NAVY MIL-C-85283 B-1994 CONTROL-MONITOR SET GUIDED WEAPON AN AWW-9B P N 1064AS4100《AN AWW-9B P N 1064AS4100O型制导武器控制系统监控器装备》.pdf

1、1 September I994 SUPERSEDING MIL-C-85283A(AS) 5 January 1988 MILITARY SPECIFICATION CONTROL-MONITOR SET, GUIDED WEAPON, AN/AWW-9BY P/N 1064AS4100 This specification is approved for use by the Naval Air Systems Command, Department of the Navy, and is available for use by all Departments and Agencies

2、of the Department of Defense. 1. SCOPE 1.1 ScoDe. This specification establishes the design, performance, manufacture, and acceptance requirements for the Control-Monitor Set, Guided Weapon AN/AWW-gB herein referred to as the Pod. The Pod covered by this specification is for airborne use and perform

3、s as a major component part of the data link communication network, providing transmission of command signals and reception of video data, between a control aircraft and a WALLEYE guided weapon or Standoff Land Attack Missile. specification consists of one major assembly. The equipment covered by th

4、is 2. APPLICABLE DOCUMENTS 2.1 Government documents. 2.1.1 Specifications. standards and handbooks. The following specifications, standards, and handbooks form a part of this document to the extent specified herein. Unless otherwise specified, the issues of these documents are those listed in the is

5、sue of the Department of Defense Index of Specifications and Standards (DODISS) and supplement thereto cited in the solicitation (see 6.2). Beneficial ccinments (recommendations, additions, deletions) and any pertinent data which may be of use in improving this document should be addressed to: Comma

6、nder, Naval Air Warfare Center Aircraft Division, Systems Requirements Department, Code SR3, Highway 547, Lakehurst, NJ 08733-5100, by using the self-addressed Standardization Document Improve- ment Proposal (DD Form 1426) appearing at the end of this document or by 1 etter. AMSC N/A FSC 1430 Distri

7、bution Statement A. Approved for pub1 ic release; distribution is unlimited. Licensed by Information Handling ServicesSPECIFICATIONS MILITARY MIL-D-3464 - MIL-W-5088 - MIL-M-7793 - MIL-A-8591 - MIL-E-17555 - MIL-N-18307 - MIL-H-46855 - MIL-C-81582/1 - MIL-C-81582/2 - MIL-T-81624 STANDARDS MILITARY M

8、IL-STD-129 MIL-STD-130 MIL-STD-454 MI L-STD-461 MIL-STD-462 MIL-STD-704 MIL-STD-781 MIL-STD-810 MIL-STD-965 Desiccants, Activated, Bagged, Packaging Use and Static Dehumidification. Wiring, Aerospace Vehicle. Meter, Time Totalizing. Airborne Stores, Suspension and Aircraft-Stores Interface (Carriage

9、 Phase), General Design Criteria for. Electronic and Electrical Equipment, Accessories, and Provisioned Items (Repair Parts); Packaging of. Nomenclature and Identification for Aeronautical Systems Including Joint Electronics Type Designated Systems and Associated Support Systems. Human Engineering R

10、equirements for Mil i tary Systems, Equipment and Facilities. Connectors, El ectri c, Bayonet Coupl i ng, Umbi 1 ical Receptacle, Jam Nut Mounting, RFI Shielded, Crimp Contact, Class E. Connector, Plug, Electric, Bayonet Coupl ing, Lanyard Release, RFI Shielded, Crimp-Type Contacts, Class E. Televis

11、ion Display Requirements for the Weapon System for Guided Weapon Mark 1 all Mods (WALLEYE) and Guided Weapon, Practice MK 4 Mod 0/1. Marking for Shipment and Storage. Identification Marking of U.S. Military Property. Standard General Requirements For Electronic Equipment. Requirements for the Contro

12、l of Electromagnetic Interference Emissions and Susceptibility. Measurement of Electromagnetic Interference Characteristics. Aircraft Electric Power Characteristics. Reliability Testing for Engineering Development, Qual i f icat i on , and Product i on. Environmental Test Methods and Engineering Gui

