ARMY MIL-F-50994-1972 FUZE ROCKET M423 MODIFIED (BUNKER) LESS BOOSTER AND LEAD《M423改装(燃料)少助推器和导线火箭弹引信》.pdf

《ARMY MIL-F-50994-1972 FUZE ROCKET M423 MODIFIED (BUNKER) LESS BOOSTER AND LEAD《M423改装(燃料)少助推器和导线火箭弹引信》.pdf》由会员分享，可在线阅读，更多相关《ARMY MIL-F-50994-1972 FUZE ROCKET M423 MODIFIED (BUNKER) LESS BOOSTER AND LEAD《M423改装(燃料)少助推器和导线火箭弹引信》.pdf（40页珍藏版）》请在麦多课文档分享上搜索。

1、MTLZTARY SPECIFICATION FUZE, DCKET, M423, WDIFTED (BUNKER) IESS BCX)STER AND LEAD 1. SCOPE 1.1 This specification covers the quality assurance pra- Visions and special requirements not covered by the parts and assenbly drawin of a point detonating me, modified for bun- ker penetration, designated as

2、 Fuze, Fbcket, m23, bbdifled (Bmker) Less Booster and Booster Lead (see 6.7). 2. APPLICBrn Ix)cuMENTs 2.1 ?he follbwing docunients of the issue in effect .on date of invitation for bids or request for proposals form a part of this specification to the extent specified herein. SPECIFICATIONS MILITARY

3、 _- MLA-8625 - Anodic Coatinpg for Aluminum and Aluminum MILD-18665 - Detonator, Mark 59 Alloys PURQIPSE iE3ClUFTIoN AEZ-93 - Primr, ML04 (XI94Ei) Parts for and Mading, AssenKihg and Packing STANDARD3 MILITARY MIGSTD-105 - Sanpling Procedures and T Functional Test - Aircraft Vibratrion, Method 514,

4、Curve Z, as specified in MIL-STD-810. The vibration conditioninq shall be continuously performed until completed. After completion of the Five Foot Drop Test and the Functional Test, including the acceptance criteria for these tests (leak test, non-arming test, and arming time test), the same fuzes

5、shall be tested for hiqh order functioning, 3.4.6 Seal leakage test,-The leakage in the fuze shall not cause a pressure drop greater than 0,00072 psi in 10 sec, 3,4,7 Fuze Firing 3.4.7.1 Point Detonating Elode,-The fuze assembly shall function the explocive elements when a weight is dropped onto the

6、 nose of the luze, 3,4,7,2. Bunker Moda,-The fuze assembly in the bunker mode shall function the explosive elements when the fuze is dropped nose-down onto a steel plate, 3.5 Workmanshi ,-AU parts and assemblies shall be free from burrs, chips, _fi_p s arp edges, cracks, unblendad radii, surface de-

7、 fects, dirt, grease, rust, porosity, warpage, burn marks, checks, blisters, excess flash, corrosion products and other foreign matter. The cleaning method used shall not be injurious to any part nor shall the parts be contaminated by the cleaning agents, Surface coating shall be continuous except f

8、or a few slight scratches not exposing base material, The loading and assembly operatlons shall be performed in a thorough workmanlike manner consistent with the best practices of the industry. All required marking shall be neat and sharply defined. 4 Provided by IHSNot for ResaleNo reproduction or

9、networking permitted without license from IHS-,-,-MIL-F-50774 13 977770b 0333284 O MIL-F-50994 (MU) 3.6 First article inspection.-This specification makes provisions for first article inspection, Requirerent for the sub- mission of first article samples by the contractor shall be as specified in the

10、 contract. 4. QUALITY ASSURANCE PROVISIONS 4.1 Responsibility for inspection.-Unless otherwise speci- fied in the contract or purchase order, the supplier is responsible for the performance of all inspection requirerents as specified herein. Except as otherwise specified in the contract or order, th

11、e supplier may use his own or any other facilities suitable for the performance of the inspection requirements specified herein, unless disapproved by the Government. The Government reserves the right to perforri?. any of the inspections set forth in the speci- fication where such inspections are de

12、emed necessary to assur2 supplies and services conform to prescribed requirements. 4.1.1 Submission of product,-At the time each completed lot o iterrs deliverable under the contract is submitted to the Govsrn- ment for acceptance, the contractor shall supply the following information accompanied by

13、 a certificate which attests that the inforration provided is correct and applicable to the product being submitted : a. A statement that the lot complies with all of the quality assurance provisions specified in this specification. b, Drawing and specification number and date, together with identif

14、ication and date of changes thereto. c, A statemnt that all material purchased by the con- tractor mets requirements, when such material is controlled by Governmnt or commercial specifications referenced in any of the contractual documents, and that certificates of conformance are on fila and availa

15、ble for review, The certificate shall be signed by a responsible agent of the cer- tifying organization. The initial certificate submitted shall be substantiated by evidence of the agents authority to bind his prin- cipal, Substantiation of the agents authority will not be required with subsequent c

