NAVY MIL-T-46626 C-1994 THRUSTER CARTRIDGE ACTUATED M2A2 ASSEMBLY《M2A2集合发动弹药筒推进器》.pdf

1、. * I INCH-POUND I MIL-T-46626C(OS) 11 Aumist 1994 SUPERSEDING 17 January 1975 ML-T46626B(MU) MILITARY SPECIFICATION THRUSTER, CARTRIDGE ACTUATED, M2A2 ASSEMBLY kis specif cation is approved for use by the Naval Sea Systems Command, Department of the Navy, and is available for use by all Departments

2、 and Agencies of the Departments of Defense. 1. SCOPE 1.1 Scope. This specification covers the requirements for the M2A2 Cartridge Actuated Thruster Assembly (see 6.1). 2. APPLICABLE DOCUMENTS 2.1 Government documents. 2.1.1 Specifications and standards. The following specifications and standards fo

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

4、MILITARY MIL-A-25 50 Ammunition, General Specification For MIL-T-46632 Thruster, Cartridge Actuated, M2A2 Metal Parts Assembly MIL-T-60696 Thruster, Cartridge Actuated, M2A2 Remanufactured Metal Parts Assembly Beneficial comments (recommendations, additions, deletions) and any pertinent data which m

5、ay be of use in improving this document should be addressed to: Commaoder, Mian Head Division, Naval Surface Warfare Center, Standardization Branch (Code 8420), 101 Strauss Avenue, Indian Head, MD 20640-5035, by using the Standardization Document Improvement Proposai D Form 1426) appearing at the en

6、d of this document or by sending a letter. AMSC N/A 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-,-,-flIL-T-4bb2bC H 9999906 1785872 853 MIL-T-46626C( OS) STAND

7、ARDS MILITARY MIL-STD-LOS Sampling Procedures And Tables For Inspection By Attributes MIL-STD-109 Quality Assurance Terms And Definitions MIL-STD-453 Inspection, Radiographic MIL-STD-1168 Ammunition Lot Numbering MS28741 Hose Assembly, Detachable End Fitting, Medium Pressure (Unless otherwise indica

8、ted, 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 s

9、pecification 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) 8593275 Cartridge, Impulse, M43 Assembly DL8593873 Thruster, Cartridge Actuated, M2A2 Ass

10、embly 8797633 Box, Fiberboard (Inner), Packing, Ammunition, For Thruster, Cartridge Actuated, M2A2 8797634 Box, Packing, Ammunition, For Thruster, Cartridge Actuated, M2A2 9235819 Box, Fiberboard (Outer), Alternative, Packing Ammunition, for Thruster, Cartridge Actuated, M2A2 U.S. Air Force TPO 00-9

11、21-5048 Thruster, Cartridge Actuated, M2A2 (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 Provided by IHSNot for ResaleNo reproduction or networking permitted without

12、 license from IHS-,-,- - MIL-T-4bbZbC 99999Ob 1985873 79T Components Head and body 2.2 Order of precedence. 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, supersedes applicab

13、le laws and regulations unless a specific exemption has been obtained. A B C Seating or bottoming Breakaway, min Run On, min (inch pounds) (including A) (inch pounds) 50 600 f 20 400 (inch pounds) 3. REQUIREMENTS 3.1 Materiais. All materials used in the manufacture of the thrusters shall conform to

14、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 the drawings, the bidders s

15、elections shall be clearly stated in the proposal. 3.2 Components. 3.2.1 Primary components. For the purpose of this specification, the M43 impulse cartridge (Drawing 8593275) is defined as a primary component. Only primary components from a single lot shall be used in a production lot of thrusters;

16、 however, one primary component production lot may be used in more than one thruster production lot. 3.2.2 Component parts. Ail component parts shall meet the applicable requirements of MIL-T- 46632 or MIL-T-60696 prior to assembly. 3.3 Torque. Torque requirements shall be as specified in table I. N