13、 del i nes . Parts Control Program. 2 Licensed by Information Handling ServicesMI L-C-85283B (AS) STANDARDS (Conti nued) MI L I TARY ( Con t i nu ed ) MIL-STD-1472 - Human Engineering Design Criteria for Military MIL-STD-5400 - Electronic Equipment, Airborne, General Systems, Equipment and Facilitie

14、s. Requirements for. HANDBOOKS b MILITARY MIL-HDBK-781 - Re1 i abi 1 i ty Test Methods, P1 ans, and Environments for Engineering Development, Qualification and Production. (Unless otherwise indicated, copies of federal and military specifications, standards, and handbooks are avail able from DODSSP

15、- Customer Service, Standardization Documents Order Desk, 700 Robbins Avenue, Bldg. 4D, Phi lade1 phi a, PA 1911 1-5094. ) 2.1.2 Other Government documents, drawinqs, and oublications. The following other Government documents, drawings, and pub1 ications form a part of this document to the extent sp

16、ecified herein. the issues are those cited in the solicitation. Unless otherwise specified, DRAWINGS NAVAL AIR SYSTEMS COMMAND 6 3A6 7A3 O 184AS163 184AS 166 184AS290 196AS 196 196AS212 196AS2 50 1035AS 11 5 1035AS120 1035AS193 1064AS 1 O 7 1064AS 141 1064AS142 1064AS 143 1064AS166 196AS501-3 - Brea

17、thing System. - - Video Amplifier Assembly (A5). - Foam Compound. - SCP Voltage Regulator. - 2.3 kHz Oscillator and Video Driver (All). - Power Supply Assembly (A6). - Receiver. - BIT No. 1 Assembly (A2) . - BIT No. 2 Assembly (A12). - Mixer, Double Balanced. - Casing Assembly. - Power Amp1 i fier.

18、- Vol tage Control 1 ed Osci 11 ator. - Low Pass Filter. - One Wire Demodulator Assembly. Sync Remover and Horizontal Generator Assembly (A4). 3 Licensed by Information Handling ServicesDRAWINGS (Continued) NAVAL AIR SYSTEMS COMMAND (Cont 1 nued) 1064AS190 1064AS 198 1 06 4AS 2 04 1064AS229 1064AS23

19、2 1 064AS 2 3 3 1 O 64AS3 O O 1064AS303 1064AS327 1064AS428 1064AS433 1064AS438 1064AS453 1064AS462 1064AS470 1064AS482 1064AS487 1064AS500 1064AS506 1064AS507 1064AS508 1064AS509 1064AS608 1064AS664 1064AS1178 1064AS1470 1064AS2139 1064AS2194 1064AS2281 1064AS2292 1064AS2440 1064AS2500 1064AS2650 1

20、064AS3150 1064AS41 O0 1064AS4101 1064AS4109 1064AS4110 1064AS4391 1342AS 13 5 1342AS 180 1342AS5 1 O 1 3 4 2 AS 5 20 BIT No. 3 Assembly (A13). Di pl exer. Transformer Assembly. Multiple Transmitter Assembly. Capacitor Assembly. Diode Assembly. Filter Assembly, Electrical. Circuit Breaker. Mu1 ti pl

21、ex Fi 1 ter (A3). DPSK Assembly No. 1 (A14). DPSK Assembly No. 2 (A15). DPSK Assembly No. 3 (A16). Logic Decoding Interface (A7). Mu1 ti pl ex Decoder and Li ne Recei ver (Alo). Antenna - Radome Assembly. Sync Regenerator Board 1 (A8). Sync Regenerator Board 2 (Ag). Television Receiver Assembly. Sam

22、pl e/Hold Video Ampl if i er Modul e (B5) . PJR Ci rcui t/AGC Modul e (82). Pul se AM Detector Module (B3). - t12V Regulator Module (Bl). Vibration Isolator. Transmitter Base/Heat Sink. Power Supply Board Assembly. .- - Antenna - Radome Assembly. - Radio Transmitter Assembly - Local Oscillator. - En

23、d Assembly. - Channel Sel ect/BIT Di spl ay - BIT No. 4 Assembly (A17). - Tel evi si on Receiver Assemb - Half Sine Modulator. - Transmitter Power SuDDlY A Assembly. Y. sembl y. - - Interface Control Drawing. - Schematic Diagram - Signal-Control Processor. - SLAM Discrete 5 Control (Al). - Special W