16、ertificates unless, during the course of the con- tract, this authority is vested in another agent of the certifying organization. d. Number of items in the lot, e, Date submitted, 4.1,2 Contractor inspection system.-As part of the contrac- torts approved quality procedure, there shall be a provisio

17、n for checking tho adequacy of inspections mads in connection with listed critical or major defects. following provisions: These procedures shall include the Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-flIL-F-5077Y 13 m 777770b 0333285 2 m MIL-F-

18、50994 (MU) 4.1.2.1 Use of simulated defect stand.ards.-The following listed verified inspections shall be validated-and inspection equip- ment verified hourly using Design Agency approved item facsimilies or standards containing the defects and supplied by the contractor. The contractor shall resupp

19、ly the item facsimilies when it is deter- mined by the Government that the facsimilies are no longer represen- tative enough of the product to make it unidentifiable to the con- tractor inspection personnel, or it is not functioning in the neces- sary manner and cannot be corrected satisfactorily. T

20、hese standards should be representative of defects actually found or anticipated. They should be inert and readily identifiable to the Government to ensure recovery should they be inadvertently introduced into pro- duction. Simulated defect standards used to verify the following verified inspections

21、 should be constructed and identified in such a manner that they are not readily recognizable to the contractor inspection personnel as defect standards, so that their number, time, and sequence of introduction into the inspection cycle is known only to those personnel responsible for checking the a

22、ccuracy of. the operation. Adequacy o the standards shall be verified at feast once each shift, Standards should be used. Verified Inspections Paragraph 4 3,3 11 - Setback weight return capability Paragraph 4.3.3.15 - S2 Undetected defect standards. Provisions shall be established for the corrective

23、 action to be taken where the equip- ment or contractor inspection personned fail to identify a standard as defective, .These provisions shasll Include a reinspection of all acceptable material subsequent to the last acceptable verification check as a minimum, . 4.2 First Article Inspection 4.,2.1 C

24、ubmission,-The contractor shall submit a first article sample as designated by the contracting officer to a Government approved facility for evaluation Ln accordance with the provisions of 4,2.2. The first article sample shall have been produced by the contractor ox furnished by a supplier and which

25、 have been manufactured using the same production process, pro- Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-7 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL -F- 50994 (MU) i . 7. . _- .- 4-P

26、g ;f Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-S*,*,*c.*Gage Width of outside groove,Gage Depth of outside groove,.,.,.,Gage Finish of firing pin body CaVityllc.rc.4r,.,*,.,*,Gage Finish of outside diameter,.,.Gage AQL 0,65 percent Evidence of

27、poox workmanship (see 3,5), ,visua o4001 Q4002 04003 04004 04005 04006 04007 04008 04009 04010 04011 04012 04013 04014 04015 04016 04017 04018 04019 04020 04021 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-_ MIL-F-50774 13 7777906 0333274 3 MIL-F-

28、50994 (MU) 4,3,2,5 S ring, retaining (see dwg, 9269703 covering a detail of dwg,+68180) , Cate go ries Defects Critical : None defined, Method of Code No. Inspection Minor: AQL 065 percent 201, Evidence of poor workmanship (see 3.5).cc,.s,.,.Visual 05002 4.3.2.6 Sleeve, Pin, Firin3 (see dwg. 9269695

29、 covering a detail of wg. 92681 80) Categories Defects Critical : None defined, Method of Code No, Inspection Major: 101. 102, 103, 104 , 105. 106, 107, 108, 109 110 111, 112 , AQL 1,50 percent Outside diameter, max,.,Gage Inside diameter, min,.,.,Gage Diameter of small retaining spring slot.,4.,.,G

30、age Diameter of large retaining spring slot,.,.Gage Runout of inside diameter Co outside diameter,Gage Runout of small retaining spring slot diameter to outside diameter*,.,T,.,Gage Runout of large retaining spring slot diameter to outside diater,.,Gage Parallelism of edge of small retaining spring

31、slot to end of sleeve,.,C,.*.,*Gage Overall length, max.,.,.,.,Gage Length from unchamfered end of sleeve to small retaining spring slot,.,.(, . Gage Overall width of small and large retaining spring slots,. . ,Gage Width of large retaining spring slot.,c.,Gage -. 06001 06002 06003 06004 06005 06006

32、 06007 06008 06009 06010 06011 06012 15 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-I MIL-F-50994 13 M 9999906 0333296 7 M MIL-F-5 O 9 94 (MU) 4.3,2

33、,9 Support, Timer (see dwg. 9269697 covering a detail of dwg, 9268199. Cate gorie s Defects Critical: None defined, Method of Code No. inspection .Major: 101 102 10 3, 104 . 105 . 106. 107. 108, 109. 110 111, 112 * 113, i14 p 115 + 116 . 117, 118, 201, 202 203, 204, Minor: AQL 1-50 percent Outside d

34、iameter, max. . . . . . , . . . ,Gage Diameter of cushion groove, mh.Gage Width of cushion groove, min. . . . Gage Diameter of countersunk hole min., ., . . .Gage Diameter of center hole, . . . + . . . ,Gage Distance between holes,.,.,.Gage Radius of rotor cut out,.,.Gage Radius of roller lock cut o