17、o movement shall occur upon application of the breakaway torque. TABLE I. Toraue reauirements. 3.4 Trunnion rotation. Upon completion of assembly, the trunnion shall be free to rotate 360 degrees. 3.5 Residual magnetism. The thruster shall not deflect the indicator of the compass more than five degr

18、ees in either direction (see 4.3.2). 3.6 Radiographic examination. Each thruster assembly shall be radiographically examined for defects (see 4.3.3). 3 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-T-4662bC M 9999906 1985874 b2b M 3.7 Functiona

19、l. 3.7.1 Load. The thruster fired under load (see 6.3) shall perform as follows: 3.7.1.1 Stroke and velocity. The thruster shall be capable of delivering a stroke of 5.7 inches, minimum, to move an approved ejection seat either upward or downward with a maximum final velocity of 12 feet per second (

20、fps) so that the ejection seat will be in a final position for ejection. 3.7.2 After load firing. 3.7.2.1 Final lock. The thruster shall be capable of withstanding a compressive load of 11,ooO pounds, minimum, between mounting points without unlocking. 3.7.3 Temperature. The thruster shall comply wi

21、th all the ballistic requirements throughout the temperature range of -65 to +200“F. 3.7.4 Initiation. The thruster shall be fired by a source delivering an output pressure of 700 + 25, - O pounds per square inch gage Sig) at the end of 15 feet of aircraft hose, MS28741-4 at 70 f 5F. 3.7.5 Misfires.

22、 There shall be no misfires. 3.7.6 Mechanical failures. The thruster shall function without mechanical failure (see 6.5.2). 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

23、Metal defects. All components shall be free from cracks, splits, cold shuts, 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. 3.8.3 Foreign ma

24、tter. 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, the contractor is responsible for the performance of ail inspection

25、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 requirements specified herein, unless disapproved by the Government. The G

26、overnment 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 Provided by IHSNot for ResaleNo reproduction or networking permitted without lice

27、nse from IHS-,-,-MIL-T-4bbZbC 99999Ob 1985875 5bZ = 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 i

28、nspection requirements 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 accept

29、able practice to 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 acceptance of defective material. 4.1.2 Quality assurance terms and definitions. Reference shall be made t

30、o MIL-STD-109 to define the quality assurance terms used. 4.1.3 Inspections. Inspections shall be in accordance with MIL-A-2550 and MIL-STD-453. 4.2 Inspection provisions. 4.2.1 Lot. - 4.2.1.1 Submission of product. Unless otherwise specified by the contracting activity, formation, and identificatio

31、n of lots shall be in accordance with MIL-STD-105. 4.2.1.2 Size of lot. The production lot size shall be as specified in the contract (see 6.2). 4.2.2 Examination. One hundred percent examination shall be performed for all critical defects. Examination for major and minor defects shall be performed

32、in accordance with the classification of defects. Four power (4x) magnification may be used for inspection of such defects as burr and foreign matter. When compliance with the applicable requirement is in doubt as a result of visual examination, the characteristic shall be measured or gaged to deter

33、mine acceptability. All nonconforming material shall be rejected. 4.2.2.1 Cartridge, Drawing 8593275, covering a detail of Drawing 8593873. Characteristics Defect Method of Inspection Critical 1 2 3 Mixed cartridges Metal defective Marking missing, incorrect, or illegible Major 101 Foreign matter pr

34、esent Visual Visual Visual Visual Minor 20 1 Case scratched or dented Visual 5 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-4.2.2.2 Assembly, Drawing 8593873, all components except Drawings 8593876, 8593878, 8593882, and MS28775-012. Critical None

35、 defined Major 101 102 Any part missing 103 104 Metal defective 105 106 Burr 107 Foreign matter Cartridge not flush with or below body end Thread damaged or not full Protective finish inadequate or defective Manual/Visual Visual Visual Visual Visual Visual Visual Minor None defined 4.2.2.3 Assembly,

36、 Drawing 8593873, less MILC-5501/10 and MILC-5501/11. Critical 1 2 3 Metal defective Shear pin not engaged in firing pin Head in contact with holding pin Major 101 Totai length 102 Thread damaged 103 Foreign matter Minor None 4.2.2.4 Assembly, Drawing 8593873. Critical 1 Improper assembly 2 Any part

