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本文(NAVY MIL-T-60801 A-1993 THRUSTER CARTRIDGE ACTUATED M13 REMANUFACTURED METAL PARTS ASSEMBLY《M13改造金属零件集合发动弹药筒推进器》.pdf)为本站会员(周芸)主动上传,麦多课文库仅提供信息存储空间,仅对用户上传内容的表现方式做保护处理,对上载内容本身不做任何修改或编辑。 若此文所含内容侵犯了您的版权或隐私,请立即通知麦多课文库(发送邮件至master@mydoc123.com或直接QQ联系客服),我们立即给予删除!

NAVY MIL-T-60801 A-1993 THRUSTER CARTRIDGE ACTUATED M13 REMANUFACTURED METAL PARTS ASSEMBLY《M13改造金属零件集合发动弹药筒推进器》.pdf

1、MIL-T-bO80IIA = 999990b II949598 383 1 INCH-POUND I MILITARY SPECIFICATION MIL-T-60801A 29 April 1993 SUPERSEDING 25 July 1968 MIL-T-60801 THRUSTER, CARTRIDGE ACTUATED, M13 REMANUFACTURED METAL PARTS ASSEMBLY is specijcation is approved for use by all Departments and Agencies of the Department of De

2、fense. 1. SCOPE 1.1 Scope. This specification covers the requirements for the M13 Cartridge Actuated Thruster Remanufactured 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

3、 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 supplements thereto, cited in the solicitation (see 6.2). SPECIFICATIONS MILITARY MIE

4、-A-2550 Ammunition, General Specification For STANDARDS MILITARY MIL-STD-105 MIL-STD-109 MIL-STD-413 Sampling Procedures And Tables For Inspection By Attributes Quality Assurance Terms And Definitions Visual Inspection Guide for Elastomeric O-rings Beneficial comments (recommendations, additions, de

5、letions) and any pertinent 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 20640-5000, by using the Standardization Document Improvement

6、Proposal D Form 1426) appearing 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-,-,-O MIL-T-6080 1 A (

7、Unless otherwise indicated, 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 drawing

8、s form a part of this specification to the extent specified herein. Unless otherwise specified, the issues are those cited in the solicitation (see 6.2). DRAWINGS Indian Head Division, Naval Surface Warfare Center (CAGE Codes 19200 and 19203) 10520974 8836128 8836129 92 17388 U.S. Air Force TPO 00-7

9、56-350 1 Thruster, Cartridge Actuated, M13, Metal Parts Assembly Box, Fiberboard (inner), Packing, Ammunition, For Thruster, Cartridge Actuated, M13 or M19 Box, Packing, Ammunition, For Thruster, Cartridge Actuated, M13 or M19 Box, Fiberboard (Outer), Alternative, Packing Ammunition, for Thruster, C

10、artridge Actuated, M13 or M19 Thruster, Cartridge Actuated, M13 (Application for copies should be addressed to: Commander, Naval Surface Warfare Center, 101 Strauss Avenue, Data Control Branch (Code 8410), Indian Head, MD 20640-5035.) 2.2 Order of precedence. In the event of a conflict between the t

11、ext of this document and the references cited herein, 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 Materials. All materiais used in the manufacture of the t

12、hrusters 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 Navy design activity prior to manufacture. When alternate materials or methods of manufacture are specified on t

13、he drawings, the bidders selections shall be clearly stated in the proposai. The remanufactured thruster metal parts assembly shall contain new shear pins, new O-rings, and new setscrews (see 6.5). 3.2 Hydrostatic pressure. The body shall withstand a hydrostatic pressure of 11,500 pounds per square

14、inch (psi) for 15 seconds, minimum, without leaking, deformation, or mechanical failure (see 6.3.1). 2 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-. Component Piston and piston fastener MIL-T-b08OLA W Ob 1799600 8bl B C Seating or Bottoming (inch

15、 pounds) Breakaway (inch pounds) 100 f 20 75 min MIL-T-60801 A 0 3.3 Torque. Torque requirements shall be as specified in table I. No movement or deformation shall occur upon application of the breakaway torque. TABLE I. Toraue reauirements. 3.4 Protective finish. Protective finish shall be in accor