24、arning Decals. - - - Guided Weapon Controi Monitor Set AN/AWW-gB Video Cassette Tape Recorder (VCTR). De-Emphasi s Video Ampl if i er Modul e (A15). - +12V Regulator Module (A16). . 4 I Licensed by Information Handling Services flIL-C-85283B 9999906 1990395 198 MI L-C-85283B(AS) DRAWINGS (Continued)

25、 NAVAL AIR SYSTEMS COMMAND (Continued) 1342AS531 - Pre-amp1 ifier (Al); Sample/Hold Module (A12). 1342AS532 - Filter, Band Pass (A2). 1342AS533 - Mixer, Microwave (A3). 1342AS535 - FM Limiter/Discriminator (A14). 184AS290 - Foam Compound. 196AS196 - SCP Voltage Regulator. 2300287 - Cover Assembly, R

26、eceptacle. TECHNICAL MANUALS NAVAL AIR SYSTEMS COMMAND NAVAIR 16-30AWW9-3 - Guided Weapon Control Monitor Set AN/AWW-gB. NAVAIR 16-30AWW9-3A - Guided Weapon Control Monitor Set AN/AWW-gB, Classified Supplement. (Copies of other Government documents, drawings, and pub1 ications required by contractor

27、s in connection with specific acquisition functions should be obtained from the contracting activity or as directed by the contracting activity.) this document and the references cited herein, the text of this document shall take precedence. Nothing in this document, however, shall supersede applica

28、ble laws and regulations unless a specific exemption has been obtained. 2.2 Order of wecedence. In the event of a conflict between the text of 3. REQUIREMENTS 3.1 First article. When specified (see 6.2), a sample shall be subjected 3.2 Parts and materials. to first article inspection (see 4.3 and 6.

29、4). monitor sets shall conform to the requirements of the drawings and subsidiary speci fi cat ions speci f ied herein, except i nsofar as errors on the drawings may be incompatible with the requirements of this specification and related specifications. Unless otherwise specified in the contract, pr

30、oposed changes, either to correct drawing discrepancies or to effect improvements, shall be subject to the acceptance of the contracting activity. The parts and materials used in the control- 3.2.1 Nonstandard parts and material approval. Approval for the use of nonstandard parts shall be obtained b

31、y the contractor in accordance with MIL-STD-965, Procedure I. Approval for use of materials shall be obtained by the contractor in accordance with MIL-STD-5400. 5 Licensed by Information Handling Servicesw MIL-C-85283B 9999906 1990396 024 Parameters 3.2.2 Sumlemental requirements. In the event that

32、the contractor proposes to alter the equipment specified herein and applicable drawings, the following supplemental requirements for the selection of parts and materials are appl i cab1 e. Value 3.2.2.1 Basic conformance. Parts and materials selected for use in the Pod shall conform to the requireme

33、nts of MIL-STD-5400. 3.3 Desiqn and construction. The Pod shall be manufactured in accordance with the drawings and subsidiary specifications listed in Drawing 1064AS4100 and related lists, except insofar as errors of omission or commission on the drawing may be incompatible with the requirements of

34、 this and related specifications. In any case, it is a condition of final acceptance that the Pod manufactured shall meet all the performance requirements of this specification, and such acceptance test documents as may be applicable. Proposed changes, either to correct drawing discrepancies or to e

35、ffect improvements, shall be specifically accepted by the contracting activity prior to their incorporation. 3.3.1 Physical characteristics. 3.3.1.1 DescriDtion. The Pod shall consist of three major sections: The forward radome assembly, aft radome assembly, and the casing (center body) assembly. Al

36、l principal dimensions and locations of particular features, including center-of-gravity, shall be as detailed in table I and on figure 1. TABLE I. Weiaht and dimensions for the Pod. Length Di ameter I/ Vol urne Weight 124.3 inches 15 inches 10.3 cubic feet 690 pounds max - i/ Major diameter of casi

