NAVY MIL-C-85392-1987 CONTROL-MONITOR SET GUIDED WEAPON AN AWW-7D GENERAL SPECIFICATION FOR《AN AWW-7D型控制系统监控器设备总说明书》.pdf

《NAVY MIL-C-85392-1987 CONTROL-MONITOR SET GUIDED WEAPON AN AWW-7D GENERAL SPECIFICATION FOR《AN AWW-7D型控制系统监控器设备总说明书》.pdf》由会员分享，可在线阅读，更多相关《NAVY MIL-C-85392-1987 CONTROL-MONITOR SET GUIDED WEAPON AN AWW-7D GENERAL SPECIFICATION FOR《AN AWW-7D型控制系统监控器设备总说明书》.pdf（38页珍藏版）》请在麦多课文档分享上搜索。

1、I- - MIL-C-5372 10 E 7777706 0364714 O E 5- 37-67 MIL-C-85392(AS) 8 SEPTEKBEF. 1487 MILITARY SPECIFICATION CONTROL-MON ITOR SET, GUIDED WEAPON, AN/AWW-ID, GENERAL SPECIFICATION FOR This specification is approved for use within the Naval Air Systems Command, Department of the Navy and is available fo

2、r use by all Departments and Agencies of the Department of Defense. 1. SCOPE 1.1 Scope. This specification establishes the design, performance, and acceptance requirements for the Guided Weapon Control-Monitor Set AN/AWW-7D herein referred to as the a major component part of transmission of command

3、s control aircraft and a Wa e 2 APPLICABLE DOCUMENTS pod. the data 1 ink communication network, providing gnals and reception of video data, between a 1 eye guided weapon. The pod is- for airborne use and performs as 2.1 Government documents 2.1.1 Specifications an.d standards. The following specifi

4、cations and standards form a part of this specification to the extent specified herein. Unless otherwise specified, the issues of these documents shall be those listed in the issue of the Department of Defense Index of Specifications and Standards (DODISS) and supplement thereto, cited in the solici

5、tation. 1 1 Beneficial comments (recommendations, additions, deletions) ard any pertinent data which may be of use in improving this document shouid bc addressed to: Cornmarding Officer, Naval Air Engineering Center, Systems Engineering atxi Standardization Department (SESD) Code 93, lakehurst, NJ 0

6、8T33.5100, by usinq the setf.addressed Standardirat ion Document Improvement Proposal (DD Form 1426) appearing at the end of this document or by tetter. I I AMSC N/A FSC 1095 DISTRIBUTION STATEMENT A. Approved for pub1 ic release; distribution is 1 imited. THIS DOCUMENT CONTAINS 38 PAGES. Provided b

7、y IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-_ fi- 11 MIL-C-5392 LO rn 7979706 03611735 2 rn MI L-C-85392 (AS) SPEC1 FICATIONS MILITARY MIL-D-3464 MIL-W-5088 MIL-E-5400 MIL-T-5422 MIL-M-7793/6 MIL-A-8591 MIL-E-17555 MIL-N-18307 MIL-H-46855 MIL-T-81624 STAN

8、DA RD S MI L ITARY MIL-STD-129 MIL-STD-454 MI L-STD.-46 1 Desiccants, Activated, Bagged, Packaging Use and Static Dehumidi fi cat i on Wiring, Aircraft, Selection and Instal 1 ation of Electronic Equipment, Aerospace General Speci fi cat i on for Testing, Environmental, Airborne Electronic Equipment

9、 Meter, Time Totalizing Airborne Stores, Associated Suspension Lugs and Aircraft Stores Interface, General Design Specification for Electronic and Electrical Equipment, Accessories and Repair Parts; Packaging and Packing of Nomencl ature and Namepl ates for Aeronautical Electronic and Associated Equ

10、ipment Human Engineering Requirements for Military System Equipment and Facilities Television Display Requirements for the Weapon System for Guided Weapon Mark 1 Mod O and Mod 2 (Walleye) Marking for Shipment and Storage Standard General Requirements for Electronic Equipment Electromagnetic Emission

11、 and Susceptibility Requirements for the Control of Electromagnetic Interference 2 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-. - -a MIL-C-85392 LO 9999306 0364736 4 MIL -C -85392 (AS) MI L - STD - 4 6 2 MIL-STD-704 MIL-STD-781 MI L-STD-810 MIL-

12、STD-965 MIL-STD-1472 El ectromagnet i c Interference Characteristics, Measurement of Electric Power, Aircraft Characteristics and Uti1 ization of Re1 i abi 1 i ty Tests , Exponent i al Di stri but i on Environmental Test Methods and Engineering Gui del i nes Parts Control Program Human Engi neeri ng

13、 Des i gn Criteria for Military Systems Equipment and Facilities 2.1.2 Drawings. to the extent specified herein. be that in effect on the date of the solicitation. The following drawings form a part of this specification Unless otherwise specified, the issue shall DRAWINGS NAVAL AIR SYSTEMS COMMAND

