NAVY MIL-R-21073 A-1960 RECORDER MAGNETIC DISTORTION RO-32 ASQ《RO-32 ASQ型磁失真记录仪》.pdf
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1、/-7 MIL-R-211073A 66 7997706 01130257 5 = l5APRIL 1960 MI L-R-21073 (AER 1 I MAY 1958 SUPERSEDING MILITARY SPECIFICATION RECORDER, MAGNETIC DISTORTION, RO-32/ASQ This specification has been approved by the Bureau of Naval Weapons, Department of the Navy. 1. SCOPE 1.1 S cope - The equipment covered b
2、y this specification shall provide a dual recording milliammetewable of recording energy in the frequency range of O to 3 cps on suit- able paper when energy is applied from either or both of two separate sources. Classification - The Recorder, Magnetic Distortion, RO-32/ASQ shall be of one type and
3、 shall cons- of the folIowing: 1.2 Max. Allow. Max. Type Size (Inches) Allow. APPl. Item Designation w H/L D Wt. Lbs. Para. Recorder, Magnetic Distorition RO-32/ASQ 5-3/4 7-318 6-1/2 8.8 3.5 2. APPLICABLE DOCUMENTS 2.1 SPECIFICATlONS Genezal - The following documents of the issue in effect on the da
4、te of in- vitation for bids form amthis specification to the extent specified herein: Militarv MIL-E-4682 Electron Tubes and Transistors, Choice ad Application of MIL-W-5088 Wiring, Aircraft, installation of MIL-E-5400 Electronic Equipment, Aircraft, General MIL-T- 5422 Specification for Testing; En
5、vironmental Aircraft Electronic Equipment interference Limits, Tests and Design Requirements, Aircraft Electrical and Electronic Equipment Control Panel; Aircraft Equipment, Rack or Console Mounted MIL-1-6181 MIL-C-6781 MIL-P-7788 Plate, Plastic, Cockpit and Interior Controls Provided by IHSNot for
6、ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-R-2L073A bb 797770b OL30Zb0 1 MIL-R-21073A (WEP) MIL-P- 17555 Preparation for Delivery of Electronic Equipment; Miscellaneous Electrical Equipment (Except Rotating Electrical Equipment) and Associated Repair Parts inspect
7、ion, for Aircraft Electronic Equipment; Format for Nomenclature and Nameplates for Airborne Electronic and Associated Equipment Fastener, Control Panel, Aircraft Equipment MIL-T-18303 Test Procedures, Preproduction and MIL- N- 1 8307 MIL- F-25173 STANDARDS Military MIL-STD-704 Electric Power, Aircra
8、ft, Characteristics and Utilization of MS 25245 Connections - input Power Airborne Electronic Equipment; 28-Volt DC, 115-Volt Single Phase AC, and/or 115/200-Volt Three Phase AC, or combinations PUBLICATIONS - LWreau of Naval Weapons EI- 3 5 2 Avionics Installation Instruction for Magnetic Distortio
9、n Recorder RO-32/ASQ SAR-300 Material Changes and Material Bulletins; Preparation of 2.2 Availability of Documents - (1) When requesting specifications, standards, drawings, and publications refer to both title and number, Copies of this specification and applic- able specifications required by cont
10、ractors in connection with specific procurement functions may be obtained upon application to the Commanding Officer, Naval Supply Depot, Code CDS, 5801 Tabor Avenue, Philadelphia 20, Pennsylvania. 3, REQUIREICIENTS of major design objectives shall be th e prime consideration. in so doing, the follo
11、wing shall (1) Parts and materials requirements shall conform to Specification (2) Nonrepairable subassemblies, as outiined in specification MIL-E-5400, shaii be used when practicable. The general size of the subassembly, and the amount of circuitry to be included therein shall be approved by the pr
12、ocuring activity, Nonrepairable subassemblies must be reliable. A mean-time-to failure of more than 5000 hours should be the goal of a. 1 Parts and Materials - In the selection of parts and materials, fulfillment govern: MIL-E-5400, each, i. IL.- - - 2 Provided by IHSNot for ResaleNo reproduction or
13、 networking permitted without license from IHS-,-,-MIL-R- 21073A NEP) (3) When previously produced models of this equipment did not use non- repairable subassemblies, the design shall not be changed to employ nonrepairable assemblies without the approval of the procuring activity, 3.1.1 Nonstandard
14、Parts and Material Approval - Approval for the use of non- standard parts and materials shall be obtained as outlined in Specification MIL-E-5400. Electron Devices - Electron tubes, transistors and diodes shall be chosen and applied, and the complements reported as outlined in Specification MIL-E-46
15、82. The comple- ment report ,must be submitted to the procuring activity for review and approval prior to prepro- duction testing. . 3.1.2 3.2 Design and Construction - 3.2.1 General - The equipment shall conform with all the applicable requirements of Specification MlL-E-mr design, construction and
16、 workmanship, unless otherwise specified herein. Service Conditions - The equipment shall operate satisfactorily under any of the environmental and mechanical service conditions or reasonable combination of these condi- tions as specified in Specification MIL-E-5400 for Class I equipment, with the f
17、ollowing modifica- tions: 3.2.2 3.2.2.1 Temperature - The equipment shall operate satisfactorily over the temp- erature rangel of minus 30“ to plus S3“C. Altitude - The equipment shall operate satisfactorily at all altitudes from sea level to 10,000 feet.Nopermanent damage shall result when the equi
18、pment is transported to any altitude up to 50,000 feet while in an operating or non-operating condition. Satisfactory opera- tion shall resume immediately when pressure equivalent to 10,000 feet altitude is returned. estabiish normal performance requirements and for making laboratory bench tests on
19、the equip- ment. 3. 2. 2. 2 3. ?. 3 Standard Conditions - The following conditions shall-be used as a basis to Temperature Room ambient 25C 115.C Altitude Normal ground Vibration None Humidity Input power voltage Room ambient up to go% relative humidity 115 however, there are no requirements on equi
20、pment performance at frequencies below the lower established operating limit. input Power Connection - input power connections shall be in accordance with MS 26246, except that the inverter starting reiay circuit is not required. Overload Protection - Overload protection for the equipment shall be p
21、ro- vided in the equipment. AL1 parts and circuits of the equipment which are likely to carry an over- load due to any failures or poor adjustments shall have suitable protective devices or shall be proportioned to withstand such overload without permanent damage to the equipment, The use of fuzes a
22、nd other protective devices shall be held to a minimum. below the mnimum specified and shall automatically resume normal operation when the voltage returns within limite. 3.2.7 Control Panels - All rack or console mounted control panels shall conform 3.2.8 3.2.8.1 3.2.9 3.2.10 3.2.10,l ndervoltage P
23、rotection - The equipment shall not be damaged by voltages 3.2.11. Moisture and Fungus Resistant Treatment - Equipments shall be fungue- proofed by selection of parts and materials as non-nutrient for fungu s or the parts and materials ahall be treated prior to their use in the equipment so that ove
24、r-all spraying of the equipment is not necessary. approval for equipment Identification shall be in accordance wth Specification MIL-N-18307. See 6.4, quirements as defined in Specification MIL-E-5400. shall be as specified in Specificatio- . pec c test points and test facilities shall be provided t
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