NAVY MIL-T-85032 A-1980 TEST SET GUIDED WEAPON AN DSM-92C《AN DSM-92CB制导武器试验装置》.pdf

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1、HZL-T-85032A 47 W 7777706 0257547 7 . MI L-T- 85032A( AS) 7 July 1980 Superseding MIL-T-85032( AS) MILITARY SPECI FICATION TEST SET, GUIDED WEAPON AN/DSM-gPC This specification is approved for use by the Naval Air Systems Command, Department of the Navy and is available for use by all Departments an

2、d Agencies of the Department of Defense. 1. SCOPE 1.1 Scope. The equipment (Test Set) covered by this Specification. shall be for flightline and shop use to perform an operational readiness check (GO/NO-GO) of WALLEYE weapons defined in 6.1. 2. APPLI CABLE DOCUMENTS 2.1 Issues of documents. The foll

3、owing documents of the issue in effect on the date of invitation for bids or request for proposal, form a part of this specification to the extent specified herein. SPECI FICATIONS Federal PPP-B- 636 - Boxes, Shipping, Fiberboard Mi 1 i tary MIL- P-.l16 - Preservation-Packaging, Methods of MI L-E- 5

4、400 - Elecfxonic Equipment, Airborne, General Specification for MIL-T-5422 - Testing, Environmental, Aircraft Electronic Equipment MIL-E- 17555 - Electronic and Electrical Equipment, Accessories, and Repair Parts; Packaging and Packing of Beneficial comnents (recomendations, additions , deletions) a

5、nd any pertinent data which may be of use in improving this document should be addressed to: Comnanding Officer, Naval Air Engineering Center, Engineering Specifications and Standards Department (ESSO Code 93, Lakehurst, NJ 08733, by using the self-addressed Standardization Document Improvement Prop

6、osal (OD Form 1426) appearing at the end of this document or by letter. t I Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-T-85032A Li7 777770b 0257548 O 9 llIL-T-85032A( AS ) MIL-T-18303 MIL-T-28800 HIL-F-23419 M IL -A - 5 53 3 9 STANDARDS Fede

7、ral FED STD 123 Military MIL-STD-108 MIL-STD-129 MIL-STD-130 M IL - S TD - 1 6 7 MIL -STD -461 M IL-STD-704 NIL-STD-781 - Test Procedures; Preproduction , Acceptance , and Life, for Aircraft Electronic Equipment , Format for Electronic Equipment , General Specification for - Test Equipment for use w

8、ith Electrical and - Fuses, Instrument Type , General Specification for - Adapter , Connector, Coaxial , Radio Frequency (Between Seri es and Ni thi n Series), General Specification for - Marking for Shipment (Civil Agencies) - Definitions of and Basic Requirements for Enclosures for Electric and El

9、ectronic Equipment - Marking for Shipment and Storage - Identification Marking of US Military Property - Mechanical Vibrations of Shipboard Equipment (Type I - Environmental and Type II - Internally Excited) - Electromagnetic Interference Characteris- tics Requirements for Equipment - Electric Power

10、, Aircraft Characteristics and Utilization of - Re1 iabil ity Tests: Distribution Exponential f.1 IL -STD - 81 O - Environmental Test Methods tl IL-STD -965 - Parts Control Program MS17322 - Meter, Time Totalizing, Miniature, Digital , 115 Volt, 400 Hertz 2 Provided by IHSNot for ResaleNo reproducti

11、on or networking permitted without license from IHS-,-,-DRAW IN GS DL 1008S1000 -Data List for Guided Weapon Test Set NAVA1 R 16- 30DSM92-2 -Maintenance Instructions (Organizational, (Copies of specifications, standards, drawings, and pub1 ications required bjr contractors in connection with specifi

12、c procurement functions should be obtained flrom the procuring activity or as directed by the contracting officer.) 3.2.1 General. The parts and materials specified in the drawings and 9 related documents for use in the construction of this equipment were selected to ensure the fulfillment of all th

13、e requirements of this specification. specified parts and materials necessarily places both the burden of proof for the acceptability of the change and the associated cost upon the cnntractor. Approval for deviations must be requested from the procuring activity by the contractor and granted by the

14、Government representative prior to submission of equipments for preproduction (first article) tests. Approval of parts and material deviations shall not be construed by the contractor to constitute a waiver of the performance requirements or any other requirements of this suecification. Any deviatio

15、n by the contractor from the use of these specified in MIL-STD-965. 3 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-3.2.3.2 in terc hangea b conforming to abil ity of al 3.3 Dee accordance wi MIL-T-85032A LI9 0b 0257550 7 m MIL-T-85032A( AS) 3.2.3

16、Supplemental requirements. In the event that the contractor proposes to alter the equipment delineated by this specification and applicable drawings, the following supplemental requirements for the selection of parts and materials shall be applicable. 3.2.3.1 Basic conformance. Materials selected fo