14、DL 875AS1000 and all drawings therein Drawing List for Guided Weapon Control Monitor Set AN/AWW-7D (Copies of specifications, standards, and drawings required.by contractors in connection with specific acquisition functions should be obtained from the contracting activity or as directed by the contr

15、acting activity.) 2.2 Order of precedence. In the event of a conflict between the text of this specification and the references cited herein (except for associated detail specifications, specification sheets or MS standards), the text of this specification shall take precedence. Nothing in this spec

16、ification, however, shall supersede applicable laws and regulations unless a specific exemption has been obtained. 3. REQUIREMENTS 3.1 First article, When specified in the contract or purchase order, a sample shall be subjected to first article inspection (see 4.4 and 6.3). 3.2 Farts and materials,

17、3.2.1 General. Parts and materials used in the control-monitor sets shall conform to the requirements of the drawings and subsidiary specifications listed in the drawing list (DL) specified herein except, insofar as errors on the drawings may be incompatible with the requirements of this specificati

18、on and related specifications. Unless otherwise specified in the contract, proposed changes, either to correct drawing discrepancies or to effect improvements, shall be subject to the acceptance by the procuring activity. 3 Provided by IHSNot for ResaleNo reproduction or networking permitted without

19、 license from IHS-,-,-MIL-C-5372 LO W 9997706 03b4717 b mi Pa i MI L-C-85392 (AS) 3.2.1,l Nonstandard parts and material approval. Approval for the use of nonstandard parts and materials shall be obtained by the contractor as out1 ined in MIL-E-5400, and consistent with procedures cited in MIL-STD-9

20、65. 3,2.1.2 Basic conformance. pod shall be in accordance w 3.3 Design and construction tured in accordance with the in DL 875AS1000, except inso drawincis mav be incomDatible Parts and materials selected for use in the th MIL-E-5400, The control-monitor set shall be manufac- drawings and subsidiary

21、 specifications 1 isted ar as errors of omission or commission on the with the requirements of this specification. In any-case; it is a condition of final acceptance that the pods manufactured shall meet all the performance requirements of this specification and the appropriate test documents. Propo

22、sed changes, either to correct drawing discrepancies or to effect improvements, shall be acceptable to the procuring. activity prior to their incorporation. 3.3.1 Physical characteristics. 3.3.1.1 Description The pod shall consist of three major sections: The forward radome assembly., the aft radome

23、 assembly, and the casing (center bdy) assembly. All principle dimensions and locations of particular features, including center-of-gravity, shall be as shown on figure 1 and as specified in table I. 3,3.1.2 Total weight, Total weight of the pod shall be not greater than 645 pounds92 ki 1 ograms) .

24、3.3.1.3 Flight requirements. The Control-Monitor Set, Guided Weapon AN/AWW-7D shall be in accordance with DL 875AS1000 and shall be functionally cdmpatible and flight certifiable as an emergency jettisonable pod on the fol 1 owing aircraft: a. A-4 b. A-7A/B/E C. TA-7C d, F-4 The pod shall be designe

25、d for carriage on the centerline or inboard wing- station, as applicable to the specified aircraft, and shall be capable of captive flight. 3.3.2 Reliability. 3.3.2.1 Operational stability. The pod shall operate with required Derformance, continuously or intermittently, for a period of at leas hours

26、 or 1 year without the necessity for readjustment of any contro are inaccessible to the operator during normal use. 1 O0 s which 3.3.2.2 Operating life. The equipment shall have atotal operating life of not less than 300 hours with minimal servicing and replacement of parts. 4 Provided by IHSNot for

27、 ResaleNo reproduction or networking permitted without license from IHS-,-,-, T MIL-C-85372 LO 779770b 03b47LB 8 W I b! 1 L - C - 853 9 2 (AS) V). . w- N n.z I- O VI x I -I a W b- I -I w 5 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-C-5372 LO

28、 7777706 0364737 T c MIL-C-85392(AS) TABLE I. Weight and dimensions for the pod. Parameters Length Di ameter 1/ Vol Ume Weight Val ue 124.3 inches (3.16 meters) 15 inches (38.1 centimeters) 10.3 cubic feet (0.292 cubic meters) 645 pounds (292 ki 1 ograms) typical I/ Major diameter of casing excludin

29、g bomb lug wells, umbilical connector, ejector footpad and sway brace pads. 3.3.2.3 Reliability in mean-time-between-failure (MTBFL. The pod shall have a specified mean (operating) time between failures (MTBF) of 50 hours when tested and accepted as specified in 4.5.3. 3.3.2.4 Time totalizing meter.