16、dance with the applicable specifications and drawings and shall apply to all surfaces of the component regardless of configuration. Remanufactured exterior components (see 6.3.2) shall have the existing protective finish stripped and the specified protective finish reapplied. When there are only sma

17、ll surface areas of exposed base metal on the aluminum exterior components (body assembly and end cap) it may be permissible to treat the surfaces with chemical film Class 1A as specified in MIL-C-5541. 3.5 Residual magnetism. The metal parts assembly shall not deflect the indicator of the compass m

18、ore than five degrees in either direction using the procedures of 4.5.4. 3.6 Shear pin strength. The shear pin, after application of protective finish, shall shear when a load of 41 ti 5 pounds is applied at the steady rate of 0.125 inch per minute. 3.7 Metal parts assembly. Parts shall be combined

19、to produce an assembly which conforms to the requirements of the metal parts assembly drawing. All threaded joints shall be assembled with sufficient torque to bottom components, except as noted in table I. 3.7.1 Integrated plant products. When remanufacturing and loading of the assembly is performe

20、d in an integrated plant, the metal parts assembly requirement may be waived and the residual magnetism requirement performed on the loaded assembly only. 3.7.2 Threaded component parts. Class 2A or 2B thread gage shall be used on remanufactured component parts inspection versus class 3A or 3B threa

21、d gage required on new hardware for thrusters. 3.8 Workmanship. Thrusters shall be free of cracks, splits, or other defects which might prevent proper mating with connecting parts or proper functioning of the device. 3.8.1 Metal defects. All components shall be free from cracks, splits, cold shuts,

22、inclusions, porosity, or any similar defect. 3.8.2 Burr. No part shall have a burr which might interfere with the assembly or function of the item or which might be injurious to personnel handling the item. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS

23、-,-,-J MIL-T-bO8OLA 9999906 194bOL 7T8 MIL-T-60801A 3.8.3 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 otherwise specified in the contract or purchase order,

24、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 facilities suitable for the performance of the inspection requir

25、ements 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 services conform to prescribed requirements (see 6.2). 4.1.1 Responsib

26、ility 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 requirements in the specification shall not relieve the c

27、ontractor 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 ascertain conformance to requirements; however, th

28、is does not authorize submission of known defective material, either indicated or actual, 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 Ins

29、pections. Inspections shall be in accordance with MIL-A-2550. 4.2 Inspection conditions. Unless otherwise specified (see 6.2), all inspections shall be performed under the following conditions: a. b. Altitude: sea level c. d. Atmospheric pressure: 14.7 psi Temperature: room ambient (68 to 77F) Humid

30、ity: 50 percent relative, maximum 4.3 Quality conformance inspection. 4.3.1 Lot. 4.3.1.1 Submission of product. Unless otherwise specified by the contracting activity, formation and identification of lots shall be in accordance with MIL-STD-105. 4.3.1.2 Size of lot. For the purpose of identification

31、 and shipment, the shipping lots of metal parts assemblies shall consist of 1200 assemblies, maximum, provided the homogeneity requirements of inspection lots have been retained. 4 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-NIL-T-BOIA Ob l194960

32、2 634 = MIL-T-6080 1A 0 4.3.2 Examination. On reprocessed parts, 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. Four power (4x) magnification m

33、ay 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 examination, the characteristic shall be measured or gaged

34、 to determine acceptability. All nonconforming material shall be rejected. 4.3.2.1 Examination of reclaimed parts. Examination of reusable parts, which require no reprocessing, shall be limited to inspection of defects that require visual type inspection. One hundred percent examination shall be per

35、formed for all such defects. All nonconforming parts shall be reprocessed or rejected. 4.3.2.2 Ring, Drawing 10520489, covering a detail of Drawing 10520974. Characteristics Defect Method of Inspection Critical None defined Major 102 103 104 Metal defective Protective finish inadequate or defective

36、Burr Foreign matter Visual Visual Visual Visual Minor None defined 4.3.2.3 Pin, Firing, Drawing 10520978, covering a detail of Drawing 10520974. Critical None defined Major 101 102 103 104 Metal defective Protective finish inadequate or defective Burr or sharp corner Foreign matter visual Visual Vis

