NAVY MIL-T-45498 C-1993 THRUSTER CARTRIDGE ACTUATED M1A2 METAL PARTS ASSEMBLY《M1A2金属零件集合开动弹药筒推进器》.pdf

1、4 MIL-T-45498C 9999906 1853043 267 = I INCH-POUND I MIL-T-45498C 19 March 1993 SUPERSEDING 20 August 1969 MIL-T45498Bo MILITARY SPECIFICATION “RUSTER, CARTRIDGE ACTUATED, M1A2 MITAL PARTS ASSEMBLY his specijlcation is approved for use by all Departments and Agencies of the Department of Defense. 1.

2、SCOPE 1.1 Scope. This specification covers the requirements for the M1A2 Cartridge Actuated Thruster Metal Parts Assembly (see 6.1). 2. APPLICABLE DOCUMENTS 2.1 Government documents. 2.1.1 Specifications and standards. The following specifications and standards form a part of this document to the ex

3、tent 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 supplements thereto, cited in the solicitation (see 6.2). SPECIFICATIONS MILITARY MIL-A-2550 Ammunition, Gene

4、ral Specification For STANDARDS MILITARY MIL-STD-105 MIL-STD- 109 MIL-STD-4 13 Sampling Procedures And Tables For Inspection By Attributes Quality Assurance Terms And Definitions Visual Inspection Guide for Elastomeric O-rings Beneficial comments (recommeadations, additions, deletions) and my pertin

5、ent data which may be of use in improving this document should be addressed to: Commander, indian Head Division, Naval Surface Warfare Center, Standardization Branch (Code 8420), 101 Strauss Avenue, Indian Head, MD 20640-5035, by using the StanJardization Document Improvement Proposai D Fom 1426) ap

6、pearing at the end of this document or by sending a letter. AMSC NIA FSC 1377 DISTRIBUTION STATEMENT A: Approved for public release; distribution is unlimited. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-T-45498C (Unless otherwise indicated,

7、copies of federal and military specifications and standards are available from Standardization Documents Order Desk, Bldg. 4D, 700 Robbins Avenue, Philadelphia, PA 191 11-5094.) 2.1.2 Other Government documents, drawings, and publications. The following Government drawings form a part of this specif

8、ication to the extent specified herein. Unless otherwise specified, the issues are those cited in the solicitation (see 6.2). DRAWINGS Naval Surface Warfare Center, Indian Head (CAGE Codes 19200 and 19203) 8593855 Thruster, Cartridge Actuated, M1A2 Metal Parts Assembly 879763 1 Box, Fiberboard (Inne

9、r), Packing, Ammunition, For Thruster, Cartridge Actuated, M1A2 Box, Packing, Ammunition, For Thruster, Cartridge Actuated, M1A2 Box, Fiberboard (Outer), Alternative, Packing Ammunition, for Thruster, Cartridge Actuated, M1A2 8797632 9221261 U.S. Air Force TPO 00-891-5488 Thruster, Cartridge Actuate

10、d, M1A2 (Application for copies should be addressed to: Commander, Indian Head Division, Naval Surface Warfare Center, Attn: Data Control Branch (Code 8410), Indian Head, MD 20640-5035.) 2.2 Order of precedence. In the event of a conflict between the text of this document and the references cited he

11、rein, the text of 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 6.2), a sample shall be subjected to

12、 the first article inspection (see 4.3 and 6.3). 3.2 Materials. All materials used in the manufacture of the thrusters shall conform to the specifications referred to on the respective drawings unless specific approval in writing covering a departure therefrom has been obtained from the cognizant Na

13、vy 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. 3.2.1 Raw material. The contractor shall be responsible for selecting from the classification list contained in t

14、he raw material specification the surface and physical condition of the raw material intended for use in manufacture. 2 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-T-4549C m 9999906 LB53045 03T m MIL-T-45498C 3.3 Hardness and other physical p

15、roperties. Hardness and other physical properties required by the drawing shall be uniform throughout the part within specified tolerances. Requirements for all alloy steel parts shall be achieved by quenching and tempering. 3.4 Hydrostatic pressure. The body and head shall withstand a hydrostatic p

