1、 INCH-POUND MIL-DTL-60201D 14 December 2010 SUPERSEDING MIL-T-60201C 21 September 1992 DETAIL SPECIFICATION THRUSTER, CARTRIDGE ACTUATED, M25A1 ASSEMBLY This specification is approved for use by all Departments and Agencies of the Department of Defense. 1. SCOPE 1.1 Scope. This specification covers
2、the requirements for the M25A1 Cartridge Actuated Thruster 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 this specification o
3、r 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 or not they are list
4、ed. 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 solicitation or contract.
5、 DEPARTMENT OF DEFENSE SPECIFICATIONS MIL-A-2550 Ammunition, General Specification For MIL-T-50713 Thruster, Cartridge Actuated, M25A1 Remanufactured Metal Parts Assembly MIL-T-60561 Thruster, Cartridge Actuated, M25A1 Metal Parts Assembly Comments, suggestions, or questions on this document should
6、be addressed to Department of the Navy, Indian Head Division, NSWC, Code E12P, Document Control, 4123 Artisans Court, Suite 103, Indian Head, Maryland 20640-5085, OFFICIAL BUSINESS, or emailed to amanda.pennnavy.mil. Since contact information can change, you may want to verify the currency of this a
7、ddress information using the ASSIST Online database at https:/assist.daps.dla.mil/.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-,-,-MIL-DTL-60201D 2 DE
8、PARTMENT OF DEFENSE STANDARDS MIL-STD-1168 Ammunition Lot Numbering and Ammunition Data Card MS28741 Hose Assembly, Detachable End Fitting, Medium Pressure (Copies of these documents are available online at https:/assist.daps.dla.mil/ or from the Standardization Documents Order Desk, Building 4D, 70
9、0 Robbins Avenue, Philadelphia PA 19111- 5094.) 2.2.2 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 are those cited in th
10、e solicitation or contract. DRAWINGS Naval Surface Warfare Center, Indian Head (CAGE Codes 19200 and 19203) 10520589 Cartridge, Impulse, M127 Assembly 8797741 Box, Fiberboard (Inner), Packing, Ammunition, For Thruster, Cartridge Actuated, M5A2, M20A1, or M25A1 8797742 Box, Packing, Ammunition, For T
11、hruster, Cartridge Actuated, M5A2, M20A1, or M25A1 DL11730533 Thruster, Cartridge Actuated, M25A1 Assembly 9217579 Box, Fiberboard (Outer), Alternative, Packing Ammunition, for Thruster, Cartridge Actuated, M5A2, M20A1, or M25A1 U.S. Air Force TPO 00-554-3103 Thruster, Cartridge Actuated, M25A1 (App
12、lication for copies should be addressed to the DEPARTMENT OF THE NAVY, Indian Head Division, NSWC, Code E12P, Document Control, 4123 Artisans Court, Suite 103, Indian Head, Maryland 20640-5085, OFFICIAL BUSINESS.) 2.3 Non-Government publications and drawings. The following documents form a part of t
13、his document to the extent specified herein. Unless otherwise specified, the issues of the documents are those cited in the solicitation or contract AMERICAN NATIONAL STANDARDS INSTITUTE (ANSI)/AMERICAN SOCIETY FOR QUALITY CONTROL (ASQC) ANSI/ASQ Z1.4 Sampling Procedures And Tables For Inspection By
14、 Attributes ANSI/ISO/ASQ A8402 Quality Assurance Terms And Definitions Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-DTL-60201D 3 (Copies of this document are available online at http:/e-standards.asq.org/ or from the American Society for Quali
15、ty, 600 North Plankinton Avenue, Milwaukee, WI 53203.) AMERICAN SOCIETY FOR TESTING AND MATERIALS (ASTM) ASTM E 1742 Inspection, Radiographic (Copies of these documents are available online at www.astm.org or from the American Society for Testing and Materials Customer Service, 100 Barr Harbor Drive
16、, West Conshohocken, PA 19428-2959.) 2.2 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, supersedes appl
17、icable laws and regulations unless a specific exemption has been obtained. 3. REQUIREMENTS 3.1 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 therefr
18、om 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 selections shall be clearly stated in the proposal. 3.2 Components. 3.2.1 Primary components. For the purpose of this speci