17、r use in the equipment shall be as specified in MIL-T-28800. Parts shall be selected from those conforming to MIL-E-5400, unless the parts listed therein will not perform adequately in the intended applications and environments specified herein in which case 3.2.2 applies. Interchangeability. All pa

18、rts and materials shall meet the lity requirements as specified in MIL-T-28800. DL 1008AS100 shall be the standard for measuring interchange- gn and construction. The Test Set shall be manufactured in h the drawings and subsidiary specifications conforming to DL The drawings applicable units, assemb

19、lies, subassemblies and parts. 1008AS100 and related lists, except that errors of omission or commission on the drawings may be incompatible with the requirements of this and related specifications. In any case, it is a condition of final acceptance that the equipment manufactured shall meet all the

20、 design, construction, and workman- ship requirements of this specification and applicable acceptance test docu- ments. Proposed changes, either to correct drawing discrepancies or to effect improvements, shall be specifically approved by the procuring acti- vity prior to being incorporated. (see 6.

21、2) 3.3.1 Reliability. 3.3.1.1 Operational stability. The Test Set shall operate satisfac- torily, continuously or intermittently, for a period of at least 300 hours. During this time, it shall not be necessary to readjust any controls that are inaccessible to the operator during normal use. operatin

22、g life of 2000 hours with reasonable servicing and replacement of parts. A list of parts requiring scheduled replacement due to wear during the life of the equipment, and the wearout life of such parts, shall be made available to the procuring activity. shall have a specified mean (dperating) time b

23、etween failures of 300 hours when tested in accordance with 4.6.3. 1008AS107 of DL 1008AS100) of the equipment shall contain a time totalizing meter of the type specified in MS17322-6A. 3.3.1.2 Operating life. The Test Set shall have a minimum total 3.3.1.3 Reliability in mean-time-between-failures

24、(MTBF). The Test Set 3.3.1.4 Time totalizing meter. The Weapon Control Assembly (drawing 4 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-T-85032A 99 m 7799906 0257551 O m 11 IL-T-85032A( AS) 3.3.2 Standard conditions. The following conditions s

25、hall be used to establ ish the normal performance characteristics under standard conditions for performing laboratory bench tests : a. Temperature Roan ambient (30 f 10C) b. Altitude Normal ground c. Vibration Rone d. Humidity Rom ambient up to 90% relative humidity e. Input Power Voltage 115 ? 11.5

26、 VAC, 400 f 20 Hz, 3-phase (Rotation ABC) 3.3.2.1 Service conditions. The test set shall operate satisfactorily under the following environmental service conditions. 3.3.2.1.1 Temperature-altitude. The test set shall meet the operating requirements of this specification at temperatures between t88“C

27、 and -62C at altitudes between ambient and 50,000 feet (16,000 meters). 3.3.2.1.2 Drip-proof. The test set shall meet the test requirements of MTL-STD-108 for drip proof test except the equipment shall be inclined only 15 degrees. The equipment shall operate during and after exposure. HIL-STD-810, M

28、ethod 507.1, Procedure I, including Method 507.1 paragraph entitled Summary, except the maximum temperature shall be 5OOC. HIL-STD-810, Method 509.1, Procedure I, including Method 509.1 paragraph entitled Sumnary. 3.3.2.1.3 Humidity. The test set shall mee? the test requirements of 3.3.2.1.4 Salt sp

29、ray. The test set shall meet the test requirements of 3.3.2.1.5 Explosive atmosphere. The test set shall meet the test requirements of MIL-STD-810, Method 511.1, Procedure I, including Method 511.1 paragraph. entitled , Summary, except the maximum temperature shal.1 be 55C and the maximum altitude s

30、hall be 10,000 feet (3,000 meters). 3.3.2.1.6 Vi brati on. MIL-STD-167, Type I. The test set shall meet the test requirements of 3.3.2.1.7 Shock. The MIL-STD-810, Mew516.1, entitled Summary. The equ test set shall meet the test requirements of Procedure I , including Method 516.1 paragraph pment sha

31、ll not be operating during the test. 3.3.3 Warm-up time. priorto operation shall not exceed 10 minutes under standard conditions and 20 minutes under service conditions. he time required for the equipment to warm-up 5 Provided by IHSNot for ResaleNo reproduction or networking permitted without licen

32、se from IHS-,-,-I?L-T:85032A 49 9999906 0257552 2 J H IL-T-85032A ( AS ) 3.3.4 Primary input power requirements. The test set shall meet all applicable input power requirements as specified in MIL-STD-704 for class 2 equipment. The power required shall be of the following type and shall not exceed t

33、he specified values: Il5 f 11.5 VAC, 400 f 20 Hr, %phase, 4 wire system (neutral ground), phase rotation (ABC) , 100 VA. 303.4.1 Protection. The Test Set shall be capable of withstanding inpiit power variations imposed by abnormal electric system operations as specified in MIL-STD-704. 3.3.5 Electro

34、magnetic interference suppression. The generation of radio interference by the Test Set and the vulnerability of the equipment to radio interference shall be asspecified in NIL-STD-461 for class ID equipment except that the limits for conducting electromagnetic emissions (switching transients) are i

