial load of 15 to 30 pounds has withdrawn the initiator pin 0.370 inch, minimum, and 0.425 inch, maximum

21、(see 4.3.3). 3.6 Initiator pin security. Application of an axial load of 200 to 220 pounds to the initiator pin of the metal parts assembly shall not withdraw the initiator pin past the safety pin. Load application shall cause no permanent deformation of the safety pin. 3.7 Protective finish. Protec

22、tive finish shall be in accordance with the applicable specifications and shall apply to all surfaces of the component regardless of contour configuration. 3.8 Residual magnetism. The metal parts assembly shall not deflect the indicator of the compass more than five degrees in either direction using

23、 procedures in 4.6.6. 3.9 Metal parts assembly. Parts shall be combined to produce an assembly, which conforms to the requirements of the metals parts assembly drawing. All threaded joints shall be assembled hand tight. 3.10 Workmanship. The requirements for workmanship are as specified on the appli

24、cable drawings, referenced specification, 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 interfere with the assembly or function of the item or whic

25、h 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. VERIFICATION 4.1 Classification of inspections. The inspection requirements specified herein are classified as follows: a. C

26、onformance inspection. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-DTL-60517C 44.1.1 Quality assurance terms and definitions. Reference shall be made to ASQ A8402 to define the quality assurance terms used. 4.1.2 Inspection. Inspection shall

27、be in accordance with MIL-A-2550. 4.2 Classification of Characteristics. The inspection requirements specified herein are classified as follows: a. First article inspection (see 4.4) b. Quality conformation inspection (see 4.5) 4.3 Inspection conditioning. Unless otherwise specified (see 6.2), all i

28、nspections shall be performed under the following conditions: a. Temperature: Room ambient 20 to 25 C (68 to 77 F) b. Altitude: Sea level c. Humidity: 50 percent relative, maximum d. Atmospheric pressure: 14.7 psia. 4.4 First article inspection. At the beginning of regular production, the supplier s

29、hall submit a first article sample to a Government approved facility for evaluation. The sample shall consist of 5 metal parts assemblies, 9 sets of unassembled parts, and 1 set of unassembled parts without plating or final protective finish. The sample shall be manufactured in the same manner, usin

30、g the same materials, equipment, processes, and procedures as used in regular production. All parts and materials, including packaging and packing, must be the same as will be used in regular production and shall be obtained from the same source of supply. After inspection and provisional acceptance

31、 at source, the first article sample 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 6.3). 4.5 Quality conformance inspection. 4.5.1 Lot. 4.5.1

32、.1 Submission of product. The product shall be submitted in accordance with ASQ Z1.4. 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 homogeneity requirements of inspection lots h

33、ave 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 contained herein. Four power (4X) magnification may be used

34、 in performing visual examination for such defects as burr and foreign matter. Inspection for rubber O-rings shall be in accordance with ISO 3601-3. When compliance with the applicable requirements is in doubt as a result of visual examination, the characteristic shall be measured or gaged to determ

35、ine acceptability. All nonconforming material shall be rejected. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-DTL-60517C 54.5.2.1 Chamber, Initiator, Drawing 10520407, covering a detail of Drawing 10520551. Characteristic Defect Method of Insp

36、ection Critical None Defined Major 101 Pitch diameter of large external thread, min Gage 102 Major diameter of large external thread, min Gage 103 Pitch diameter of small external thread, min Gage 104 Major diameter of small external thread, min Gage 105 Pitch diameter of internal thread, max Gage 1

37、06 Minor diameter of internal thread, max Gage 107 Concentricity of datum location with pitch diameter of small external thread Gage 108 Concentricity of pitch diameter of large thread with cavity Gage 109 Concentricity of large external thread pilot with large external thread Gage 110 Concentricity

38、 of counterbore with cavity, including perpendicularity with base of counterbore Gage 111 Diameter of counterbore Gage 112 Diameter of large thread pilot Gage 113 Depth of cavity Gage 114 Length of datum location Gage 115 Thickness of wall, min Gage 116 Metal defective Visual117 Protective finish, i

39、nadequate or defective Visual 118 Surface finish of cavity and angle of gas port, improper Visual 119 Burr Visual 120 Foreign matter present Visual Minor 201 Pitch diameter of large external thread, max Gage 202 Pitch diameter of small external thread, max Gage 203 Pitch diameter of internal thread,

40、 min Gage 204 Diameter of small external relief Gage 205 Diameter of small external thread pilot Gage 206 Diameter of hole in gas port Gage 207 Diameter of cavity Gage 208 Depth of counterbore Gage 209 Length of gas port Gage 210 Length of small thread relief Gage 211 Length from face of gas port to

41、 small thread Gage 212 Length of external thread pilot Gage 213 Thickness of wall, max Gage 214 Depth of threaded hole Measure 215 Diameter of chamfer at internal thread Measure 216 Total length Measure217 Length of large external thread Measure 218 Marking missing, incorrect or illegible Visual Pro

42、vided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-DTL-60517C 6219 Radius or chamfer, missing or incorrect Visual 220 Surface finish improper, except as otherwise classified Visual 4.5.2.2 Cap, Initiator, Drawing 10520552, covering a detail of Drawing

43、10520551. Critical None defined Major 101 Pitch diameter of small internal thread, max Gage 102 Minor diameter of small internal thread, max Gage 103 Pitch diameter of large external thread, max Gage 104 Minor diameter of large external thread, max Gage 105 Concentricity of pitch diameter of large i

44、nternal thread with midsection cavity, including perpendicularity with base of counterbore of large cavity Gage 106 Concentricity of pitch diameter of small internal thread with midsection cavity, including perpendicularity with base of counterbore of large cavity Gage 107 Concentricity of hole betw

45、een small cavity and boss cavity with midsection cavity, including perpendicularity with base of counterbore of large cavity Gage 108 Concentricity of undercut in large cavity with large internal thread Gage 109 Concentricity of boss cavity with hole between small cavity and boss cavity Gage 110 Con

46、centricity of flange with hole between small cavity and boss cavity Gage 111 Concentricity of body, large end with large internal thread Gage 112 Concentricity of small cavity with midsection cavity Gage 113 Concentricity of thread with large internal thread Gage 114 Symmetry of thickness of mountin

47、g lugs with body, large end Gage 115 Symmetry of length of mounting lugs with body, large end Gage 116 Variation of centerline of mounting holes with small hole between boss cavity and small cavity Gage 117 Diameter of large cavity rear of undercut Gage 118 Diameter of small cavity Gage 119 Diameter

48、 of boss cavity, max Gage 120 Diameter of hole between small cavity and boss cavity, max Gage 121 Diameter of undercut at large internal thread Gage 122 Diameter of safety pin hole, max Gage Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-DTL-605

49、17C 7123 Diameter of flange Gage 124 Length of effective small interior thread, min Gage 125 Length of small interior thread, max Gage 126 Width of undercut behind large interior thread Gage 127 Location of safety pin hole Gage 128 Height of boss Gage 129 Metal defective Visual 130 Protective finish, inadequate or defective Visual 131 Burr Visual132 Foreign matter present Visual Minor 201 Pitch diam