19、fication, the M127 impulse cartridge (Drawing 10520589) is defined as a primary component. Only primary components from a single lot shall be used in a production lot of thrusters; however, one primary component production lot may be used in more than one thruster production lot. 3.2.2 Component par
20、ts. All component parts shall meet the applicable requirements of MIL-T-50713 or MIL-T-60561 prior to assembly. 3.3 Torque. Torque requirements shall be as specified in table I. No movement shall occur upon application of the breakaway torque. Provided by IHSNot for ResaleNo reproduction or networki
21、ng permitted without license from IHS-,-,-MIL-DTL-60201D 4TABLE I. Torque requirements. Components A B C Run On, min (inch pounds) Seating or bottoming (including A) (inch pounds) Breakaway, min (inch pounds) Head and retainer guide 50 300 20 200 Retainer guide and sleeve after insertion of cartridg
22、e 300 20 200 Head and body1/50 600 20 400 Cap screws 20 minimum 10 1/At no time will torque be applied between the piston and body assembly. 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 th
23、e indicator of the compass more than five degrees in either direction (see 4.3.2). 3.6 Radiographic examination. Each thruster assembly shall be radiographically examined for defects (see 4.3.3). 3.7 Functional. 3.7.1 Load. The thruster fired under load (see 6.3) shall perform as follows: 3.7.1.1 Th
24、rust. With the piston connected to a 50 pound weight, the thruster shall deliver sufficient thrust to overcome a 3,000 pound resistive load, horizontally, throughout its total stroke of 5 inches minimum. The resistive load shall not be applied on the piston before initial movement. 3.7.1.2 Operating
25、 time. The time from initial thrust rise to completion of the piston stroke shall be 30 milliseconds, minimum, and 90 milliseconds, maximum. 3.7.1.3 Maximum thrust. A thrust-time record shall be made for each ballistic firing. The maximum thrust will be computed from that trace and recorded for info
26、rmation purposes on the firing sheet. 3.7.2 Ignition delay. The ignition delay time shall not exceed 65 milliseconds (see 6.5.1). 3.7.3 Temperature. The thruster shall comply with all the ballistic requirements throughout the temperature range of -65 to +200F. 3.7.4 Initiation. The thruster shall be
27、 fired by a source delivering an output pressure of 700 + 25, - 0 pounds per square inch gage (psig) at the end of 15 feet of aircraft hose, MS28741-4 at 70 5F. 3.7.5 Misfires. There shall be no misfires. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,
28、-,-MIL-DTL-60201D 53.7.6 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 Metal defe
29、cts. 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 matter. No p
30、art or assembly shall contain chips, dirt, grease, rust, corrosion, or other foreign matter. 4. VERIFICATION 4.1 Classification of inspections. a. Quality conformance inspection 4.1.1 Quality assurance terms and definitions. Reference shall be made to ANSI/ISO/ASQ A8402 to define the quality assuran
31、ce terms used. 4.1.2 Inspections. Inspections shall be in accordance with MIL-A-2550 and ASTM E 1742. 4.2 Inspection provisions. 4.2.1 Lot. 4.2.1.1 Submission of product. Unless otherwise specified by the contracting activity, formation, and identification of lots shall be in accordance with ANSI/AS
32、Q Z1.4. 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 in accordance with the classification of de
33、fects. 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 determine acceptability. All nonconforming mater
34、ial shall be rejected. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-DTL-60201D 64.2.2.1 Cartridge, Drawing 10520589, covering a detail of Drawing 11730533. Characteristics Defect Method of Inspection Critical 1 Mixed cartridges Visual 2 Metal
