NAVY MIL-T-22143 A-1960 TELETYPEWRITER TT-264 AG《TT-264 AG电传打字电报机》.pdf
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1、M I L-T-2 2 I 4 3 A (WE P1 20MAY i960 MILITARY SPECIFICATION TELETYPEWRITER, TT-264/AG This specification has been approved by the Bureau of Naval Weapons, Department of the Navy, 1. SCOPE 1.1 Scope - The equipment covered by this specification is a transmitting and re- ceiving page printing telegra
2、ph set, which may be operated into, or out of, a converter for use over half duplex (simplex) or fuil duplex radio communication links between aircraft and properly equipped surface stations or other aircraft. 1.2 Classification - The Teletypewriter TT-264/AG shail be of one type and shall consist o
3、f the foilowing items: Apple Items Type Designation Para, 3.3.1 3.3. 2 Transmitting Keyboard (*I Receiving Page Printer (*I Connecting Chassis (including Internal line battery supply) (*) 3.3.3 case (*I Automatic Paper Winder . (*) Mounting (*) Airborne type carrying 3.3.4 3.3.5 3.3.4. 2 NOTE: (*) S
4、ee paragraph 6.2. the following equipments which are not to be supplied as part of this equipment. 1.3 Compatibility Requirement - The equipment shall be capable of operating with - unit Type Designation Radio Set AN/ARC-38 (Modified for FSK operation) Keyer, Frequency Shift KY- 3 O2/ARC- 3 8 Collin
5、s Radio Co. Model 706B-1 or an approved equivalent equipment Coilins Radio Co. Model 614C-4 or an approved equivalent equipment Control, FSK 2. DOCUMENTS 2.1 General - The following documents of the issue in effect on the date of invita- tion for bids form a part of this specification, to the extent
6、 specified herein: SPECIFICATIONS Militarv MIL-C-172 Cases; Bases, Mounting; and Mounts, Vibration (For, Use with Electronic Equipment in Aircraft 1 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-T-221434ONEP) MIL- E -4682 MIL-W- 5088 MIL-E- 540
7、0 MIL-T-5422 MIL-1-6181 MIL-P-7788 MIL- P- 17555 MIL-T-18303 MIL- N- 18307 Electron Tubes and Transistors, Choice and Application of Wiring; Aircraft, installation of Electronic Equipment, Aircraft, General Specification for Testing, Environmental Aircraft Electronic Equipment Interference Limits, T
8、ests and Design Requirements, Aircraft Electrical and Electronic Equipment Plate, Plastic, Cockpit and interior Controls Lighting Preparation for Delivery of Electronic Equipmen, Miscellaneous Electrical Equipment (Except Rotating Electrical Equipment) and Associated Repair Parts Test Procedures, Pr
9、eproduction and Inspection, For Aircraft Electronic Equipment, Format for Nomenclature and Nameplates for Airborne Electronic and Associated Equipment STANDARDS 2. 2 Military MS 25245 Connections, input Power Airborne Electronic Equipment; 28-Volt DC, 115-Volt Single-phase AC, or 115/200 Volt 3-Phas
10、e AC, or Combinations . MIL -STD - 704 Electric Power, Aircraft, Characteristics and Utilization of . Bureau of Naval Weapons SAR-300 Material Changes and Material Bulletins, Preparation of Availabilitv of Documents - (1) When requesting applicable documents give both the title and number. Copies of
11、 this specification and applicable documents may be obtained upon application to the Commanding Officer, Naval Supply Depot, (CDS), 5801 Tabor Avenue, Philadelphia 20, Pennsylvania. 3. REQUIREMENTS 3.1 Parts and Materials - in the selection of parts and materials, fulfillment of major design objecti
12、ves shall be the prime consideration. in so doing the following shall govern: (1) Parts and materials as approved by Specification MIL-E-5400 shall be given first consideration. (2) Nonrepairable subassemblies, as outlined in Specification MIL-E-5400, shall be used when practicable. The general size
13、 of the subassembly, and the amount of circuitry to be included therein shall be approved by the procuring activity. Nonrepairable subassemblies must be reliable, A mean-time-to failure of more than 5000 hours should be the goal of. each. 2 i Provided by IHSNot for ResaleNo reproduction or networkin
14、g permitted without license from IHS-,-,-MIL-T-22193A 58 7779706 0150832 T B .- e-. .* I MIL-T-22143A WEP) (3) When previously produced models of this equipment did not use non- repairable subassemblies, the design shall not be changed to employ non- repairable assemblies without the approval of the
15、 procuring activity. Nonstandard Parts and Material Approval - Approval for the use of non- Electron Devices - Transistors and diodes shall be chosen and applied, and 3. i. 1 standard parts and materials shall be obtained as outlined in Specification MIL-E-5400, the complements reported as outlined
16、in Specification MIL-E-4682. The complement report must be submitted to the procuring activity for review and approval prior to preproduction testing. No electron tubes shall be used. 3.1.2 3.2 Design and Construction - 3.2.1 General - This equipment shall fulfill all applicable design and construct
17、ion requirements of SpecificatioMIL-E-5400 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 conditions as specified in Specification MIL-E-5400 for Cl
18、ass 1 equipment. tablish normal performance requirements and for making laboratory bench tests. Temperature Altitude Normal ground Vibration None Humidity input power voltage Total Weight - The total weight of the equipment, excluding a full size stand- 3.2.2 3.2.3 . Standard Conditions - The follow
19、ing conditions shall be used as a basis to es- Room ambient (30C f 10OC) Room ambient up to 90% relative humidity 115 f 1. O V AC 3.2.4 ard paper roll and external cables, shall be a minimum consistent with good design and shall not exceed 30 pounds. Operational Stability - The equipment shall opera
20、te with optimum performance for 100 hours, continuously or intermittently, without the necessity for readjustment of any controls which are inaccessible during flight, 3.2.5 3.2-6 Operating Life - 3.2.6.1 Reliable Operating Life - The equipment shall have a reliable operating life of at least 250 ho
21、urs without removal for bench servicing. Parts requiring servicing or replacement at the end of this interval to renew this service life shall be specified by the manufacturer. 3.2.6.2 Total Operating Life - The equipment shall have a minimum total operating life of 2,000 hours with reasonable servi
22、cing and replacement of parts. Parts requiring replace- ment within this interval and the life of such parts shall be specified by the manufacturer. 3.2.7 eration using external wiring in accordance with the applicable requirements of Specification MIL-W-5088. The external wiring shall be unshielded
23、, except that a minimum number of the in- dividual wires may be shielded when demonstrated as necessary to meet interference control re- quirements and provided the assembly of the cable to its plugs may be easily accomplished. Cables and Connectors - The equipment shall provide for the use of cable
24、s and connectors in accordance with Specification MIL-E-5400. However, cables and that portion of the connectors which is to be attached to the cables shall not be supplied as part of the equipment. An appropriate power cord six feet long shall be provided. Interconnection Cabling - This equipment s
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