37、ual Visual Minor None defined 5 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-T-6080 1 A 4.3.2.4 Cap, Base, Drawing 10520982, covering a detail of Drawing 10520975. Critical None defined Major 10 1 102 Metal defective 103 104 Burr or sharp corn

38、er 105 Foreign matter Threads damaged or not full Protective finish inadequate or defective Visual Visual Visual Visual Visual Minor None defined 4.3.2.5 Fastener, Piston, Drawing 10520983, covering a detail of Drawing 10520980. Critical None defined Major 101 102 Metal defective 103 104 Burr 105 Fo

39、reign matter Threads damaged or not full Protective finish inadequate or defective Minor None defined 4.3.2.6 Body, Drawing 10520976, covering a detail of Drawing 10520974. Critical None defined Major 101 102 103 104 1 05 Threads damaged or not full Metal defective Protective finish inadequate or de

40、fective Burr or sharp corners Foreign matter Visual Visual Visual Visual Visual Visual Visual Visual Visual Visual Minor None defined 6 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-T-bO801A 9999906 1949604 407 MIL-T-60801A 4.3.2.7 Piston, Draw

41、ing 10520984, covering a detail of Drawing 10520979. Critical None defined Major 101 102 103 104 105 Threads damaged or not full Metal defective Protective finish inadequate or defective Burr or sharp corners Foreign matter Visual visual visual visual visual Minor None defined 4.3.2.8 10520974. Base

42、 Cap and Pellet Assembly, Drawing 10520975, covering a detail of Drawing Critical None defined Major 101 102 103 104 Pellet missing, loose, or improperly inserted Thread damaged Burr Foreign matter Manual/Visual Visual visual Visual Minor None defined 4.3.2.9 Piston and Pellet Assembly, Drawing 1052

43、0979, covering a detail of Drawing 10520974. Critical None defined Major 101 102 103 104 Pellet missing, loose, or improperly inserted Thread damaged Burr Foreign matter ManuaWisual Visual Visual visual Minor None defined 7 Provided by IHSNot for ResaleNo reproduction or networking permitted without

44、 license from IHS-,-,-MIL-T-bO801A W 999990b 1949605 343 D MIL-T-60801A 4.3.2.10 Piston Fastener and Pellet Assembly, Drawing 10520980, covering a detail of Drawing 10520974. Critical None defined Major 101 102 103 104 Pellet missing, loose, or improperly inserted Thread damaged Visual Burr Visual F

45、oreign matter Visual ManualNisual Minor None defined 4.3.2.11 Breech and Firing Pin Subassembly, consisting OE Breech, Drawing 10520977; Firing Pin, Drawing 10520978; and O-ring, MS29513-9; covering a detail of Drawing 10520974. Critical 1 Firing pin protrusion Major 101 102 Burr 103 Foreign matter

46、Protective finish inadequate or defective Minor None defined 4.3.2.12 Metal Parts Assembly, Drawing 10520974. Critical None defined Major 101 102 103 104 105 Minor 20 1 202 203 204 Piston not free to rotate 360 degrees clockwise Any part missing, except as otherwise classified Improper assembly Thre

47、ad damaged or not full Foreign matter Protective finish inadequate or defective Barrier material missing from setscrews Protective cap or plug missing Pellet missing from piston fastener Gage Visual Visual Visual Manual Visual Visual Visual Visual Visual Visual Visuai Visual 8 Provided by IHSNot for

48、 ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-T-bO80LA = 9999906 L949bOb 2BT = MIL-T-60801A 4.3.2.13 Breech, Drawing 10520977, covering a detail of Drawing 10520974. Critical 1 O Surface finish or cavity improper Major None defined Minor None defined 4.3.2.14 Box, F

49、iberboard (Inner), Packing, Ammunition, Drawing 8836128. Critical None defined Major None defined Minor 20 1 Contents loose 202 Box damaged 203 Marking missing, incorrect, or illegible 204 Cut, damaged, or improperly sealed bag 4.3.2.15 Box, Packing, Ammunition, Drawing 8836129. Critical None defined Major None defined Minor 20 1 202 203 204 205 206 Gage Manual Visual Visual Visual Contents loose VisuallManu

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