35、n excess of the values of MIL-STD-461. for test methods CEO1, CE02, CE03, CE04, and CE05 apply. transients are as follows: . Limits Limits on the a. POWER ON/OFF switch transients are permissible on the equipment input power leads 30 dBA above the limits of MIL-STD-461 in the frequency range of 30 H

36、z to 50 MHz. STATION SELECT switch transients are permissible on the equipment input power leads 10 dBA above the limits of MIL-STD-461 in the frequency range of 30 Hz to 50 MHz. c. Transients caused by operating the equipment POWER ON/OFF switch are permissible on the equipment power leads (400 Hz)

37、 to the load (WALLEYE weapon) 50 dBA above the limits of MIL-STD-461 in the frequency range of 30 Hz to 50 MHz. b. 3.3.6 Dimensions. The dimensions of the Test Set case shall be as fol 1 ows : a. Length - 12“ (30.48 cmsj b. Width - 19-1/2“ (49.53 cm) c. Depth - 13-6/8“ (34.61 cm) 3.3.7 Weight. The t

38、otal weight of the equipment, including cables shall not exceed 50 pounds (22.5 kgs). 3.3.8 Color and finish. The color and finish of the equipment shall be in accordance .with drawing 1008AS105 of DL 1008AS100. identification marking shall be in accordance with MIL-STD-130 and as specified in DL 10

39、08AS100. 3.3.9 Identification plate and item markings. Nomenclature and 6 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-T-85032A L19 m 9999906 0257553 L1 MIL-T-85032A( AS) 3.4 Performance. The performance of the test set shall be as specified h

40、erein in addition to the performance requirements specified in DL 1008AS100. Un1 ess otherwise speci fi ed, these requi rements shall apply under both standard and extreme service conditions. When reduced performance re- quirements for service conditions are acceptable, such variations are speci fi

41、ed . herein. 3.4.1 Functions. The Test Set shall perform the functions specified 3.4.1.1 Power ON/OFF switch. The power ON/OFF switch shall permit the vidicon gyro to attain rated speed, and the vidicon filaments to warm up prior to uncaging the gyro and totally energizing the WALLEYE weapon. incorp

42、orated to prevent mechanical uncaging of the vidicon gyro before the gyro fias attained operating speed. guidance section of various weapons. -This switch shall also control the mechanical caging and uncaging of the vidicon gyro. cross hairs of the weapons vidicon onto the target-pattern display of

43、AN/DSM-779 Test Sets. 3.4.1.2 Time-delay relay. A 2-minute thermal time-delay relay shall be 3.4.1.3 Station select. The STATION SELECT switch shall energize the 3.4.1.4 Lock-on. The LOCK-ON switch shall enable the locking of the This checks weapon lock-on and tracking functions. 3.4.1.5 Gimbal enab

44、le. The GIMBAL ENABLE switch and circuitry shall be capable of offsetting the vidicon gyro in azimuth and elevation. 3.4.1.6 Roll gyro. The roll gyro circuit shall be capable of caging the gyro. 3.4 e 1.7 Dome-heater overri di ng ci rcui t. Prevent i on of operat i on of the dome heater iaccompl ish

45、ed with the dome-heater nv I-rriding circuit. returri the mechanically-caged position of the vidicon gyro to weapon boresi ght . . stop the motor of the video tape recorder (Mk 4 Mods 1 and 4). 3.4.1.8 m. Thecaging retainer and boresighter test circuit shall 3.4.1.9 Film advance. The FILM ADV switch

46、 and circuit shall start and 3.4.1.10 Intent-to-launch. The INTENT-TO-LAUNCH circuit shall supp +28 VDC to the launch relay of Mk 4 weapons only. 3.4.1.11 Self-test. The Test Set shall have a self-test capability This shall include testing of t12, -12, and t28 VDC power supply outputs video indicato

47、r operation test without the use of an external video generator. 3.4.1.12 Video dis la . The video display shall be capable of pre- senting externa y video or of monitoring internal video patterns for self- test purposes. 7 Y and Provided by IHSNot for ResaleNo reproduction or networking permitted w

48、ithout license from IHS-,-,-MIL-T-85032A( AS) 3.4.1.13 Video switch. The video switch shal functions : a. cockpit b. guidance c. test d. e. f. provide the following 300 lines 200 1 ines shades 3.4.1.13.1 Cockpit. In the COCKPIT position, the video display shall exhibit external video when a video si

49、qnal is applied to pin 37 of conne tor - *. WlP1 6 3.4.1.13.2 Guidance In the GUIDANCE position, external video shal appear on the video display when a video signal is applied to pin 50 of connector 32. 3.4.1.13.3 Test. In the TEST position, the video display shall exhibit external video when a video signal is applied to connector W2P4 or to pin 5 of connector W2P2. 3.4.1.13.4 300 lines. In the 300 LINES position, a 300-line stab