ARMY MIL-F-63434 A-1982 FUZE PROBE ASSEMBLY SPRING ASSEMBLING AND PACKING (TOW)《引信探针组装 弹簧组装和包装(陶式武器)》.pdf

上传人:proposalcash356 文档编号:444839 上传时间:2018-11-16 格式:PDF 页数:84 大小:1.72MB
下载 相关 举报
ARMY MIL-F-63434 A-1982 FUZE PROBE ASSEMBLY SPRING ASSEMBLING AND PACKING (TOW)《引信探针组装 弹簧组装和包装(陶式武器)》.pdf_第1页
第1页 / 共84页
ARMY MIL-F-63434 A-1982 FUZE PROBE ASSEMBLY SPRING ASSEMBLING AND PACKING (TOW)《引信探针组装 弹簧组装和包装(陶式武器)》.pdf_第2页
第2页 / 共84页
ARMY MIL-F-63434 A-1982 FUZE PROBE ASSEMBLY SPRING ASSEMBLING AND PACKING (TOW)《引信探针组装 弹簧组装和包装(陶式武器)》.pdf_第3页
第3页 / 共84页
ARMY MIL-F-63434 A-1982 FUZE PROBE ASSEMBLY SPRING ASSEMBLING AND PACKING (TOW)《引信探针组装 弹簧组装和包装(陶式武器)》.pdf_第4页
第4页 / 共84页
ARMY MIL-F-63434 A-1982 FUZE PROBE ASSEMBLY SPRING ASSEMBLING AND PACKING (TOW)《引信探针组装 弹簧组装和包装(陶式武器)》.pdf_第5页
第5页 / 共84页
亲,该文档总共84页,到这儿已超出免费预览范围,如果喜欢就下载吧!
资源描述

1、L 1 ML-F-63LI3YA 13 U 777770b 0350353 = MIL-F-63434A (AR) 30 AUGUST 1982 SUPERSEDING MIL-F-63434 (AR) 13 May 1981 MILITARY SPECIFICATION FUZE PROBE ASSEMBLY, SPRING, ASSEMBLING AND PACKING (TOW) This specification is approved for use by the U.S. Army Armament Research and Development Command and is

2、available for use by all Departments and Agencies of the Department of Defense. 1. SCOPE 1.1 This specification contains requirements not covered by the drawings and provides quality assurance provisions for fabrication of parts, assembly and packing of one type of fuze probe for use in the Improved

3、 TOW Missile. 2 APPLICABLE DOCUMENTS 2.1 Issues of Documents. The following documents 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. S PE C I FI CATIONS MILITARY MIL-A-48078 STANDARDS MILITARY MIL-STD-

4、105 Ammunition, Standard Quality Assurance Provisions for SampLing Procedure and Tables for Inspection by Attributes /- -. THIS DOCUMENT CONTAINS ng warhead standoff. tip cha;. A crush switch shall be provided at the forward The Probe shall be mechanically locked in the stowed position prior -ne pro

5、be and at .the ogive immediately forward of the explosive . to hunch and in the extended position after deployment. extending mechanism shall be self contained and shall be rider assembly at missile launch. 3.4 Missile Flight Vibration. The Fuze Probe shall Missile Flight Vibration Test. The Fuze Pr

6、obe actuated by a bore be subjected to the 3.5 Missile Launch Shock. The Fuze Probe shall be subjected to the Missile Launch Shock Test. 3.6 Transportation Vibration. The Fuze Probe shall be subjected to the Transportation Vibration Test 3.7 Electrical Resistance. * 3.7.1 Electrical resistance of bl

7、ack wire to outer ogive base shall no-t exceed 0.5 Ohm. * 3.7.2 Electrical resistance of black wire to outer probe tip shall not exceed 0.5 Ohm. 2 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-HIL-F-63q3qA 13 9779906 0350353 1 MIL -F-6 34 34A (AR)

8、* 3.7.3 Electrical resistance of brown wire to inner probe tip shall not exceed 0.5 Ohm. * 3.7.4 Electrical resistance of brown wire to inner ogive shall not exceed 0.5 Ohm. Electrical resistance between the brown and black wires shall be 100 megohms minimum at 100 2 5 Vdc. 3.8 Electrical Capacitanc

9、e. The capacitance as measured between the brown and black wires of the Fuze Probe shall be 75 Picofarads (Pf) + 15 Pf. - 3.9 Hot Deployment. The Probe Assembly shall be tested for hot deplayment. not exceed 0.100 seconds and the forward tip of the extended probe with a 4.25 plus or minus a .25 poun

