NAVY MIL-A-81370-1970 ASSEMBLY CENTER STATION 65A132F6《65A132F6中间座位装配》.pdf

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1、i- / / - - .- A- MILITARY SPECIFICATION - .*y . -. -_- - -_ -_ - MIL-A-81370(AS) 4 June 1970 . . ASSEMBLY, CENTER STATION 65A132F6 This specification has been approved by the Naval Air Systems Command, Department of the Navy. 1, SCOPE 1.1 Scope - The equipment covered by this specification shall be

2、capable of providing release signals to the center weapon station. 1.2 Classification - Center station assembly 65A132F6 shall consist of the item listed in 6.9. 2. APPLICABLE DOCUMENTS 2.1 General - The documents listed in 6.11 of the issue in effect on the date of invitation for bids form a part o

3、f this specification to the extent specified herein. 3. REQUIREMENTS _ - 3.1 Preproduction - This specification makes provision for preproduction testing. 3.2 Parts and Materials - in the selection of parts and materials, fulfullment of major design objectives shall be the priFe consideration. in so

4、 doing the following shall govern: 1 (1) Microelectronic items shall conform to requirements specified herein. (2) Wer parts and materials requirements shall conform to Specifica- tion MIL-E-5400. +- Y (3) Nonrepairable subassemblies, as outlined in Specification MIL-E- . 5400, shall be used when pr

5、acticable. The general size of the .subassembly and the amount of circuitry to be included therein shall be approved by the procuring activity. Nonrepairable subassTmblies must be reliable (See 6.4) , *. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-

6、,-(4) When previously produced models of this equipment did not use nonrepairable subassemblies, the design shall not be changed to . employ nonrepairable assemblies without the approval of the pro- curing activity. 3.2.1 Nonstandard Parts and Materials Approval - Approval for the use of jnonstanard

7、 parts and materials (including transistors and diodes) shall be obtained as out- lined in Specification MIL-E-5400. 3.2.2 Microelectronic Modular Assemblies - When used , microelectronic modular assemblies shall be described by a contractor procurement specification and must be approved by the proc

8、uring agency . Microelectronic modular assemblies (microelectronic circuits) (MICS) shall be contained within maintenance modules (for example, on printed circuit cards). The choice of microelectronic modular assemblies shall be based on at least two sources of supply, which can be used interchangea

9、bly. 3,2.3 Modules, Maintenance - The electronic portions of the equipment shall be divided into maintenance modules (see Specification MIL-S-23603). Maintenance modules aha normally be considered repairable. 3.2.4 Microelectronic Interchangeability - Microelectronic circuits (MICS) shall be interch

10、angeable at the MC level, or at the maintenance module level when approved by the procuring activity (see 6.13). 3.3 Design and Construction - The equipment shall conform with all the applicable requirements of Specification MIL-E-5400 for design, construction and workman- ship, except as otherwise

11、specified herein. 3.3.1 Total Weight - The total weight of the equipment, excluding cables, shall be a minimum consistent with good design and shall not exceed 3.6 ounces. 3.3.2 Reliability - 3.3.2.1 Operational Stabia - The equipment shall operat? with satisfactory performance, contiimoiisly or iii

12、tcrniittcntly for :I pc?riod o at icast 1,000 hours without the necessity for readjustment of any controls which are iniicccssibleto the operator during norm or (2) Switches S3, 54 and S5 are open. in the absence of such conditions, the output at terminal 5 shall remain at the logic 1 level. . . , -

13、 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-J MIL-A-82370 22 m 7777706 0357230 8 m - -_ -. . . . . . - -_ - - - . _._-I-. . . . . - - -. _ -_ MIL-A-8 13 70 (AS) 6.10.7.2 6,lO 7.3 Center Station Select (Refer to figure 1) (I) Switch S9 ttON1l. (2

14、) Switch 52 “ON“. (3) Pin B should read llOtl. (4) Switch S7 lON1t. (5) Pin B should read 2 2.0 volts or Center Station Priority (Refer to figure I) (1) Switch S9 ltON1l. 5.0 volts. . (2) Pin B should read ifoft. (3) Switch 57 ltON1t. (4) Pin B should read 2 2.0 volts or S 5.0 volts. (5) Switch S5 I

15、10Ntt. (6) Pin B should read ttO1l. (7) Switch S5 and 54 ltON1t. (8) Pin B should read (9) Switch 54 “OFFfr and S3 ltONfT. (10) Pin 3 should read 10tt. 6-10.7.4 Center Station Output (Refer to figure 1) (1) Pin 5 should read 26V. (2) Switch S9 llON1t. (3) Pin 5 should read 26V. (4) Switch 57 llON1l.

