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本文(NAVY MIL-T-81527 B-1971 TEST SET MISSILE CONTROL SYSTEM AWG-10 SIDE BENCH《AWG-10方凳导弹控制系统测试集》.pdf)为本站会员(花仙子)主动上传,麦多课文库仅提供信息存储空间,仅对用户上传内容的表现方式做保护处理,对上载内容本身不做任何修改或编辑。 若此文所含内容侵犯了您的版权或隐私,请立即通知麦多课文库(发送邮件至master@mydoc123.com或直接QQ联系客服),我们立即给予删除!

NAVY MIL-T-81527 B-1971 TEST SET MISSILE CONTROL SYSTEM AWG-10 SIDE BENCH《AWG-10方凳导弹控制系统测试集》.pdf

1、MIL- T - 8 15 Z7B (AS) i 29 January 1971 SUPERSEDING MIL- T-8 1527A(AS) . 4 December 1970 MILITAR Y SPECIFICATION TEST SET, MISSILE CONTROL SYSTEM, AWG-10 SIDE BENCH - This Specification has been approved by the Naval Air Systems Command, Department of the Navy 1. SCOPE a* 1.1 Scope. The equipment l

2、isted herein shall be an integrated assembly of Contractok-Furnished and Government -Furnished Equipment to facilitate detailed maintenance of AN/AWG-10 Missile Control System (MCS) at the Intermediate Level where a sidebench is available. AN/AWG-10 MCS Test Set, of and by itself, does not fulfill c

3、omplete main- tenance requirements for the Intermediate Level Maintenance of the AN/AWG-10 MCS. MIL-T-81517B(AS), Test Set, Missile Control System AN/AWM-21. i. 2 Classification. The AWG-10 Side Bench Missile Control System Test Set shall consist of the following items: FGrthermore, an I Facilities

4、having a centerline bench should refer to ITEMS TYPE DESIGNATION Table -Rack, Radar Maintenance FN-Z12E/AWG- 1 O Fixture, Antenna Maintenance MX-7340C/AWM-21 MX-8$91/ WG-10 OA-8124B P AWM-21 TK - 2 1 Coaxial, Dual Coaxial, Twin Con- ductor, and Twin Lead. MIL-P-642 - Plugs, Telephone. MIL-C-3767 - C

5、onnectors Electrical (Power Bladed Type) General 5 Specification for. $ 1 1 : MILT -5422 - Testing , Environmental, Aircraft Electronic Equipment . MIL-H-5606 - Hydraulic Fluid, Petroleum Base, Aircraft and Ordinance. MIL-1-6181 - Interference Control Requirements, Aircraft Equipment. MIL-H-15362 -

6、Harness; Test Bench, Avionic Equipment, General * j : 3 Specification for. a 6 : 9 9 i q i -4 MIL-W -16878. - Wire, Electrical, Insulated, High Temperature. MIL-M-17096 - Multimeter, AN/PSM-4. MIL-E -17555 - Electronic and Electrical Equipment and Associated d Repair Parts, Preparation for delivery

7、of. MIL-T-18303 = Test Procedures; Preproduction and AcceptancT40r e: ,I . . 1 I -. -5 i 1 2 d-7*, . - -, Aircraft Electronic Equipment, Format For. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-. MIL-T-L527B 12 W 7779706 0357909 9 m MIL-T-8 1527B(

8、AS) MIL-T-21200 - Test Equipment for Use with Electronic and Fire Control Systems, General Specification for. MIL-C-22750 - Covering Epoxy Polyamide MIL-S- 22885 - Switch; Push - But ton/Illuminat ed . MIL-T-23336 - Technical Directives (Letter Type): Preparation Of. MIL-C-24165 - Counter, Electroni

9、c, 500 Megacycle, AN/USM-207 MIL-S-52059 - Shelter, Electrical Equipment S- 141( )/G MIL-M-55088 - Multimeter, Electronic TS-505( )/U MIL-A-81030 - Air Transportable, Shelter Vans, For Dressing and briefing, Dental and Sick Bay, Aircraft Maintenance, Aerological. MIL-R-81114B - Radar Set AN/APG-59.

