NAVY MIL-T-22007 A-1973 TEST SET BATTERY AN AMM-1《AN AMM-1电池测试设置》.pdf
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1、MIL-T-22007A 66 7777706 0330589 Lt ,- MI L-T-Z2007A(AS) 28 November 1973 SU PERSE DING MIL- T- 2200 7(Aer) 6 April 1959 MILITARY SPECIFICATION TEST SET, BATTERY AN/AMM- 1 This specification has been approved by the Naval Air Systems Command, Department of the Navy. 1. SCOPE 1.1 Scope. The equipment
2、covered by ?his specification shall be capable of functioningas a d-c power source for Radiosonde Set AN/AMT-11( ), as a resistive load for activation of Battery BA-353/AM7 and as a current and voltage monitor of the d-c power required for operation of Radiosonde Set AN/AMT-11( ). 1.2 Classification
3、. - The Test Set, Battery AN/AMM-1 shall be of one type and shall consist of the following: Maximum Maximum Allowable Allowable 5Pe Size (Inches) Weight Applicable Unit Designation w H/D L (Pounds) Paragraph Test Set, - Battery TS-llOl/AM 9 7-1/2 12 19 3.5 Cable, Power W-1 48 O. 5 3.5 Cable, Radioso
4、nde W-2 2. APPLICABLE DOCUMENTS 39 O. 5 3.5 2.1 The following documents, of the issue in effect on date of invi- tation for bids or request for proposal, form a part of the specification to the ex- tent specified herein. /- Provided by IHSNot for ResaleNo reproduction or networking permitted without
5、 license from IHS-,-,-MIL-T-22007A(AS) SPECIFICATIONS Military MIL-E-17555 MIL-T-18303 MIL-S-I 95 O0 MIL-T-21200 STANDARDS I- Military MIL-STD-105 MIL-STD-130 MIL-STD-454 ! MIL-T-22007A bb II 7979706 0130570 O Electronic and Electrical Equipment, Accessories, and Repair Parts, Packaging and Packing
6、of Test Procedures, Preproduction, Acceptance, and Life, for Aircraft Electronic Equipment, Format for Semiconductor Devices, General Specification for Test Equipment for Use with Electronic and Fire Control Systems, General Specification for Sampling Procedures and Tables for Inspection by Attribut
7、es Identification Marking of U. S. Military Proper Standard General Requirements for Electronic Equipment DRAWINGS Naval Air Systems Command 57A119ASKl 5 7A119 D2 2 List of Drawings for Test Set, Battery, AN/AMM-l Panel Mounting Assembly (Copies of specifications, standards, drawings, and publicatio
8、ns required by suppliers in connection with specific procurement functions should be obtained from the procuring activity or as directed by the contracting officer.) 2.2 - Precedence. When the requirements of the contract, this specification, or applicable subsidiary specifications are in conflict,
9、the following precedence shall apply: (1) - Contract. The contract shall have precedence over any specification. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-Provided by IHSNot for ResaleNo reproduction or networking permitted without license from
10、 IHS-,-,- MIL-T-22007A bb m 7779706 0230572 Li - -_ request for approval shall be forwarded to the Naval Air Systems Command before the part is purchased or fabricated. in addition to or in lieu of the Nonstandard Part Data Sheet, the contractor shall submit an itemized List of the parts, their sour
11、ces, and the contractors draw- ing or purchase specification covering the parts. 3.2.2 Diode types. The choice and application of electron diodes used in the equipment shall be in accordance with the following requirements and in the sequence noted: (a) MIL-S-19500 (b) The use of any diode not meeti
12、ng the requirements of (a) above shall be approved by the Naval Air Systems Command; however, before consideration for approval, the contractor shall submit the following information: (1) Quantitative data on the electrical advantages and mechanical adequacy of the proposed diode over the equivalent
13、 type on the acceptable listings. (2) Test data and performance limits of the diode which must be maintained to ensure satisfactory and reliable performance in the equipment. (3) information as to whether the diode manufacturer has received Military or Navy qualification approval for the particular
14、diode. 3.2.2.1 Diode complement. A diode complement report shall be pre- pared and submitted to the Naval Air Systems Command for review and approval prior to first article testing. The diode complement shall include all diodes used in the equipment. 3.2.3 Performance objectives. Minimum size and we
15、ight, simplicity of operation, ease of maintenance, and an improvement in the performance and reliability of the specific functions beyond the requirements of this specification are objectives which shall be considered in the production of this equipment. Where it appears a substantial reduction in
16、size and weight or improvement in simplicity of design, performance, ease of maintenance or reliabilify will result from the use of materials, parts and processes other than those specified in MIL-T-21200, it is desired their use be investigated. When investigation shows advantages can be realized,
17、a request for approval shall be submitted to the Naval Air Systems Command for consideration. Each request shall be accompanied by complete supporting information. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-T-22007A bb 9999906 0330593 b m MI
18、L- T-2 20 O 7A(AS) Design and construction: 3.3 3.3.1 General. This equipment shall fulfill all applicable design and construction requirements of MIL-T-21200 unless otherwise specified herein. 3.3.2 Service conditions. The equipment shall operate satisfactorily under the service (environmental) con
19、ditions contained in 3.3.2.1 through 3.3.2.4. 3.3.2.1 Temperature. As specified in MIL-T-21200 for Class 2 equipment. 3.3.2.2 Humidity. As specified in MIL-T-21200 for Class 2 equipment. 3.3.2.3 Vibration. The equipment shall not suffer damage or fail to give specified performance when subjected to
20、the vibration test of 4.8.3. 3.3.2.4 Shock. As specified in MIL-T-21200 except that the impact shocks shall be log. 3.3.3 - Standard conditions. The following conditions shall be used as a basis to establish normal performance requirements and for making laboratory bench tests on the equipment. Temp
21、eratur e Altitude Normal ground Room ambient (30C t 10C) Vibration None Humidity Room ambient up to 90% relative humidity Input Power 115 V AC t5% 60 cycles O. 22 to O. 30 amperes 3.3.4 Total weight. The total weight of the equipment, including cables, shall be a minimum consistent with good design
22、and shall not exceed 20 pounds, 3.3.5 Operational stabi li$. The equipment shall operate with optimum performance for 200 hours, continuously or intermittently, without the necessity for readjustment of any of the controls which are not readily accessible on the front panel. Provided by IHSNot for R
23、esaleNo reproduction or networking permitted without license from IHS-,-,-3.3.6 Operating life. 3.3.6.1 Reliable operating life. The equipment shall have a reliable operating life of at least 200 hours without the necessity for bench servicing. Parts requiring servicing or replacement within this in
24、terval to renew this service life shall be specified by the manufacturer. 3.3.6.2 Total operating life. The equipment shall have a minimum total operating life of 10,000 hours with reasonable servicing and replacement of parts. Parts requiring replacement within this interval and the life of such pa
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