ARMY MIL-C-60458-1967 CARTRIDGE 105MM HE ROCKET ASSISTED XM548 DELAY ASSEMBLY FOR《XM548型105MM HE炮弹火箭辅助迟延装载》.pdf
《ARMY MIL-C-60458-1967 CARTRIDGE 105MM HE ROCKET ASSISTED XM548 DELAY ASSEMBLY FOR《XM548型105MM HE炮弹火箭辅助迟延装载》.pdf》由会员分享,可在线阅读,更多相关《ARMY MIL-C-60458-1967 CARTRIDGE 105MM HE ROCKET ASSISTED XM548 DELAY ASSEMBLY FOR《XM548型105MM HE炮弹火箭辅助迟延装载》.pdf(15页珍藏版)》请在麦多课文档分享上搜索。
1、- =-. MIL-C-601158 13 79777Ob 03386117 b /- 5-39-6 MIL-C-60458 (MU) 27 October i967 Super se des 1 February1966 PA-PD-2 781 MILITARY SPECIFICATION CARTRIDGE, 105MM, HE, ROCKET ASSISTED, XM548, DELAY ASSEMBLY FOR 1. SCOPE 1.1 This specification covers the quality assurance provisions for the delay as
2、sembly parts and loading, assembly and packing for the 105MM Rocket Assisted Cartridge, XM548. 2. APPLICABLE DOCUMENTS 2.1 The following documents of the issue in effect on date of invitation for bids or requests for proposal form a part of this specification to the extent specified herein. SPECIFIC
3、ATIONS MILITARY MIL-E-463 - Ethyl Alcohol, for Ordnance Use. MIL-A-2550 - Ammunition and Special Weapons, MIL-C-13739 - Composition, Delay. General Specification for. . MIL-1-45607 - Inspection Equipment, Supply and Maintenance of. STANDARDS MILITARY MIL-STD-105 - Sampling Procedures and Tables for
4、Inspection by Attributes. MIL-STD-109 - Quality Assurance Terms and Definitions. MIL-STD-1168 - Lot Numbering of Ammunition. MIL-STD-1235 - Single or Multilevel Continuous Sampling Procedures and Tables for Inspection by Attributes. FSC: 1315 . THIS DOCUMENT CONTAINS /*5 PAGES. Provided by IHSNot fo
5、r ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-C-60458 (MU) DRAWINGS ARMY 9212402 - Delay Assembly for 105MM RAP. 9212403 - Washer. 9212404 - Housing. PUBLICATIONS ARMY ET-9212402 - Equipment Tabulation. (Copies of specifications standards, drawings and publications
6、 required by suppliers in connection with specific procurement functions should be obtained from the procuring activity or as directed by the contracting officer. 3. REQUIREMENTS 3.1 Material. - Materials shall be in accordance with the applicable drawings and specifications. shall comply with all r
7、equirements specified on drawing 9212402, 9212403, and 9212404 and with all requirements specified in applicable specifications. 3.2 Parts and assemblies. - The parts and assemblies 3.3 Pyrotechnic Composition. - The flash, delay, and igniter composition shall comply with applicable drawing require-
8、 ments. 3.3.1 Process (see 6.4).-The delay composition shall be manu- factured using conventional wet blending techniques and shall employ ethyl alcohol, grade III or V of NIL-E-463 as a blending medium and passed through a No. 16 mesh screen to provide initial granulation. 3.3.2 Particle Size. - Th
9、e dried delay composition shall be sieved and shall be retaineci on an 80 mesh screen. 3.3.3 Moisture content. - The moisture content of the flash, delay, and igniter composition at the time of loading shall not exceed 0.05 percent when tested in accordance with 4.4.3. 2 Provided by IHSNot for Resal
10、eNo reproduction or networking permitted without license from IHS-,-,-. . MIL-C-bO458 13 = 777770b 0338651 4 MIGC-60458 (MU) 3.4 Flight Test 3*4.1 Pyrotechnic Material Acceptance (see 4.3.3.4.1) - plus 70F - After conditioning at 70F for a period of 12 hours, minimum the delays shall be fired at a p
11、roving ground as specified in 4.4.1.1. The average delay time shall be 15.75 seconds plus or minus 0.75 seconds and the standard deviation of the delays shall not exceed 0.50 seconds. 3.4.2 Delay Assembly Accetpance 3.4.2.1 Plus 155OF - After conditioning at 155OF for a period of 24 hours minimum, t