37、ng excluding bomb lug wells, umbilical connector, heat sink, ejector foot pad and sway brace pads. 3.3.1.2 Total weiciht. Total weight of the Pod shall be not greater than 690 pounds. 3.3.1.3 Fliqht requirements. The Control-Monitor Set, Guided Weapon AN/AWW-gB shall be in accordance with Drawing 10

38、64AS4100 and shall be functionally compatible and flight certifiable as an emergency jettisonable Pod on the following aircraft: 6 Licensed by Information Handling Services MIL-C-85283B 99999Ob 1990397 TbO MI L-C-85283B (AS) 5i U o a 9 4 n a 4 Y 2 2 c v I i s= 2 U? s/ L 2 F. o- N o z 7 Licensed by I

39、nformation Handling ServicesMIL-C-85283B 9999906 I1990398 9T7 a. A-4 b. A-7A/B/E C. TA-7C d. F/A-18 The AN/AWW-gB Pod shall be designed for wing-station, as applicable to the spec captive fl ight. carriage on the center1 ine or inboard fied aircraft, and shall be capable o 3.3.2 Re1 i abi 1 i tv. 3.

40、3.2.1 Operational stabilitv. The Pod shall operate within the required performance, continuously or intermittently, for a period of not less than 100 hours without the necessity for readjustment of any controls which are inaccessible to the operator during normal use. i 3.3.2.2 Operatins life. The P

41、od shall have a total operating life of not less than 300 hours with minimal servicing and replacement of parts. Parts requiring scheduled replacement due to wear during the life of the Pod, and the wearout life of such parts, shall be determined by the contractor. 3.3.2.3 Re1 iabil itv in mean-time

42、-between-failure (MTBF). The Pod shall have a specified mean (operating) time between failures (MTBF) of 50 hours. 3.3.2.4 Time totalizina meter. The following units shall contain time totalizing meters in accordance with MIL-M-7793: - Unit Tvpe Meter a. Transmitter Power Supply 1064AS3150 M7793/6-0

43、01 b. Signal-Control Processor 1064AS4110 M7793/6-001 3.3.3 Construction. 3.3.3.1 Cablins and connections. 3.3.3.2 Umbilical connector. Input/output terminations to the Pod for primary power, control signals, and audio/video information shall be made through the umbilical connector, AlW1J1, mounted

44、on top of the casing assembly. The connector shall be in accordance with MIL-C-81582/1 part number type M81582/1E03SA and shall mate with the aircraft umbilical connector MIL-C- 81582/2 part number type M81582/02E03PAl. assignment, function, and current/vol tage requirements are specified on Interfa

45、ce Control Drawing 1064AS4101. A receptacle cover assembly in accordance with Drawing 2300287 shall be provided to protect the umbilical connector when the equipment is not in use. The umbil ical connector pin number 8 Licensed by Information Handling Services3.3.4 Controls. 3.3.4.1 Internal adjustm

46、ents. No adjustments to the Pod shall be a. required prior to its use with the following exceptions: The lA/C-ZA/C switch on the Transmitter Power Supply must be preset to the desired position. b. The circuit breaker, CB1 must be placed in the ON position. c. The FSK/AUTO modulation switch inside th

47、e Signal-Control Processor (SCP) must be set to the desired modulation method. d. The channel select switch on the Transmitter Power Supply must be set to match the channel of the weapon. e. The Video Cassette Tape Recorder must be loaded with a tape cassette. 3.3.5 Interchanseabil itv. Physical and

48、 functional interchangeability shall exi st for al 1 units and rep1 aceabl e assembl i es, subassembl i es, and parts of Control-Monitor Set, Guided Weapon AN/AWW-gB, in accordance with MIL-STD- 5400. The drawings listed in Drawing 1064AS4100 shall be used as the standard to measure i nterchangeabi

49、1 i ty for the AN/AWW-9B Pod. 3.3.6 Interference control. The generation of electromagnetic inter- ference by the Pod and the vulnerability of the Pod to electromagnetic interference shall be controlled within the limits of MIL-STD-461 for Class IA and Class IB equipment. EM1 testing shall be accomplished under standard conditions specified in 3.3.12 and in accordance with MIL-STD-462 to demonstrate compliance with the requirements of MIL-STD-461. interference control plan shall not be required. A complete 3.3.7 Maintainability. Maintainability provisions shall be incorporated w