35、defective Visual 3 Marking missing, incorrect, or illegible Visual Major 101 Foreign matter present Visual Minor 201 Case scratched or dented Visual 4.2.2.2 Retainer, Guide Subassembly, consisting of Guide Retainer and Pellet Assembly 10521616, Shear Pin 10521618, Firing Pin 8593864, and O-Ring MS29
36、513-12, covering a detail of Drawing 11730533. Critical 1 Striker hole obstructed Visual Major 101 Foreign matter Visual Minor None defined 4.2.2.3 Head Sub-Assembly, consisting of Head 10521455, Guide Retainer and Pellet Assembly 10521616, Sleeve 10521617, Shear Pin 10521618, Firing Pin 8593864, Ca
37、rtridge 10520589, and O-Rings MS29513-12 and MS29513-212, covering a detail of Drawing 11730533. Critical None defined Major 101 Thread damaged or not full Visual 102 Protective finish inadequate or defective Visual 103 Burr Visual 104 Foreign matter Visual Minor 201 Excess sealant not removed Visua
38、l Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-DTL-60201D 74.2.2.4 Assembly, Drawing 11730533, less NAS845 and NAS814. Critical 1 Foreign matter in gas port Visual 2 Shear pin not engaged in firing pin Gage Major 101 Total length Gage 102 Thre
39、ad damaged Visual Minor 201 Sealant or coating compound missing Visual 4.2.2.5 Assembly, Drawing 11730533. Critical 1 Improper assembly Visual/X-ray 2 Any part missing Visual/X-ray 3 Metal defective Visual Major 101 Marking missing, incorrect, or illegible Visual 102 Foreign matter Visual Minor 201
40、Trunnion not free to rotate 360 degrees Manual 202 Location of labels incorrect Visual 203 Protective cap or plug missing Visual 204 Total length Visual 4.2.2.6 Box, Fiberboard (Inner), Ammunition, Drawing 8797741. Critical None defined Major None defined Minor 201 Contents loose Manual 202 Box dama
41、ged Visual 203 Sealing strip broken or missing Visual 204 Marking missing, incorrect, or illegible Visual 205 Cut, damaged, or improperly sealed bag Visual Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-DTL-60201D 84.2.2.7 Box, Ammunition, Packi
42、ng, Drawing 8797742. Critical None defined Major None defined Minor 201 Contents loose Manual 202 Strapping missing, loose, broken, or improperly engaged Visual/Manual 203 Contents of box exposed Visual 204 Box damaged Visual 205 Marking missing, incorrect, or illegible Visual 206 Number of units in
43、correct Visual 4.2.2.8 Box, Fiberboard (Outer), Alternative, Ammunition, Packing, Drawing 9217579. Critical None defined Major None defined Minor 201 Contents loose Manual/Visual 202 Carton broken or damaged Visual 203 Number of units contained incorrect Visual 204 Marking missing, incorrect, or ill
44、egible Visual 205 Tape incomplete Visual 4.2.3 Inspection testing. The following tests shall be performed in accordance with 4.3. 4.2.3.1 Breakaway torque. 4.2.3.1.1 Retainer guide and sleeve. Each retainer guide and sleeve subassembly shall be subjected to a breakaway torque. Failure of any subasse
45、mbly to comply with the requirements of column C, table I in 3.3 shall be cause for rejection of the subassembly. 4.2.3.1.2 Head and retainer guide. Each head and retainer guide subassembly shall be subjected to a breakaway torque. Failure of any subassembly to comply with the requirements of column
46、 C, table I in 3.3 shall be cause for rejection of the subassembly. 4.2.3.1.3 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. Provide
47、d by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-DTL-60201D 94.2.3.2 Residual magnetism. Each 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 reject
48、ion 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-one 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 com
49、ply with 3.7.1 through 3.7.6 shall be cause for rejection of the lot. TABLE II. Conditioning temperature. Sample size Method Temperature (F) 7 7 7 Load (see 3.7.1) Load (see 3.7.1) Load (see 3.7.1) -65 to -70 65 to 75 195 to 205 Ballistic test samples for small lots shall be: Lot size Ballistic Sample
