NAVY MIL-T-60102 A-1974 THRUSTER CARTRIDGE ACTUATED M9 METAL PARTS ASSEMBLY《M9金属零件集合发动弹药筒推进器》.pdf

1、MIL-T-bOL02A 13 9779906 033559Z T MIL-T-60102A (MU) 18 July 1974 SUPERSEDING MIL-T-60102 (MU) 24 January 1964 MILITARY SPECIFICATION THRUSTER, CARTRIDGE ACTUATED, M9 METAL PARTS ASSEMBLY This specification is approved for use by all Departments and Agencies of the Department of Defense. 1. SCOPE 1.1

2、 This specification covers Thruster, Cartridge Actuated, M9, Metal Parts The assembly willultimately be loaded and used in conjunction with Assembly. other propellant actuated devices in aircrew emergency escape systems. 2. APPLICABLE DOCUMENTS 2.1 The following documents of the issue in effect on d

3、ate of invitation for bids or request for proposals, form a part of this specification to the extent specified herein: SPECIFICATIONS Mi lit ar y . MIL-A-2550 - Ammunition and Special Weapons, General Specification for STANDARDS Military MIL-STD-105 MIL-STD-109 MIL-STD-413 DRAWINGS Armament Command

4、F10520479 C8845196 - Sampling Procedures and Tables for Inspection - Quality Assurance Terms and Definitions - Visual Inspection Guide for Rubber O-Rings by Attributes - Thruster, Cartridge Actuated, M9 Metal - Box, Fiberboard (Inner) Packing Ammunition Parts Assembly for Thruster, Cartridge Actuate

5、d, M9 FSC 1377 - DOCUMENT CONTAINSPAGES - Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-VILrT-bO102A 13 W 7999906 0335593 L W MIL-T-60102A (MU) 2.1 (Contd) e8845197 - Box, Packing Ammunition for Thruster, Cartridge Actuated M9 C9217287 - Box, Fiber

6、board (Outer) Alternative Packing, Ammunition for Thruster, Cartridge Actuated M9 Cartridge Actuated M9, Metal Parts Assembly IEL-10520479 - Inspection Equipment List for Thruster, (Copies of specifications, standards and drawings required by suppliers in connection with specific grovernment functio

7、ns should be obtained from the procuring activity or as directed by the contracting officer.) 2.2 Other publications.-The following documents form a part of this specification to the extent specified herein. Unless otherwise indicated, the issue in effect on date of invitation for bids or request fo

8、r proposal shall apply ANSI-B. 1 - Surface Texture (Application for copies should be addressed to ehe American National Standards Institute (ANSI), 1430 Broadway, New York, N.Y. 10018.) 3. REQUIEMENTS 3.1 General.-Materials, parts and assemblies shall comply with the require- ments specified on the

9、applicable drawings and referenced specifications. 3.2 Mechanical properties.-Mechanical properties required by the drawings shall be uniform throughout the part within specified tolerances. alloy steel parts shall be achieved by quenching and tempering. Requirements for all 3.3 Hydrostatic pressure

10、.-The body shall withstand a hydrostatic pressure of 10,000 pounds per square inch (PSI), minimum, for 15 seconds, minimum, without application of any external load and shall show no evidence of leakage or mechani- cal failure (see 6.1). 3.4 which conforms to the requirements of the metal parts asse

11、mbly drawing and the following : Metal parts assembly.-Parts shall be combined to produce an assembly 3.4.1 All threaded joints shall be assembled hand tight, except as specified in Table I. 2 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-3.4.2 Tor

12、que.-Torque requirements shall be as specified in Table I. No movement or deformation shall occur upon application of the breakaway torque. TABLE I A B Components Seating or Bottoming Breakaway (inch pounds) (inch pounds) 100 -I- 20 75 min. Piston and Adapter - 3.4.3 Trunnion rotation.-Upon completi

13、on of assembly, the trunnion shall be free to rotate 360 degrees. 3.4.4 Piston rotation.-Upon completion of assembly, the adapter shall be free to rotate 360 degrees in a clockwise direction. 3.5 Protective finish,-Protective finish shall be in accordance with the applicable specifications and drawi

14、ngs, and shall apply to all surfaces of the component regardless of contour configuration. 3.6 Residual magnetism.-The metal parts assembly shall not deflect the indicator of the compass more than 3 degrees in either direction when passed in front of the compass at a distance of 6 inches. 3.7 Workma

15、nship.-The requirements for workmanship are as specified on the applicable drawings, referenced Specifications and the following: 3.7.1 Metal defects.-All components shall be free from cracks, splits, cold shuts, inclusions, porosity or any similar defect. 3.7.2 %.-No part shall have a burr which mi

16、ght interfere with the assembly or function of the item or which might be injurious to personnel handling the item. 3.7.3 Foreign matter.-No part or assembly shall contain chips, dirt, grease, .rust, corrosion or any other foreign matter, 4. QUALITY ASSURANCE PROVISIONS 4.1 Responsibility for inspec