35、ut, . ,Gage Radius of outer plate cut out. . ,Gage Depth of rotor cut out,.,.,.,Gage Depth o$ roller lock cut out.,Gage Depth of outer plate cut out,.Gage Width of rotor cut out,.,.,.,Gage Width of roller lock cut out,Gage Length from edge of timer to rotor cut out,.(,.,.,Gage Width of rotor housing

36、 arm slot.Gage Disrance from edge of timer to outer plate cut outz . . . , . . . . , .Gage Overall thickness,.,.,l.,Gage Depth of cushion groove.,.,.,Gage Distance from outer plate cut out to post recess,.,Gage Length of tab on post.,.,.Gage Evidence of poor workmanship (see 3.5) , , . . . , , ir ,

37、. . , . . . . . ,Visual AQL 1.50 percent 09001 09002 09003 09004 09005 09006 09007 09008 09009 09010 09011 09012 09013 09014 09015 09016 09017 09018 09019 09020 09021 09022 4,3,2,10 Timet Support Assembly (see dwg, 9268199 covering a detail of dwg, 9271602), Categories Defects Critical: None defined

38、, Method of Code No, Inspection 17 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-10001 10002 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-F-50774 13 W 7777706 0333278 O W MIL-F-50994 (MU) 103

39、. Location of stud hoies and rotor housing arm slot Gage 12003 1011. Chamfer at base missing V.kstial 12004 . Minor: AQL 0.65 percent 201. Evidence of poor workmanship . (see 3.5) Visua 12005 4.3.2.13 Rotor Housing Assembly (see dwg. 8883719 for a detail of dwg. 9271602). Cat egories Defets Method o

40、f Code No. Inspection Critical: None defined. Major: AQL 0.40 percent 101. Arm width (nearest studs), min. Gage 13001 102. Location of studs and nearest arm Gage 13002 . Minor: AQL 1.00 percent 201. Surface finish on arm in- 202. Evidence of poor workmanship correct (nearest studs) . Visual 13003 (s

41、ee 3.5) . Visual 13004 4.3.2.14 Device, Safety an Arminp; (see dwg. 9215619-1 covering a detail of dwg. 9271602). Categories Defects Method of Code No. Inspection Critical: 100 percent 1. -Distance between annular gear and No. 2 gear, max. Gage 14001 Maj or: AQL 0.40 percent 101. Alignment of detona

42、tor cavity with the outside diameter ac- ross the rotor housing posts Gage 14002 Minor: . AQL 0.65 percent 201. Evidence of poor workmanship (see 3.5) . Visua i4003 19 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-Provided by IHSNot for ResaleNo re

43、production or networking permitted without license from IHS-,-,-MIL-F-50994 13 = 9999906 U333300 5 = Major : 101, 102 103. 104 , 105 , 106 , 107, 108, 109, 110. 111 112. 113, 114 * 201, 202, 203, 24, 205 . 206 * Minor : MIL-F-50994 (MU) AQL 1.5 percent Total length.,.,.,Gage Location of counterbore

44、from bottom of booster cavity,*Gage Diameter of booster cavity,Gage Diameter of lead cavity,.,.Gage Depth of lead cavity,r,.,.,Gage Height of lead.,.,Gage Thickness at end of lead cavity,.l,.,.,.,.,rGage Width of O-ring groove,.,Gage Diameter of O-ring groove,Gage Concentricity of thread pitch diame

45、ter with booster cavityC.*,.L.*.,*,Gage Concentricity of lead cavity with booster cavity,.T.,cGage Major diameter of threads,Gage Concentricity of O-ring groove Mith pitch diameter. , ,Gage Finish of O-ring groove.,.,.Gage 16001 16002 16003 16004 16005 16006 16007 16008 16009 16010 16011 16012 16013

46、 16014 AQL 2,s percent Width across wrench slots,.Gage 16015 Symmetry of wrench slots,Gage 16016 Imide diameter at crimp section,.,.,l,*,c,Gage 16017 Wall thickness at crimp section, + . , , . . , . ,Gage 16018 Protective finish missing or incomplate,t,Visuai 16019 Evidence of poor workmanship (see

47、3.5)r.,rl.r.c.r.,visua1 16020 4,3,2,17 Body (see dwg. 9269691 covering a detail of dwg. 9268177) , Cate.gories Defects Method of Code No, Inspection Critical: None defined, Major: AQL 2,50 percent 101, 102, True position of striker pin hole with S detent spring - Code No. 23001 - set-back weight spr

48、ing - Code No, 24001 - firing pin spring - Code No, 25001 - nose cap spring - Code No. 26001.-A sample of 10 springs shall be selected from each heat treatment batch, The sample shall be tested as specified in 4.4.1 using equ2pment in accordance with 4.3.4, ment batch shall be rejected if one or more springs fail to comply with the specified requ%rement, Springs tested as specified shall be discarded as scrap, Code No, 27