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
《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》由会员分享,可在线阅读,更多相关《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(84页珍藏版)》请在麦多课文档分享上搜索。
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
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