37、 missing 3 Metai defective 4 Foreign matter in gas ports Major 101 102 Marking missing, incorrect, or illegible Trunnion not free to rotate 360“ Gage Visual Visual Gage Visual Visual Visual/X-ray VisuaUX-ray Visual Visual Visual Manual 6 Provided by IHSNot for ResaleNo reproduction or networking per

38、mitted without license from IHS-,-,- MIL-T-4bbZbC 0b 1985877 335 Minor 20 1 202 203 Total length 204 Location of labels incorrect Protective cap or plug missing Setscrews not filled with barrier material 4.2.2.5 Box, Fiberboard (Inner), Ammunition, Drawing 8797633. Critical None defined Major None d

39、efined Minor 20 1 Contents loose 202 Box damaged 203 204 205 Sealing strip broken or missing Marking missing, incorrect, or illegible Cut, damaged, or improperly sealed bag 4.2.2.6 Box, Ammunition, Packing, Drawing 8797634. Critical None defined Major None defined Minor 20 1 Contents loose 202 203 C

40、ontents of box exposed 204 Box damaged 205 206 Number of units incorrect Strapping missing, loose, broken, or improperly engagec Marking missing, incorrect, or illegible Visual Visual Visual Visual Manual Visual Visual Visual Visual Manual Visual/Manua Visual Visual Visual Visual 4.2.2.7 Box, Fiberb

41、oard (Outer), Alternative, Ammunition, Packing, Drawing 9235819. Critical None defined Major None defined 7 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-Minor 20 1 Contents loose 202 Carton broken or damaged 203 204 205 Tape incomplete Number of u

42、nits contained incorrect Marking missing, incorrect, or illegible Sample sue 7 7 7 Manual/Visual Visual Visual Visual Visual Method Temperature (OF) Load (see 3.7.1) -65 to -70 Load (see 3.7.1) Load (see 3.7.1) 65 to 75 195 to 205 4.2.3 Inspection testing. The following tests shall be performed in a

43、ccordance with 4.3. 4.2.3.1 Breakaway torque. 4.2.3.1.1 Head and body. Each head and body assembly shall be subjected to a breakaway torque. Failure of any assembly to comply with the requirements of column C, table I in 3.3 shall be cause for rejection of the assembly. 4.2.3.2 Residual magnetism. E

44、ach assembly shall be subjected to the test for excessive residual magnetism as specified in 4.3.2. Failure of any unit to comply with 3.5 shall be cause for rejection of the assembly. 4.2.3.3 Functional tests. The following tests shall be performed by the Government. 4.2.3.3.1 Ballistics. Twenty-on

45、e units shall be tested to determine compliance with 3.7. The units shall be temperature conditioned as provided in table II and 4.3.4.2. Failure of any unit to comply with 3.7.1 through 3.7.6 shall be cause for rejection of the lot. TABLE II. Conditionin? temDerature. 4.2.3.3.2 Retest. There shall

46、be no retests. 4.2.3.3.3 Test failure. If a test failure is attributable to an assignable cause, excluding the test thruster, the original test results shall be discarded and that test reconducted. 4.3 Test methods and procedures. 4.3.1 Breakaway torque. A torque wrench, set at the torque requiremen

47、ts specified in table I, shall be used in conjunction with a fixture to determine the adequacy of the joints. 8 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-4.3.2 Residual magnetism. The assembly shall be tested for excessive residual magnetism us

48、ing &I approved compass in an area free of local magnetic effects by placing the assembly 5 inches from the end at the same height as the compass, in the north-south horizontal position (head end at south) with the compass set in an east-west heading. The assembly shall be moved at a speed no greate

49、r than 10 feet per minute past the compass for its entire length, rotated 90 degrees in the horizontal position about its longitudinal axis, and moved slowly back past the compass. This procedure shall be repeated for each 90 degree rotation of the assembly for four full passes. 4.3.3 Radiographic examination. All assembled thrusters shall be radiographically examined in accordance with MIL-STD-453, with the