NAVY MIL-T-46591 B-1993 THRUSTER CARTRIDGE ACTUATED M15 ASSEMBLY《M15集合发动弹药筒推进器》.pdf
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1、.J * MIL-T-465919 = 9999906 1972333 929 I INCH-POUND I MIL-T-4659 1 B 30 April 1993 SUPERSEDING 29 May 1969 MIL-T-4659 1 A(MU) MILITARY SPECIFICATION THRUSTER, CARTRIDGE ACTUATED, M15 ASSEMBLY is specijcation is approved for use by all Departments and Agencies of the Depament of Defense. 1. SCOPE 1.
2、1 Scope. This specification covers the requirements for the M15 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 form a part of this document to the extent specified herein
3、. 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, General Specification For
4、 MIL-T-46590 Thruster, Cartridge Actuated, M15 Metal Parts Assembly MIL-T-60694 Thruster, Cartridge Actuated, M 15 Remanufactured Metal Parts Assembly Beneficial comments (recommendations, additions, deletions) and any pertinent data which may be of use in improving this document should be addressed
5、 to: Commander, Indian Head Division, Naval Surface Warfare Center, Standardization Branch (Code 8420), 101 Strauss Avenue, indian Head, MD 20640-5035, by using the Standardization Document Improvement Proposal (DD Form 1426) appearing at the end of this document or by sending a letter. AMSC N/A FSC
6、 1377 DISTRIBUTION STATEMENT A: Approved for public release; distribution is unlimited. O Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-STANDARDS MILITARY MIL-STD-105 Sampling Procedures And Tables For Inspection By Attributes MIL-STD-109 Quality A
7、ssurance Terms And Definitions MIL-STD-453 Inspection, Radiographic MIL-STD-1168 Ammunition Lot Numbering MS28741 Hose Assembly, Detachable End Fitting, Medium Pressure (Unless otherwise indicated, copies of federal and military specifications and standards are available from Standardization Documen
8、ts 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 specification to the extent specified herein. Unless otherwise specified, the issues are those cited in the
9、solicitation (see 6.2). DRAWINGS Naval Surface Warfare Center, Indian Head (CAGE Codes 19200 and 19203) 8596708 Cartridge, Impulse, M94 Assembly 8 85 8440 Box, Packing, Ammunition, For Thruster, Cartridge Actuated, M 15 885844 1 Box, Fiberboard (Inner), Packing, Ammunition, For Thruster, Cartridge A
10、ctuated. M 15 DL 10520875 Thruster, Cartridge Actuated, M15 Assembly 92 17560 Box, Fiberboard (Outer), Alternative, Packing Ammunition, for Thruster, Cartridge Actuated, M15 U.S. Air Force TPO 00-607-03 14 Thruster, Cartridge Actuated, M 15 (Application for copies should be addressed to: Commander,
11、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 herein, the text of this document takes precedence. Nothing in this d
12、ocument, however, supersedes applicable laws and regulations unless a specitic exemption has been obtained. 2 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-T-46591B 9Ob 1972335 7TL W c MIL-T-4659 1B 3. REQUIREMENTS A Scsiing or bottoming (inch
13、pounds) 600 + 30 Componcnts Firing pin housing and body 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 therefrom has been obtained from the cogni
14、zant 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. B Breakaway, min (inch pounds) 400 3.2 Components. 3.2.1 Primary components. For the purpose of this speci
15、fication, the M94 impulse cartridge (Drawing 8596708) 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 parts
16、. All component parts shall meet the applicable requirements of MIL-T- 46590 or MIL-T-60694 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. TABLE i. Toruue requirements. 3.4 Residual magnetism. The
17、 thruster shall not deflect the indicator of the compass more than five degrees in either direction (see 4.3.2). 3.5 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, shall perform
18、as follows (see 6.3). 3.7.2 Thrust. With the piston rod connected to an 11-pound mass, the thruster shall deliver sufficient thrust to shear a 3750-pound shear pin located at zero inches stroke and simultaneously overcome a 2250-pound resistive load from zero inches stroke to completion of stroke. 3
19、.7.3 Stroke. Complete a stroke of 4.42 inches, minimum. 3 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-. 1 MIL-T-4b591B W 999990b I1972336 b38 MIL-T-4659 1 B 3.7.4 Operating time. Time between initiation of cartridge to completion of stroke shall
20、not be less than 750 milliseconds. 3.7.5 After load firing. 3.7.5.1 Final lock. The thruster shall be capable of withstanding a static tensile load of 15,000 pounds, minimum, applied at the rate of O. 125 inches per minute, between the mounting points without unlocking. 3.7.6 Temperature. The thrust
21、er shall comply with all the ballistic requirements throughout the temperature range of -65 to +200“F. 3.7.7 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 5
22、F. 3.7.8 Misfires. There shall be no misfires. 3.7.9 Mechanical failures. The thruster shall function without mechanical failure (see 6.5.1). 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
23、the device. 3.8.1 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
24、. 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, the contractor is responsible for the performance
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