10、MIL-T-81516 MIL-T-81517 - Test Set, Missile Control System AN/AWM-21 MIL-C-81583 - Cabinet, Electronic Equipment MIL-T-81741 Test Set, Missile Control System AN/AWM-22 - Test Set, Missile Control Group OQ-5O/AWM-21, OQ-51 /AWM-21, and OQ-52/AWM-21 STANDARDS Mili tar y MIL-STD-167 - Mechanical Vibrat

11、ions of Shipboard Equipment. MIL-STD- I89 - Racks, Electrical Equipment, 19-inch and Associated Panels. MIL-STD -78 1 - Reliability Test , Exponential Dis tribution. MIL-STD-803 - Human Engineering Design Criteria for Aerospace Systems and Equipment. Federal FED-STD-595 - Colors DRAWINGS Military MS

12、-3100 - Connector Electrical MS-3102 - Connector, Receptacle , Electric, Box Mounting I r,- ._ *5 p- -*c. . MS-3126 - Connector, Plug, Electric MS-17322 - Meter, Time Totalizing .* MS-25307 - Switch, Toggle, Double Pole. o -_- - -_ Provided by IHSNot for ResaleNo reproduction or networking permitted

13、 without license from IHS-,-,-MIL-T-815278 12 I 7779906 0357405 h . MIL-T-81527B (AS) - MS-33656 - Fitting End, Standard Dimension for Flared Tube. NAMC 610415 - Shipboard Workbench for Aviation Electronics Shops 2.1.1 Availability of Documents - Copies of Specifications, Standards, drawings, and pu

14、blications required by suppliers in connection with specific procurement functions should be obtained from the procuring activity or as directed by the contracting office (see 6.4). 3, REQUIREMENTS 3.1 Parts and Materials - In the selection of parts and materials, ful- fillment of major design objec

15、tives shall be the prime consideration. doing the following shall govern: In so (a) Parts and Materials as approved by MIL-T-21200 shall be given fir s t cons id e r at io n. ) Guidelines for the selection of nonstandard parts shall be per MIL-T-21200, Selection of parts and materials. t (c) In the

16、selection of parts, the above considerations shall apply if the assembly is to be built for detail part maintenance. In the event the entire assembly is built to be expended, the assembly shall be constructed and the quality of the individual parts shall be such that the unit as a whole will pass el

17、ectrical and environmental test. 3.1.1 Nonstandard Parts - Nonstandard parts and materials shall be as outlined in MIL-T-21200 Materials, Parts and Processes, except that mechanical parts shall be considered as nonstandard parts only when the material requirements of MIL-T-21200, as modified herein,

18、 are not met. 3.1.2 Tube Types and Semiconductors Types - The choice and application of electron tubes and semiconductor types used in the equipment shall be in accordance with MIL-T-21200 and MIL-STD-70 1. 3.1.3 Noncarrosive Hardware - External, Military Standard (MS) hard- ware which is used durin

19、g servicing or installing test equipments shall be of a corrosive-resistance type and shall not be further finish-treated. 3* l-4 Paint - Paint shall be epoxy polyamide per MIL-C-22750; color shall , be aircraft gray, color number 16473, per FED-STD-. .r c. 4 Provided by IHSNot for ResaleNo reproduc

20、tion or networking permitted without license from IHS-,-,-. I 3.2 Design and Construction - Unless otherwise specified herein or in the detail equipment specification, Contract0 r -Furnished Equipment (C FE) shall conform with all the requirements of MIL-H-15362 or MIL-T-21200 as applicable for desi

21、gn, construction, and workmanship. Furnished Equipment (GFE) shall conform to the applicable detail equipment specification. System Test Set shall not exceed 5,000 pounds. 3-2.1 Operational Stability - Unless otherwise specified in the individual equipment specification, the equipment shall operate

22、with satisfactory per - formance, continuously or intermittently, for a period of 24 hours without necessity for readjustment of any operator controls which are inaccessible to the operator during use. Government - The total weight of the AWG-10 Side Bench Missile Control However, adjustments at poi