10、d load applied axially to the tube sections shall be 14.14 inches minimum from the assembly base. The bore rider shall return to the retracted position after deployment. The time from bore rider release to probe fully extended shall 3.10 Cold Deployment. The Probe Assembly shall be tested for cold d

11、eployment. The time from bore rider release to probe fully extended and locked shall not exceed 0.100 seconds and the forward tip of the extended probe with a 4.25 plus or minus .25 pound load applied axially to the tube sections shall be 14.14 inches minimum from the assembly base. shall return to

12、the retracted position after deployment. change, when the load direction is reversed, shall not exceed one degree total. The bore rider The probe angle 3.11 Ambient Deployment. The Probe Assembly shall be tested for ambient deployment. The time from bore rider release to probe fully extended and loc

13、ked shall not exceed 0.100 seconds and the forward tip of the fully extended probe with a 4.25 plus or minus .25 pound load applied axially to the tube sections shall be 14.14 inches minimum from the assembly base. rider shall return tq the retracted position after deployment. The bore 3.12 Angular

14、Alignment. The angle formed between a point tangent to the probe at 1.5 probe diameters aft of the probe tip and the warhead centerline shall not exceed 1 degree total included angle when loaded to 18 pounds. 3.13 First Article Inspection. This specification makes provision for First Article Inspect

15、ion. Requirements for the submission of First Article samples by the contractor shall be as specifed in the contract. 3 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,- MIL-F-b3Ll34A 13 m 9799906 035035Ll 3 MIL- F-63434A (AR) 3.14 Workmanship. The TO

16、W, Fuze Probe Assembly and its components shall be fabricated and finished in a thorough, workmanlike manner. It shall be free of burrs, chips, sharp edges, unblended radii, cracks, surface defects, dirt, grease, rust, corrosion products and other foreign matter. methods used shall not be injurious

17、to any part, nor shall parts be contaminated by the cleaning agents. continuous except for a few light scratches. neat and sharply de fined . The cleaning Exterior surface coatings shall be All required markings shall be 3.15 Weight. The weight of the complete probe assembly shall not exceed 1.53 po

18、unds. 4. QUALITY ASSURANCE PROVISIONS 4.1 Responsibility for inspections f - HIL-F-63434A 13 m 7779706 0350360 7 m rl d m m 1 1 In In .rl .rl 3 3 O O d d 10 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-NIL-F-63LI3LIA 33 m 7979706 0350363 O m P E 3

19、1 rl rlrl rl (Dm (D 1 v) 11 -4 .FI ?FI 33 3 v)v) O0 O . rlrl rl -0 al 0 .FI ici al n rec O -a O % al - o e al a 11 n Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-h rl LI 0 al m 2 P % ti *rl U cn LI al I4 N b. MIL-F-6343LiA 13 7999906 0350362 2 O0

20、O dd d I a .rl ici al U al 2 E c, U ao c1 8% Nd B cc .rl e3 .rl .rl .rl mm 00 mumu cc cucu .rl .rl .rl .rl a3 a3 agmg a *I4 m z i3 O 3 LI O O a ici O al al a .rl 3 w c 4 G u W w H 91 d O N I 12 F z 3 rl Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,

21、-8 rl E B MIL-F-63434A 13 m 7799906 O350363 4 m rl O0 O Ar4 rl C 3 9 ria u 3ci 13 p Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-_ MIL-F-63434A 13 7797706 0350364 6 a O O d r( VI al d .iI WO OW i 14 Provided by IHSNot for ResaleNo reproduction or

22、networking permitted without license from IHS-,-,- - MIL-F-63434A 13 7779706 0350365 8 9 ON rl4 O rl 38 a *rl 5 -E 8 a LI O O a W O al u c al -u .rl ? w 15 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-_ MIL-F-63434A 13 799990b 03.50366 T O rl 99 r

23、lrl U d W al -u al 2; 2 k al a O k d ? a .d c v 2 E c !2 a W O al u c al U .rl 3 w I Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,- z E 4 u MIL-F-63434A I3 7777906 O350367 I W h d .n al v) ul m c o U .FI a 8 3 fi i$ I; O O00 d ;A U ius - ll-l hvIh

24、m $ ll-l O k al u al m .FI a n 23 P Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-a a u CI al k al n 3 B l% + n a MIL-F-b3434A 13 m 99999Ob 0350374 9 m O00 O000 . ddd $A 5 al El .A vi al Fi dd 4 4 dl 24 Provided by IHSNot for ResaleNo reproduction

25、or networking permitted without license from IHS-,-,-MIL-F-63434A 13 m 7777906 0350375 O m a ra I 3 .rl al CI al z g al U a 1 e al CI *rl 2 E .,a - a u 25 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-d t5 t d I X m c, i .rl 1 MIL-F-63434A 13 m 777