17、tion.-Unless otherwise specified in the contract or purchase order, the supplier is responsible for the performance of all inspection requirements specified herein. in the contract or order, the supplier may use his own or any other facilities suitable for the performance of the inspection requireme

18、nts specified herein, unless disapproved by the Governmant. perform any of the inspections set forth in the specification and drawing where such inspections are deemed necessary to assure supplied and services conform to prescrLbed requirements, Except as otherwise specified The Government reserves

19、the right to 3 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-T-bOL02A 13 7779706 0335575 5 0 4.1.1 Quality Assurance terms and definitions.-Reference shall be made to Standard MIL-STD-109 to define quality assurance terms used. 4.1.2 Inspection

20、.-Inspection shall be in accordance with Specification MIL-A-2550 and MIL-1-45208, except as specified herein. 4.2 First artical sample.-Prior to initiation of regular production, a sample shall be submitted in accordance with contract requirements and shall consist of 5 metal part assemblies, 19 se

21、ts of unassembled parts and 50 shear pins from the same lot of shear pins tested by the contractor. shall be manufactured in the same manner using the same materials, equipment, processes and procedures as used in regular production, including packaging and packing shall be the same as used for regu

22、lar production and shall be obtained from the same source of supply. The sample All parts and materials, 4.2.1 Examination and tests.-After inspection and provisional acceptance at source, the sample shall be inspected for all requirements of the drawings and specifications at a Government laborator

23、y or such other facility specified in the contract. 4.2.2 Initial production sample failure.-Failure of the sample to comply with requirements af the drawings and specifications shall result in sample disapproval. 4.3 Inspection provisions. 4.3.1 Lot. 4.3.1.1 Submission of product.-Unless otherwise

24、specified by the contracting officer. formation of lots and presentation of lots shall be in accordance with the “Submission of Product“ proh.sions of MIL-STD-105. 4.3.1.2 Size of lot.-The shipping lots of the metal parts assemblies shall consist of 1200 thrusters maximum provided the homogeneity re

25、quirements of in- spection lots have been retained. the contracting officer, A smaller lot may be shipped upon approval of 4.3.-2 Examination.-One hundred percent examination shall be performe$ for all critical defects. Examination for major and minor defects shall be performed on a defect basis in

26、accordance with the classification of defects contained herein using the sampling plan and associated criteria in Tables II and III. For an individual defect (single characteristic), the criteria in Table II shall be used. For total defects within a major or minor group, the criteria in Table III sh

27、all be used. Inspection for rubber O-rings shall be in accordance with MIL-STD-413. The roughness comparison specimens prescribed in ANSI-Bft6.1-N2, shall be used as a basis of comparison for surface roughness determination. in performing visual examination for such defects as burr and foreign matte

28、r. All nonconforming material shall be rejected. Four power (4X) magnification may be used 4 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-. MIL-T-60102A(MU) TABLE II Ma j or Minor Lot Size Sample Size Accept Reject Accept Reject 1 to 300 100% Exam

29、ination - - - - 301 to 1300 110 1 2 2 3 1301 to 3200 150 2 3 3 4 3201 to 8000 225 3 4 4 5 8001 to 22000 300 4 5 5 6 TABLE III Total allowable defects per sample size Sample Size for Major Defects - - - - - - - 110 150 Number of Characteristics in Class 2- 3 1 2 4- 7 2 3 8 - 19 3.4 20 - 43 4 5 Over 4

30、3 6 8 Sample Size for Minor Defects - - - - - - - 110 150 Number of Characteristics in Class 2- 3 4- 7 8 - 16 17 - 48 Over 48 4.3,2.1 Adapter, Drawing C10520480 Defect CRITICAL None defined MAJOR 2 3 3 4 4 5 6 8 8 11 225 3 4 5 8 11 225 4 5 8 11 17 300 4 5 7 10 14 300 5 7 10 14 20 covering a detail o

31、f Drawing F10520479 Ele t hod of Inspect ion 101. Pitch diameter of external thread, min. 102, Major diameter of external thread, min. 103. Pitch diameter of internal thread, max, 5 Gage Gage Gage Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-4.3.2

32、.1 (Contd) Defect i04 105 106. 107. 108. 109 c 110 c 111. MINOR 201. 202. 203. 2Q4. 205. 206. 207 208 209 210. 211. 212. 213. 214. 215. 216. 217. Minor diameter of internal thread, max. Concentricity of pitch diameter of external Concentricity of boss with pitch diameter of Thread damaged or not ful

33、l Metal defective Protective coating inadequate or defective Burr Foreign matter thread with pitch daimeter of internal thread internal thread Pitch diameter of internal thread, min. Pitch diameter of external thread, max. Diameter of undercut, internal thread Diameter of undercut, external thread D