12、he delay assembly shall be flight tested at a proving ground (see 4.4.1.2.1). The average delay time shall be 12.5 seconds plus or minus 1.5 seconds and the standard deviation shall be no greater than 0.8 seconds. a period of 24 hours minimum, the delay assembly shall be flight tested at a proving g
13、round (see 4.4.1.2.2). time shall be 20.0 seconds plus or minus 1.5 seconds and the standard deviation shall be no greater than 0.8 seconds. 3.4.2.2 Minus 65OF - After conditioning at minus 65OF for The average delay 3.5 Pyrotechnic Porosity test. - The pressure recorded at the exit end of the delay
14、 assembly, 80 seconds after application of the nitrogen gas, shall not be greater than i35 P.S.I. above the zero pressure reference. The pressure recorded at the exit ad of the delay assembly, 110 seconds after application of the nitrogen gas, shall be no less than 10 P.S.I. and no greater than 200
15、P.S.I. above the zero pressure reference. The test shall be conducted in accordance with 4.4.2. 3.6 Workmanship. - All parts and assemblies shall be fab- ricated and loaded in a thorough workmanlike manner. be free of burrs, sharp edges, cracks, dirt, rust and other foreign matter. to any part nor s
16、hall the parts be contaminated by the cleaning agent. a few light scratches not exposing base material. All required markings shall be neat and sharply defined. 3.7 First Article Inspection. - This specification makes provisions for first article inspection. Requirements for the submission of first
17、article samples by the contractor shall be They shall The cleaning method used shall not be injurious Exterior surface coatings shall be continuous except for as specified in 3.8 Crimp of withstanding in 4.3.3.5. the contract. strength. - The washer crimp shall be capable a 500 pound minimym load wh
18、en tested as specified 3 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,- MIL-C-bO458 13 m 9999906 0338652 6 I MIL-C-60458 (MU) 4. QUALITY ASSURANCE PROVISIONS 4.1 General quality assurance provisions.-Unless otherwise specified in the contract or pu
19、rchase order,the supplier is responsible for the performance of all inspection requirements as specified herein. Except as otherwise specified, the supplier may utilize his own facilities or any commercial laboratory accept- able to the Government. The Government reserves the right to perform any of
20、 the inspections set forth in the specification where such inspections are deemed necessary to assure supplies and services conform to prescribed requirements. Reference shall be made to Standard MIL-STD-109 in order to define terms used herein. The provisions of Specification MIL-A-2550 shall apply
21、. Submission of product.-At the time the completed lot of product is submitted to the Government for acceptance, the contractor shall supply the following information accompanied by a certificate which attests that the information provided is correct and applicable to the product being submitted: a.
22、 A statement that the lot complies with all of the quality assurance provisions specified within this specification. b. c. Results obtained, by defect code, for all inspections performed. d. Drawing, specification number and date, together with an identification and date of changes. e. Certificates
23、of conformance on all material purchased by the contractor when such material is controlled by Government or commercial specifications referenced in any of the contractual documents. The certificate shall be signed by a responsible agent of the certifying organization. The initial certificate submit
24、ted shall be substantiated by evidence of the agents authority to bind his principal. Substantiation of the agent s authority will not be required with subsequent certificates unless, during the course of the contract, this authority is vested in another agent of the certifying organization. 4.1.2 G
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