26、7906 O350376 2 m O d O000 GGGA al d 8 k m d Cu O td al u a rl I n al U o al a .rl i% 2 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-rl 8 d MIL-F-63434A 13 E 7779706 0350377 Li E .rl FI .rl m U 2 ti n I.( o CA O t-l O000 ; o) N .rl m a Q, 2 FI 27 P

27、rovided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-F-b3g3gA 13 9 7779706 0350378 b O00 rlrlrl . O00 4GA al rl O s GO a E .A Yi al 2; ct oi U e oi U .rl 3 2 30 i Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-

展开阅读全文
相关资源
猜你喜欢
  • BS PD CEN TR 15149-3-2014 Solid biofuels Determination of particle size distribution Rotary screen method《固体生物燃料 粒度分布的测定 回转筛选法》.pdf BS PD CEN TR 15149-3-2014 Solid biofuels Determination of particle size distribution Rotary screen method《固体生物燃料 粒度分布的测定 回转筛选法》.pdf
  • BS PD CEN TR 15160-2005 Petroleum and related products - Applicability of diesel fuel test methods for Fatty Acid Methyl Esters (FAME) - Information and results non round .pdf BS PD CEN TR 15160-2005 Petroleum and related products - Applicability of diesel fuel test methods for Fatty Acid Methyl Esters (FAME) - Information and results non round .pdf
  • BS PD CEN TR 15177-2006 Testing the freeze-thaw resistance of concrete — Internal structural damage《混凝土抗冻融性能试验 内部结构损坏》.pdf BS PD CEN TR 15177-2006 Testing the freeze-thaw resistance of concrete — Internal structural damage《混凝土抗冻融性能试验 内部结构损坏》.pdf
  • BS PD CEN TR 15193-2-2017 Energy performance of buildings Energy requirements for lighting Explanation and justification of EN 15193-1 Module M9《建筑物能源性能 照明的能源需求 EN 15193-1.pdf BS PD CEN TR 15193-2-2017 Energy performance of buildings Energy requirements for lighting Explanation and justification of EN 15193-1 Module M9《建筑物能源性能 照明的能源需求 EN 15193-1.pdf
  • BS PD CEN TR 15232-2-2016 Energy performance of buildings Accompanying TR prEN 15232-1 2015 Modules M10-4 5 6 7 8 9 10《建筑的能源性能 引用TR prEN 15232-1-2015 M10-4 5 6 7 8 9 10模块》.pdf BS PD CEN TR 15232-2-2016 Energy performance of buildings Accompanying TR prEN 15232-1 2015 Modules M10-4 5 6 7 8 9 10《建筑的能源性能 引用TR prEN 15232-1-2015 M10-4 5 6 7 8 9 10模块》.pdf
  • BS PD CEN TR 15276-1-2009 Fixed firefighting nsystems — Condensed naerosol extinguishing nsystems nPart 1 Requirements and test methods nfor components《固定的消防系统 浓缩气溶胶灭火系统 .pdf BS PD CEN TR 15276-1-2009 Fixed firefighting nsystems — Condensed naerosol extinguishing nsystems nPart 1 Requirements and test methods nfor components《固定的消防系统 浓缩气溶胶灭火系统 .pdf
  • BS PD CEN TR 15276-2-2009 Fixed firefighting nsystems — Condensed naerosol extinguishing nsystems nPart 2 Design installation and nmaintenance《固定式消防系统 浓缩气溶胶灭火系统 第2部分 设计、安.pdf BS PD CEN TR 15276-2-2009 Fixed firefighting nsystems — Condensed naerosol extinguishing nsystems nPart 2 Design installation and nmaintenance《固定式消防系统 浓缩气溶胶灭火系统 第2部分 设计、安.pdf
  • BS PD CEN TR 15278-2006 Workplace exposure - Strategy for the evaluation of dermal exposure《作业场所暴露 经皮暴露的评估策略》.pdf BS PD CEN TR 15278-2006 Workplace exposure - Strategy for the evaluation of dermal exposure《作业场所暴露 经皮暴露的评估策略》.pdf
  • BS PD CEN TR 15281-2006 Guidance on Inerting for the Prevention of Explosions《爆炸预防用惰化导则》.pdf BS PD CEN TR 15281-2006 Guidance on Inerting for the Prevention of Explosions《爆炸预防用惰化导则》.pdf
  • 相关搜索

    当前位置:首页 > 标准规范 > 国际标准 > ARMY

    copyright@ 2008-2019 麦多课文库(www.mydoc123.com)网站版权所有
    备案/许可证编号:苏ICP备17064731号-1