NAVY MIL-N-81604 C-1976 NAVIGATION SET INERTIAL AN ASN-92(V)《AN ASN-92(V)型惯性航海装备》.pdf
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1、Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-1.3 associated equipment listed in 6.6. Associated Equipment - This equipment shall operate with the 1.4 Appendix - Appendix I is included in this specification for information, except as required by co
2、ntract, as to the applica- tion of the CAZNS equipment: in the E-2C aircraft. 2 APPLICABLE DOCUMENTS 2.1 General - The following documents form a part of this speci- fication to the extent specified herein. of the documents in effect for the previous procurement. in lieu of the issue listed, the con
3、tractor shall use the latest issue in effect of these documents where feasible. the latest issue will affect design performance or interchange- ability of anv rerdaceable part, then the issue of the document Listed are the issues However, If the use of used. listed-below ihaii be SPEC IFICATIONS Mil
4、itary MIL-B-5087 MIL-C-172C Amendment 2 MIL-C-6781B MIL-D-81124B MIL-D-81170B MIL-E-17555G MIL-E-5400K Bonding, Electrical for Aerospace Systems Cases, Bases, Mounting: and Mounts, Vibration (For use with Electronic Equipment in Aircraft) Control Panel: Aircraft Equipment, Rack or Console Mounted Di
5、gital Data Communications Set AN/ASW-25B Digital Data Communication Set, * AN/ASN- ( * ) Electronic and Electrical Equipment * and Associated Repair Parts, Preparation for Delivery of Electronic Equipment Aircraft, General Specification for * .k * * * * 2 , Provided by IHSNot for ResaleNo reproducti
6、on or networking permitted without license from IHS-,-,-Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-N-LbOqC 58 77777Ob 0171115 T MIL-N-81604C(AS) Para 2.1 (cont) Naval Air Systems Command (cont) AR-1OA AR-15 AR-34 AR-57A AR-65 XAS -1 23 3A ST
7、ANDADS Mi1,itary MIL-STD-275 MIL-STD-461B MIL-STD-462 Maintainability of Avionics Equipment and Systems, General Requirements for Programmable Airborne Computer Data Failure Classification for Reliability Testing, General Requirements for Shipboard Alignment Specification CAINS E-2C Computer Perform
8、ance Specification Calibration and Maintenance Console Printed Wiring for Electronic Equipment Electromagnetic Interference Characteristics, Requirements for Equipment Electromagnetic Interference Characteristics, Measurement of MIL-STD-463 MIL-STD-470 MIL-STD-704A MIL-STD-781B MIL-SFD-785 Deinition
9、s and Systems of Units, Electromagnetic Interference Technology Maintainability Requirements Electric Power, Aircraft, Characteristics and Utilization of Reliability Tests, Exponential Distribution Parts and Equipment, Procedures for Packaging and Packing of Reliability Proqam for Syttms aid Equipmn
10、t Development and Production 4 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-Military (cont) MIL-STD-81OB Environmental Test Methods MIL-STD-1130 Connection, Electrical, Solderless Wrapped MS-17322D Meter, Time Totalizing Miniature Digital 115V 400
11、 Cycle * * * . . 2.1.1 Availability of Documents - When requesting specifications, standards, drawings, and publications, refer to both title and number. Copies of this specification and applicable specifica- tions required by contractors in connection with specific procure- ment functions may be ob
12、tained upon application to the Commanding Officer, Publications and Forms Center, Code 105 Tabor Avenue, Philadelphia, Pennsylvania 19120. 3. REQUIREMENTS 3.1 Preproduction - This specification makes provision for pre- production testing. a. Microelectronic technology shall be considered and . micro
13、electronic items shall conform to requirements specified herein. b. Other parts and materials requirements shall conform to MIL-E-5400. c. Nonreparable subassemblies shall be used in accordance with Specification AR-10 and as outlined in MIL-E-5400. * (Refer to 6.5.) * d. When previously produced mo
14、dels of this equipment did not use nonreparable subassemblies, the design shall not be changed to employ nonreparable assemblies without the approval of the procuring activity. 5 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-N-8lhOLlC 58 a 7777
15、706 0171lL7 3 3.2.1 Nonstandard Parts and Materials Approval - Approval for the use of nonstandard parts and materials (including electron tubes, transistors and diodes) other than microelectronic devices shall be obtained as outlined in MIL-E-5400. Microelectronic * devices shall be approved as out
16、lined in AR-5. 3.2.2 Microelectronic Modular Assemblies - When used, micro- AR-5. Conformal coatings, encapsulants, embedments, or potting materials used with modular assemblies (designated as reparable) containing integrated circuits and discrete parts shall be easily removable without damage to th
17、e assembly. 3.2.3 Modules - The electronic portions of the equipment shall be functionally modularized in accordance with AR-i0 when prac- ticable. not incorporate AR-10, the design shall not be changed to incor- 3.3 tion, and workmanship, except as otherwise specified herein. 3.3.1 Total Weiqht - T
18、he total weight of the equipment, excluding cables, the CAU, and the CAU mount, shall. be a minimum consistent with good design and shall not exceed 103.6 pounds with 12K words of computer memory. For the maximum WRA weights, refer to 3.5. 3.3.2 3.3.2.1 Operational Stability - The equipment shall op
19、erate with satisfactory performance continuously or intermittently for a period of at least 700 hours without the necessity for readjust- ment of any control other than that required to initiate an equipment recalibration sequence. The equipment shall not re- quire calibration more frequently than e
20、very 300 operational hours to meet the equipment performance requirements specified herein. electronic modular assemblies shall meet the requirements of * When previously produced models of this equipment do parate AR-10 without the approval of the procuring activity. all applicable requirements of
21、MIL-E-5400 for design, construc- * * Desiqn and Construction - The equipment shall conform with For CAU weight, refer to Appendix I. * Reliability - A Reliabilitv Plan shall he provided in accordance with) EILT,-STD-785. I Shipboard recalibration shall be performed with equip- peratinq Life - The eq
22、uipment shall have a total ment designed in accordance with XAS-1233, or equivalent. * 3.3,2.2 operating life of 10,000 hours with reasonable servicing and replacement of parts. Parts requiring scheduled replacement shall be specified by the contractor and approved by the pro- curing activity before
23、 use in the equipment design. 6 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-(operating) time between- failures when tested in accordance with MIL-STD-781B. The reliability apportionment (minimum MTBF/unit) shall be as shown in table I. I TABLE I.
24、 RELIABILITY APPORTIONMENT Unit inertial Measuring Unit (IN) Air Navigation Computer Unit (ANCU) Control Indicator Unit (CIU) Power Supply Unit (PSU) Converter Amplifier Unit (CAU) MTBF (Minimum) 1,800 hours 2,000 hours 13,200 hours 17,300 hours 4, 1.75 hours 3.3.2.4 Elapsed Time Indicators. Each un
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