16、ressure of 7,500 pounds per square inch (psi) for 15 seconds, minimum, without leaking, deformation, or mechanical failure (see 6.4.1). 3.5 Shear pin strength. The shear pin, after application of protective finish, shall shear when a load of 48 f 4 pounds is applied at the steady rate of 0.125 inch

17、per minute. 3.6 Metal parts assembly. Parts shall be combined to produce an assembly which conforms to the requirements of the metal parts assembly drawing. All threaded joints shall be assembled handtight. 3.7 Protective finish. Protective finish shall be in accordance with the applicable specifica

18、tions 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 procedures in 4.6.5. 3.9 Workmanship. Thrusters shall be free o

19、f cracks, splits, or other defects which might prevent proper mating with connecting parts or proper functioning of the device. 3.9.1 Metal defects. All components shall be free from cracks, splits, cold shuts, inclusions, porosity, or any similar defect. 3.9.2 Burr. No part shall have a burr which

20、might interfere with the assembly or function of the item or which might be injurious to personnel handling the item. 3.9.3 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 inspecti

21、on. Unless otherwise specified in the contract or purchase order, 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 othe

22、r facilities 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 this specification where such inspections are deemed necessary to ensure supplies and serv

23、ices conform to prescribed requirements (see 6.2). 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 in

24、spection requirements in the specification shall not relieve the contractor of the responsibility of ensuring that all products or supplies submitted to the Government for 3 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-T-45498C W 7999906 18530

25、46 T7b W MIL-T-45498C acceptance comply with all requirements of the contract. Sampling inspection, as part of manufacturing operations, is an acceptable practice to ascertain conformance to requirements; however, this does not authorize submission of known defective material, either indicated or ac

26、tual, nor does it commit the Government to acceptance of defective material. 4.1.2 Quality assurance terms and definitions. Reference shall be made to MIL-STD-109 to define the quality assurance terms used. 4.1.3 Inspections. Inspections shall be in accordance with MIL-A-2550. 4.2 Classification of

27、inspections. The inspection requirements specified herein are classified as follows: a. b. First article inspection (see 4.4) Quality conformance inspection (see 4.5) 4.3 Inspection conditions. Unless otherwise specified (see 6.2), all inspections shall be performed under the following conditions: a

28、. Temperature: room ambient (68 to 77F) b. Altitude: sea level c. Humidity: 50 percent relative, maximum d. Atmospheric pressure: 14.7 psi 4.4 First article inspection. At the beginning of regular production, the contractor shall submit an initial production sample to a Government approved facility

29、for evaluation. The sample shall consist of five metal parts assemblies, nine sets of unassembled parts, one set of unassembled parts without plating or final protective finish, and fifty shear pins from the same lot of shear pins tested by the contractor. The sample shall be manufactured in the sam

30、e manner, using 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 for regular production and shall be obtained from the same source of supply. After inspection and provisi

31、onal acceptance 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 an acceptable sample is submitted (see 6.3). 4.5 Quality conformance inspection. 4.5.1 Lot. 4.5

32、.1.1 Submission of product. Unless otherwise specified by the contracting activity, formation and identification of lots shall be in accordance with MIL-STD-105. 4.5.1.2 Size of lot. The production lot size shall be as specified in the contract. 4.5.2 Examination. One hundred percent examination sha

33、ll be performed for all critical defects. Examination for major and minor defects shall be performed on a defect basis in accordance with the 4 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-T-45498C = 9999906 1853047 702 = . MIL-T-45498C classi

34、fication of defects. Four power (4x) magnification may be used in performing visual examination for such defects as burr and foreign matter. Inspection for rubber O-rings shall be in accordance with MIL-STD-413. When compliance with the applicable requirement is in doubt as a result of visual examin

35、ation, the characteristic shall be measured or gaged to determine acceptability. All nonconforming material shall be rejected. 4.5.2.1 Key, Drawing 8593857, covering a detail of Drawing 8593855. Characteristics Defect Method of Inspection Critical None defined Major 101 102 Radial profile of width 1

36、03 Surface finish incorrect 104 105 Metal defective 106 Burr or sharp corner 107 Foreign matter Radial profile of length, inside and outside Protective finish inadequate or defective Minor 20 1 Total length 202 Radius or chamfer incorrect Gage Gage Visual Visual Visual Visual Visual Gage Gage 4.5.2.