16、 (5) Pin 5 should read 26V. (6) Switch S1 tlON1l. (7) Pin 5 should read ltOtt. (8) Switch S1 ItOFF1I. - -.- (9) Pin 5 should read 26V. - _- - 6.10 . 7.5 Cepter Station Stores (Refer to figure 11 6.10.7.5.1 Switch Transfer (1) Switch S8 “ONvt. -_ Provided by IHSNot for ResaleNo reproduction or networ

17、king permitted without license from IHS-,-,- - - _ MIL-A-8 1370 (AS) Switch Si Reset Pin B should read 2 2. O volts or L 5. O volts. Switch S8 llOFFfl. Pin B should read W Switch S6 ltON1l. Reset Pin B should read b 2. O volts or S 5. O volts. Switch S6 tlOFF1l. Pin B should read “0 26V. (8) Pin B s

18、hould read 1011 and pin 5 should read 26V. (9) Switch S1 OFFf1. (10) Pin B should read “0“ and pin 5 should read 26V. 6.10.7.5.3 Count 2-6 Transfer Switch S8 “ONt1. Switch 57 ltON1f. Reset Pin B should read B 2.0 volts or S 5.0 volts, and pin 5 should read 26V. Switch S1 )IONf1. Pin B should read 5

19、2.0 volts or S 5.0 volts and pin 5 should read llO1l. Switch S1 “OFFt1. . * - 13 .v- Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-9_- MIL-A-81370 12 9797906 0359243 b -.“(.a- Pin B should read a 2, O volts or s 5 O volts, and pin 5 should read 26V

20、. Repeat steps (5), (6), (7) and (8) four more times. Switch S1 Pin B should read read Wtl. Switch S1 “OFF“. Pin 33 should read Switch S1 “ON“. Pin B should read Switch S1 vtOFF. Pin B should read 6,-10,7,5.1 lCount Two“ Transfer Switch S8 “ON“. Switch 57 26V. “0“ and pin 5 should read 26V. 11011 an

21、d pin 5 should read 26V. B 2. O volts or S 5. O volts and pin 5 should Pin B should read 2 2. O volts or $5 5. O volts and pin 5 should read (0“. Switch S1 “OFFff. Pin B should read h 2.0 volts or s 5.0 volts and pin 5 should read 26V. Switch S1 “ON“. Pin B should read 2 2. O volts or 5 5.0 volts, a

22、nd pin 5 should read llOfl. Switch SS “OFF“. Pin B should read B 2.0 volts or 5 5.0 volts, and pin 5 should read Switch S1 “OFF“. Pin B should read lfO1l and pin 5 should read 26V. Switch S1 “ON“. Pin B should read and pin 5 should read 26V. . Provided by IHSNot for ResaleNo reproduction or networki

23、ng permitted without license from IHS-,-,-MIL-A-8 1370 (AS) (17) Switch S1 “OFFtf. (18) PinB should read “0“ and pin 5 should read 26V. 6.10: 7.5.5 Count Seven or More Transfer (1) Gwitch S6 itONtl. (2) Switch 57 ttON1l. (3) Reset (4) PUZ B should read 2 2.0 volts or s 5.0 volts, arid pin 5 should r

24、ead 26V. (5) Switch S1 llON1l. (6) Pin B should read 2 2.0 volts or s 5.0 volts, and pin 5 should read tlt. (7) Switch S1 “OFF!. (8) Pin B should read 2 2.0 volts or S 5.0 volts, and pin 5 should read 26V. (9) Repeat steps (5), (6), (7), and (8) six more times. (10) Switch S1 “ON“. (11) Pin B should

25、 read 2 2.0 volts of 85.0 volts, and pin 5 should. read ri. -I (12) Switch S6 “OFF“. (13) Pin B should read L 2.0 volts or S 5.0 volts, and pin 5 should read Y) I. (14) Switch S1 WFFfl. (15) Pin B should read “O“ and pin 5 should read 26V. 6.11 Applicable Documents - SPECIFICATIONS Military MIL- E-5