23、nts inaccessible to the operator during use may be made following replacement of parts. 3.2.2 Operating Life - The equipment shall have minimum total operating life of 2,000 hours with reasonable servicing and replacement of parts. 3.2.3 Cables and Connectors - The equipment shall provide for the us

24、e of cables and connectors in accordance with MIL-H-15362 and MIL-T-21200, as applicable. 3.2.4 Interchangeability - Unless otherwise specified herein or in the detail equipment specification, the equipment shall meet the inter changeabil- ity requirements as defined in MIL-T-21200. 3.2.5 Maintenanc

25、e Provisions and Field Testing - Provisions for main- tenance shall be as specified in MIL-T-21200. facilities shall be provided to the greatest extent practicable for ease of field testing and maintenance. be in accordance with MIL-STD-803. - Specific test points and test The color of front panel i

26、ndicator lights shall 3.2.6 Calibration - Test and Measuring equipment shall be calibrated at periodic intervals established on the basis of stability, purpose, and degree of usage. continued accuracy as evidenced by previous calibration results. Calibration intervals shall be adjusted as required t

27、o assure Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-T-L527B 12 I 7777706 0357Li07 T = c MIL-T-81527B (AS) - 3.2.7 Standard Conditions - The following conditions shall be used to establish normal performance characteristics under standard con

28、ditions and for making laboratory bench tests. Temperature Room Ambient: 25“ t 15; -5“ c 77“ t27,“-9“F Altitude Normal Ground Vib rat ion None Humidity Room Ambient up to 90 percent re lative humidity Input Voltage 115 I1 volts (V) line to neutral, 3-phase, 400 Hz 12 percent 27.5 IO. 5 volts direct

29、current (Vdc) 3.2.8 Warmup Time. Unless otherwise specified herein or in the detail equipment specification, the time required for the equipment to warmup prior to operations shall be kept to a minimum and shall not exceed 5 minutes under standard conditions, 20 minutes at extreme service condi- tio

30、ns. 3.2.9 Interference Control - The generation of radio interference by the equipment and the vulnerability of the equipment to radio interference shall be controlled within the limits of MIL-1-6181. 1 ! 3.3 Performance. 3.3.1 General. Unless otherwise specified, values set forth to estab- lish the

31、 requirements for satisfactory performance apply to performance under both standard and extreme service conditions. mance under the extreme conditions is acceptable, tolerances or values When reduced perfor- setting forth acceptable variations from the performance under the standard conditions will

32、be specified herein or in the detail equipment specification. 3.3.2 Function. Set shal pr Ovide The AWG-10 Side Bench Missile Control System Test an integrated maintenance facility. This shall include :.- .r 6 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from

33、IHS-,-,-_ MIL-T-81527B 12 9999906 0359408 I -. .- 1 MIL- T-8 1527B(AS) simulated aircraft controls and equipment test bench harnesses; equipment support and handling fixtures; test equipment both special and standard; special tools; cooling equipment; and a hydraulic power supply. 3.3.3 Form Factor.

34、 Test Set shall be designed for installation in a van as described in MIL-S-52059BV as well as ship and shore avionics shop layouts. Guidance Plan CVA61 Avionics Shop No. 1, Main Deck, FRS 29-39, Drawing 610415, Bench Space 119 through 126 shall be used as a guide to shop layout and bench design. 3.