30、 The following units shall contain time totalizing meters in accordance with MIL-M-7793: Unit Type Meter a. Signal Control Processor 875AS1006 M 7793/6-O01 b. Radio Transmitter 875AS1008 M 7793/6-001 3.3.3 Cabling and connections. 3.3.3.1 Umbilical connector. Input/output terminations to the pod for

31、 primary power, control signals, and audio/video information shall be made through the umbilical connector, AlW131, mounted on top of the casing assem- bly. The connector shall be type M81582/1E03SA and shall mate with the air- craft umbil ical connector type M81582/02E03PAl. The umbil ical connecto

32、r pin number assignment, function, and current/vol tage requirements shall be as specified in table II. Drawing 2300287 shall be provided to protect the umbilical connector when the pod is not in use, umbilical connector, shall run the length of the casing assembly and interconnect the main componen

33、t assemblies, 3.3.4 Controls. 3.3.4.1 Internal adjustments. No adjustments to the pod shall be required prior to its use with the following exceptions: must be preset to the desired position; the A4/A7-F4 switch must be selected for the correct type of aircraft; the circuiat breaker, CB1 must be pla

34、ced in the ON position; the channel select switch on the transmitter assembly or cockpit channel select switch must be set to match the channel of the weapon; and the video tape recorder must be loaded with tape and placed in RECORD, 3.3.5 Interchangeability, Physical and functional interchangeabili

35、ty shall exist for all units and replaceable assemblies, subassemblies, and parts of Guided Weapon Control-Monitor Set, AN/AWW-7D in accordance with A receptacle cover assembly in accordance with The main cable assembly, terminating in the The lA/C-PA/C switch 6 P Provided by IHSNot for ResaleNo rep

36、roduction or networking permitted without license from IHS-,-,-MIL-C-85372 LO 7777706 0364720 6 W MIL-E-5400. interchangeability for the pod. DL 875AS1000 shall be used as the standard to measure 3.3.6 Interference control. The generation of electromagnetic inter- ference by the pod and the vulnerab

37、ility of the pod to electromagnetic interference shall be controlled within the limits of MIL-STD-461 for Class Al and Class 81 equipment, standard conditions specified in 3.3.13 and in accordance with the procedures of MIL-STD-462 to demonstrate compliance with the requirements of MIL-STD-461. An E

38、MI/EMC test plan and a test report shall be prepared. 3.3.7 Maintainability. Maintainability provisions shall be incorporated within the design to provide for service, access, and repair of all assemblies. The replacement of major components within the pod shall be accomplished without soldering and

39、 without the need for special tools. routine testing of the pod shall be accomplished using the special test equipment listed in the operation and maintenance instructions manual for the pod, in addition to the standard test equipment normally available in Intermedi ate Maintenance shops. EM1 testin

40、g shall be accomplished under Normal 3.3.7.1 Test connections. Normal testing of the pod shall be accomplished without disassembly except that the forward and aft antenna terminations shall be disconnected so that RF test equipment may either monitor or supply signals to the antenna feed cables. 3.3

41、.7.2 Built-in-test. The major components that compose the pod shall have buil t-in-test (BIT) features to check critical parameters. 3.3.7.3 Periodic maintenance. The pod shall require one year periodic maintenance with the exception of the following: a. The desiccant breather system and desiccant s

42、torage bags shall require periodic servicing. b. The video tape recorder shall require periodic cleaning of the recording heads and tape path to ensure that recordings meet the specified requirements. 3.3.8 Transportability. The Guided Weapon Control-Monitor Set AN/AWW-7D shall be transportable by a

43、ir, rail, truck and ship when mounted in a shipping container as specified in section 5. 3.3.9 Storage life. 3.3.9.1 Packaged condition. The pod shall unsheltered areas when packaged to the requ normal storage environmental extremes shall between -65OC and 71OC. be capable.of being stored in rements

44、 of section 5. The be at any relative humidity 3.3.9.2 Unpackaged condition. The pod sha 1 be capable of safe storage in the unpackaged, assembled condition for not less than 2 years, in the weapon ready storage area of a shore installation, without impairment to form, fit, or function. Normal stora

45、 e environment extremes shall be at any relative humidity from -54OC to t60 C. storage. The desiccant breather system and desiccant storage bags shall be 3 Covers and plugs shall be in place during 7 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-.

46、MIL-C-5372 LO 7777706 03b472L W * P MIL-C-85392 (AS) serviced, replaced, or tested periodically as specified in the operation and maintenance instructions manual for the pod. No realignment of the pod, or its component parts shall be necessary after storage. 3.3.10 Nameplates and identification mark

47、ing. Serial number assignment, nameplate approval, and identification marking, shall be in accordance with MIL-N-18307. 3.3.10.1 Decal s , namepl ates, and marking 1 ocati ons . Al 1 decal s, nameplates, and marking shall be affixed to the pod in accordance with DL 875AS1000, and all referenced mark

48、ing specifications, documents, and drawings thereon. 3.3.10.2 Serial numbers. Serial numbers will be assigned by the procuring activity for the pods under contract or order. shall serialize sequentially all pods which are delivered under the contract. The contractor 3.3.10.3 Special warning decals.

49、The forward and aft radome assemblies shall be marked on each side surface and upper surface with warning decals labeled “NO STEP RADOME“. The decals shall meet all requirements of Drawing 184AS246. 3.3.11 Safety. The contractor shall ensure that system safety require- ments are in accordance with MIL-E-5400. 3.3.11.1 Flight safety. Flight safety procedures applicable to the associated aircraft, and the Walleye guid