26、400 Electronic Equipment, Aircraft, General Specification for MIL- T- 542 2 Testing, Environmental, Aircraft Electronic Equipment Interference Control Requirements, Aircraft Equipment . MIL-1-6 18 1 o Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-

27、- - MIL-A-81370 (AS) Military - 6.11.1 MIL-E- 17555 MIL-T- 18303 MIL- N- 18307 MIL-S-23603 Electronic and Electrical Equipment and Associated Repair Parts, Preparation for Delivery of Test Procedures; Preproduction and Inspection, for Aircraft Electronic Equipment, Format for Nomenclature and Namepl

28、ates for. Aeronautical Electronic and Associated Equipment System Readiness/ Maintainability ; Avionic Systems Design, General Specificat ion for . STANDARDS Military MIL-STD- 704 Electric Power, Aircraft Characteristics and Utilization of MIL-STD- 78 1 Reliability Tests Exponential Distribution PUB

29、LICATION Naval Air Systems Command MIL-P-8 1361(AS) Programmer, Aircraft Weapons Release Set MX-7016(*)/AWE-l Availability of Documents - (1) When requested specifications, standards, drawings, and publica- tions refer to both title and number. Copies of this specification and applicable specificati

30、ons required by contractors in connection with specific procurement unctions may be obtained upon applica- tion to the Commanding Officer, Naval Supply Depot, Code 105, 5801 Tabor Avenue, Philadelphia, Pennsylvania 19120. 6.12 Criteria for Multiple Source - The criteria of this paragraph shall be us

31、ed or determining the extent to which the requirement for multiple independent source c. availability of microcircuits is satisfied. For intecliangeability at the MIC level, multiple 8ource availability exists if the devices from the different sources may be used inter- ,+changeably, device by devic

32、e, in the final equi ineiit without any need for mechanical or -% /B,. . - . - - - . o Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,- - - - MIL-A-81370 12 W 9999906 35924b L W _. - - .?.- II _- MIL-A-8 1370 (AS) electrical changes. For interchangea

33、bility at the card level, multiple source availability exists if a card composed of MICS from one source is mechanically and electrically inter- changeable with another card composed of MICS from another source. Numerous aspects need be considered to arrive at the independence of sources; these invo

34、lve production inde- pendence, corporate (or firm) and financial independence, and geographical separation. The production independence of one Bource of another is determined by the extent to which the one source is independent of the other for manufacture; and by the lack of common original supplie

35、rs of raw or processed materials. Design, process information, technol- ogy, and iffusion masks may be derived from a common source. However, in such a case, each device source shail have a demonstrated capability of originating these items. The corporate (or firm) and financial independence of one

36、source of another is determined by Re absence of common directors, common officers, or holders of large common financial interests. Geographical separation is simply the distance between the locations where prin- cipal manufacture takes place by two sources. 6.13 Microelectronic interchangeability D

37、emonstration - interchangeability of microelectronic elements shall be demonstrated as follows: (3) For the interchangeability at the MIC level, it shali be demonstrated for each type of functional MIC from one source, as used in the system, that it is mechanically and electrically interchangeable w

38、ith that from another source (see 6.12). For the interchangeability at the maintenance module level, it shall be demonstrated that modules typical of those to be used in the sys- tem composed of MICS from one source are mechanically and elec- trically interchangeable with modules composed of MICS fr

39、om another source. For the completed equipment, it shall be demonstrated that modules composed of MICS from one source are interchangeable with cor- responding modules cornposed of MICS from another source. When interchange has been effected, no degradation shall take place in system and subsystem p

40、erformance. . . Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-. - - .- _ MIL-A-8137 O (AS) I N U m. n Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-.- - A- - MIL-A-81370 (AS) .I25 2.w MCL 2 HOLES

41、.o67 t.w 4 WLES 1 1 n 1 . . 8 Figure 2. Outline Dimensions 23 2.1 - Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-A-81370 (AS) I I- 1-$ S9 A Hi5 +28V O GROUND0 . Figure 3. Diode Leakage Test 24 . 3 A- I9527 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-