35、4 Detail Requirements. 3.4.1 Table -Rack, Radar Maintenance. 3.4.1.1 Function. The Radar Maintenance Table-Rack shall be for shop use and shall provide monitoring, mounting, inter connection, hydraulic power and cooling facilities for the active Line Replaceable Units of the The AWG- 10 Side Bench M

36、is sile Control System MCS mounted on the bench. required aircraft flight functions and shall enable fault isolation, adjust- ment, and repair or replacement of defective pallets, circuits, plugin as- semblies, and components of the MCS. 3.4.1.2 Form Factor. requirements of Type II Shelters (Aircraf

37、t Maintenance) per MIL-A-81030 and shall require a space of 18-1/2 feet by 7-112 feet with 6-112 feet height. The operating and maintenance area will be 21-1/2 feet by 10 feet. weight of the equipment, including cables, shall not exceed 4, 200 pounds. The equipment shall electrically simulate MCS Th

38、e Table-Rack shall be compatible with the space The total . - 3.4.2.3 Mean Time Between Failures (MTBF). When maintained in accordance with applicable preventive maintenance procedures, the equip- ment shall demonstrate at least 400 hours MTBF. Accept-reject criteria shall be defined by paragraph 4.

39、2.8.1 of MIL-STD-781. i I j , 3.4.1.4 Service Conditions. The Equipment shall operate satisfactorily under any of the environmental service conditions or reasonable combina- % tion of these conditions of the Test and Control _.- - ._-_._ F be interlocked with the Hydraulic Panel of the Antenna Maint

40、enance Fixxre, when the Maintenance Fixture is utilized with the Table-Rack. The control shall be operable only when the Hydraulic Panel is in the BENCH position. (h) HYD OFF (Hydraulic Off) - The Hydraulics Off control shall be a red, momentary pushbutton switch which shall be used to turn off the.

41、 hydraulics while the MCS is on. . . . t! Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-T-815278 12 = 777770b 035992q T D 8 MIL- T -8 1527B( AS) PHAkE SELECTOR - The Phase Selector control shall be a 3-position rotary switch which shall select

42、the phase of the 3-phase, 400-Hz to be measured on the 400-Hz meter. Positions shall be marked A, B, and C, 3.4.1.6.3.3.2.4 Indication. The following monitors and indicating lights shall be provided on the front panel. (a) RADAR PHASE INDICATOR (400-Hz Phase Selector) - The Radar Phase Indicator sha

43、ll be a neon indicator light with a translucent white lens which shall show when the 3 -phase, 400 -Hz line voltage is connected in the proper phase sequence. (b) 400 CPS VOLTAGE (AC Voltage Monitor) - The AC Voltage Monitor shall be a voltmeter of 3 percent full scale accuracy which shall measure t

44、he MCS primary 400-Hz line voltage between 105 and 125V. (c) DC VOLTAGE (DC Voltage Monitor) - The DC Voltage Monitor shall be a voltmeter of 3 percent full scale accuracy which shall measure the primary dc line voltage between 22 and 31 Vdc. (d) ELAPSED TIME (Elapsed Time Indicator) - The Elapsed T

45、ime Indicator shall be a meter which conforms to MS 17322-6A. The meter shall indicate total “on time of the bench mounted radar. (e) LIQ FLOW (Liquid Flow Indicator) - The Liquid Flow Indicator shall be a red indicator light which shall show the state of the coolant flow interlock, When the flow th

46、rough the Liquid Cooling System is less than 2.5 + O. 1, -0.0 gallons per minute (gpm), the indicator light shall be lit. (f) HIGH TEMP (High Temperature Indicator) - The High Temperature Indicator shall be a red indicator light which shall show the state of the Temperature High interlock switch. Li

47、quid Cooling System rises above 107“ I3“C (225“ I5“F) the indicator light shall be lit. When the return temperature to the It i 5 (g) CMPTR AIR (Computer Air Indicqtor) - The Computer Air Indicator shall be a red indicator light which shall show the state of the Sensing Element installed in the plen

48、um ofthe Computer Support Structure -: . Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-and the state of the Sensing Element installed in the plenum of the Blower Assembly. water, in either plenum, the indicator light shall be lit. When the pressure

49、 is below nominal 5-1/2 inches of (h) MAG TRAP (Magnetic Trap Indicator) - The Magnetic Trap indi- cator shall be a red indicator light which shall show the state of the Mag- netic Trap filter of the Liquid Cooling System. When the trap accumulates sufficient magnetic particles, the indicator light shall be lit to indicate that trap cleaning is necessary. (i) LOW TEMP (Low Temperature Indicator) - The Low

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