34、iameter of boss Depth of thread cavity Total length Length of flange Height of boss Diameter of flange Width across flats Width of undercut, external Width of undercut, internal Location of flats Marking missing, incorrect or illegible Radius or chamfer missing or incorrect Surface finish, improper

35、Gage Gage Gage Visual Visual Visual Visual Visual Gage Gage Gage Gage Gage Gage Gage Gage Gage Measure Measure Measure Measure Measure Visual Visual Visual 4.3.2.2 Body, Drawing F10520482, covering a detail of Drawing F10520479. CRITICAL None defined MAJOR 101. Pitch diameter of large thread, max. 1

36、02. Minor diameter of large thread, max. 103. Pitch diameter of thread, bypass pert, max. 104. Minor diameter of thread, bypass port, max. 6 Gage Gage Gage Gage Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-T-bO102A L3 M 9999906 0335598 O M _ M

37、IL-T-6 0102A (MU) 4.3.2.2 (Cont d) Defect Method of Inspection 105. Concentricity cavity f thre d 106. 107. 108, 109 110. 111. 112. 113. 114 115, 116. 117. 118. 119. 120. 121. 122. 123. 124. 125. 126. 127. 128. 129. 130. MINOR 201. 202. 203. 204. 205 206. 207. 208. 209. 210. Concentricity of thread

38、cavity with large Concentricity of head with large thread Concentricity of bore with long cavity Concentricity of grooves with bore Concentricity of counterbore with bore Concentricity of pin holes True position of pin holes Diameter of long cavity, max. Diameter of bore, max. Diameter of pin holes

39、Diameter of grooves Diameter of threaded cavity, max. Diameter of internal undercut, max. if applicable Depth of cavity, bypass port Depth of counterbore, bypass port Length of thread, bypass port Diameter of chamfer, bypass port Angle of chamfer, bypass port Internal radii forward eand, long cavity

40、 Thread damaged or not full Metal defective Protective finish inadequate or defective Surface finish or long cavity and chamfer uf Burr or sharp corners Foreign matter thread bypass port, improper Pitch diameter of large thread, min. Pitch diameter of thread, bypass port, min. Pitch diameter of set

41、screw thread Minor diameter of set screw thread, max. Diameter of long cavity, min. Diameter of bore, min. Diameter of thread cavity, min. Diameter of large thread undercut, max. Diameter of body Diameter of counterbore set screw end 7 avity with long Gage Gage Gage Gage Gage Gage Gage Gage Gage Gag

42、e Gage Gage Gage Gage Gage Gage Measure Measure Measure Visual Visual Visual Gage Visual Visual Visual Gage Gage Gage Gage Gage Gage Gage Gage Gage Gage Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-T-6 0102A(MLJ) 4.3.2. 2 (Cont -d) Defect Diam

43、eter of relief undercut, bypass port Diameter of hole in bypass port Diameter of shoulder Diameter of head Diameter of counterbore, bypass port - Diameter of bypass port Depth to bottom of large cavity Depth to bottom of thread undercut Depth to bottom of large cavity Depth of counterbore Length of

44、effective set screw thread, min. Total length Length to shoulder Length of set screw thread, max. Location of pin holes Location of groove rear long cavity Location of groove near-shear pin hole Loeation of relief undercut Location of bypass port Height of bypass port Width of internal undercut, max

45、., if applicable Width of groove Width of thread undercut Width of relief undercut Length to end of undercut Profile of grooves Profile of bypass port Marking, missing, incorrect or illegible Radius or chamfer missing or incorrect, except as otherwise classified Method of Inspection 2il. 212. 213. 2

46、14. 215. 216. 217 218. 219. 220. 221, 222, 223. 224. 225. 226. 227. 228. 229. 230. 231. 232. 233. 234. 235. 236. 23-7. 238 239. Gage Gage Gage Gage Gage Gage Gage Gage Gage Gage Gage Gage Gage Gage Gage Gage Gage Gage Xeasure Measure Measure Measure Me as ur e Measure Measure Measure Visual Gage Vis

47、ual 4.3.2.3 Breech, Drawing D10520483, covering a detail of Drawing F10520479. CRITICAL None defined MAJOR 101. Pitch diameter of thread on head, min. 102. Major diameter of thread on head, min. 103. Pitch diameter of thread on body, min. 104. Major diameter of thread on body, min. Gage Gage Gage .

48、Gage 8 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,- MIL-T-60102A 13 M 7777706 0335600 5 W 4.3 2.3 (Cont d) Defect 105. 106. 107. 108. 109. 110. 111 112. 113. 114. 115. 116. 117. 118. 119. 120. 121. 122 123. 124. 125. 126. 127. 128. 129. 130. Pitc

49、h diameter of internal thread, max. Minor diameter of internal thread, max. Concentricity of groove with body Concentricity of body with body thread Concentricity of head thread with body thread Concentricity of long cavity with body thread concentricity of striker hole with long cavity Concentricity of boss cavity with long cavity Concentricity of boss with body thread True position of pin h