37、2 Pin, Firing, Drawing 8593864, covering a detail of Drawing 8593855. Critical None defined Major 101 102 103 104 105 106 107 108 1 o9 110 111 112 113 114 115 116 Concentricity of groove with body Concentricity of striker with body Concentricity of striker shoulder with body True position of hole wi

38、th body Diameter of groove Diameter of body, min Diameter of striker, max Diameter of pin hole, max Depth of pin hole Profile of striker Profile of groove Metal defective Protective finish inadequate or defective Surface finish of body and striker tip incorrect Burr or sharp corner Foreign matter Ga

39、ge Gage Gage Gage Gage Gage Gage Gage Gage Gage Gage Visual Visual Visual Visual Visual 5 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-Minor 201 202 203 204 205 206 207 208 209 2 10 21 1 2 12 213 214 215 216 217 218 219 MIL-T-q5q98C D 9999906 I185

40、3048 849 MIL-T-45498C Diameter of body, max Diameter of striker, min Diameter of pin hole, min Diameter of striker shoulder Depth of pin hole Length from body to tip of striker Length of striker Total length Location of pin hole Location of groove Depth of slot in base Length of body diameter forwar

41、d of groove, min Width of groove Width of slot in base Location of slot in base Radius incorrect Radius missing Surface finish improper, except as otherwise classified Marking missing, incorrect, or illegible Gage Gage Gage Gage Gage Gage Gage Gage Gage Gage Gage Gage Gage Gage Gage Gage Visual Visu

42、al Visual 4.5.2.3 Body Assembly, Drawing 8593859, covering a detail of Drawing 8593855. Critical None defined Major 101 102 103 104 105 106 107 108 109 110 111 112 113 114 115 116 117 118 Pitch diameter of thread, min Major diameter of thread, min Concentricity of pitch diameter of thread with large

43、 bore Concentricity of small bore with large bore Concentricity of groove with small bore Concentricity of body, thread end, with pitch diameter Concentricity of counterbore with small bore Perpendicularity of face at threaded end with pitch diameter Perpendicularity of face of flange with pitch dia

44、meter Diameter of large bore, max Diameter of counterbore Diameter of key groove Diameter of small bore Diameter of body, thread end Diameter of internal undercut, max, if applicable Location of key groove Straightness of bore Diameter of thread undercut, min of thread of thread of thread Gage Gage

45、Gage Gage Gage Gage Gage Gage Gage Gage Gage Gage Gage Gage Gage Gage Gage Gage 6 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-119 120 121 122 123 124 125 Minor 20 1 202 203 204 205 206 207 208 209 210 211 2 12 213 214 215 216 217 218 219 220 flIL

46、-T-45498C m 799990b 1853049 785 m MIL-T-45498C Profile of key groove Thread damaged or not full Metal defective Protective finish inadequate or defective Surface finish of large bore improper Burr or sharp corners Foreign matter Pitch diameter of thread, max Diameter of large bore, min Diameter of b

47、ody, max Depth of counterbore Total length Length of flange Thickness of wall Diameter of flange Length to start of angle at flange, min Length to end of angle at flange, rnax Length to large bore Length to body, thread end Width of thread undercut Width of internal undercut, max, if applicable Widt

48、h of flats Width across flats Location of flats Marking missing, incorrect, or illegible Radius or chamfer incorrect Surface finish improper, except as otherwise classified Gage Visual Visual Visual visual Visual Visual Gage Gage Gage Gage Gage Gage Gage Gage Gage Gage Gage Gage Gage Gage Gage Gage

49、Visual Visual Gage Visual 4.5.2.4 Body Assembly, Drawing 8593859, covering a detail of Drawing 8593855. Critical None defined Major 101 102 103 104 105 106 107 Diameter across top of pellets, max Gage Protrusion of pellet above major diameter of thread, min Gage Pellet missing, loose, or improperly inserted Manual/Visual Thread damaged or not full Visual Metal defective Visual Burr Visual Foreign matter Visual Minor 20 1 Location of pellet 202 Pellet radius incorr