1、MIL-T-23369B( AS) . . 2 Januarv 19 6 Supers eamg MIL-T-23369A(WEP) 8 March- 1965. MILiTARY SPECIFICATION TRANSMITTER GROUP, TERIC DATA OA-I( )/DPN This Specification has been approved by the Naval Air Systems Command, Department of the Navy 1. SCOPE 1.1 SCOPE - This specification covers the requirem
2、ent for the OA-U08( )/DPN Transmitter Group, Telemetric Data suitable for installation in the AIM-7D, and AIM-7E uided missiles (SPARROW) for use in conjunction with a telemetry system. The OA-12087 )/DPN provides a reliable crystal controlled, single channel, fre- quency modulated telemetering sign
3、al for flight testing of the AIM-V, and AIM-7E missiles. and fuzing signals vary the frequency of the radio frequency oscillator, or a sub- carrier thereon. The electrical variations produced by the missile video, cpeedgate sweep, 1.2 and consists of the following: CLASSIFICATION - The equipment cov
4、ered by this specification is of one type collectively designated as Transmitter Group, Telemetric Data OA-1208( )/DPN, MAJOR UNIT DESIGNATI ON MAX. SIZE MAX WEIGHT APPL, PARA. VHF Transmitter Unit 1 Dual Input Voltage Unit 2 Controlled Oscillator and Mixing Circuit Antenna Kit Unit 3 1.63“ x 2.87“
5、1.1 lb. 3.4.1 x 4.58“ 7.0“ x 5.0“ 1.0 lb. 3.4.2 x 4.0“ 1.0 lb. 3.4.3 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-T-23369B( AS) 1.3 ACCESSORIES .- ! specified herein, GOVERNMENT FRNISHED DOCMENTS - The following documents of the issue in effec
6、t on the date of invitation for bids or request for proposal, SPECiFICATIONS FEDERAL Federal Test Method STD NO, 151 MIUTARY MIL-w-5088 MIL-E-5 400 MIE3347555 MIL-N- 18307 SW MILITARY MIL-STD-202 MSL-STD-210 2 Metals; Test Methods Wiring, Aircraft Installation of Electronic Equipment, Aircraft; Gene
7、ral Specifications for General Specification for Electronic and Electrical Equipment and Associated Repair Parts; Pre- paration for Delivery of Nomenclature and Nameplates for Air- borne Electronic and Associated Equipment Reliability index Determination for Avionics Equipment Models; General Specif
8、ication for Teat Methods for Electronic and Electric Camponents Parts Climatic Extremes for Military Equipment Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-T-2336qB.(PSs) -,- .,: - ,*.-!: MIL-STD-454 Requirment No. 29 General Requirepent .fior
9、-; -.:. ; .k MIL-STD-461 Electromagnetic Inter-ferenc-e- I ._. =. e Elecprbriic. Equipment; , - - *. . - -L :-.;= i - . 0 :;. : . s . - . f( . I -* . .- Charsct erist ics, Requirements .- - for Equipment .-. c.- tc . :. 1. -I -5 * L .I i MIL-sTD-: 1, - Reliability Te.s -. Distribution . I . . d- MIL
10、-STD-794 Parts and Equipment; Procedwe MIL-STD-810 Military Standsrci Enviramental for Packaging of Test Methods for Aerospace ad Ground Equipment BULLETINS ANA-445- and Supp. No. 1 Engineering Changes to Fieapons Systems, Equipment and Facilities WBLICATIONS DEPARTMENT OF DEFENSE . Telemetry Standa
11、rds Revised March 1966 (IRIG No. 106-66) DRAWINGS Oklahoma Aerotronics Inc. DL loi2134 . VHj? Transmitter DL 1012252 DL lOl2351 DL loi2354 Transmitter Group, Telemetric Data OA-1208( )/DPN Fuze and Missile Speedgate Sweep Indicator plus FPU Frequency Monitor Antenna Kits including One Each of Couple
12、rs 5028C-5016 and 5028C- 5022 3 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-_ _ _ MIL-T-233bB 58 997990b 0352334 3 a MIL-T-23369B( AS) 22 AVAILABILITY OF SPECIFICATIONS, PUBLICATIONS AM) DRAWINGS - i (1) When requesting specifications publication
13、s and rawings refer to both title and number. Government inspector. Copies of applicable specifications, and publications may be obtained upon application to the Commanding Officer, Naval Aviation Supply Depot (Code log), 5801 Tabor Avenue, Philadelphia, Pennsylvania 19120. Copies of the Oklahoma Ae
14、rotronics, Inc. drawings may be obtained from the Inspector of Naval Material, Torrance, California 90509. AU. requests should; be made via the cognizant (2) (3) 2.3 PRECEDENCE - When the requirements of the contract, this specification, or shall apply: other applicable specifications are in conflic
15、t, the following precedence (1) (2) Contract - The contract shall have precedence over any specification. This Specification - “his specification shall have precedence over all applicable subsidiary specifications. Any deviation from this specifi- cation or from subsidiary specifications where appli
16、cable, shall be specifically approved in writing by the aval Air Systems Command Head- quarters * (3) The drawings listed in this specification. (4) Referenced Specification - Any specification referenced herein or on the drawings listed in this specification shall have precedence over all applicabl
17、e subsidiary specifications referenced herein . referenced specifications shall apply to the extent specified. A11 and procedures proposed for the production. in Section 4 herein and is for the purpose of determining that, prior to starting production, the contractors production methods are capable
18、of yielding items that comply with the technical requirements of the contract. shall be delivered prior to approval of the preproduction model. Prefabrication of production equipment, prior to such approval, is at the contractors own risk. The preproduction model shall not; be considered as one of t
19、he equipments under the con- tract; however, it may be reworked by the contractor and submitted for acceptance as a production equipment I The sample will be tested as specified Bo production equipaent 3.2 Aerotron3cs Inc. Drawing DL 1012252 except insofar as errors of omission TRANSMImER GROUP - !C
20、he Transmitter Group, Telemetric Data OA-l208( )/DPN shall be mandaTtured in accordance with Oklahana Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-or commission in the technical documentation may be incompatitile.with . - -2 the requirements of th
21、is specification. in any case a condition of final acceptance is that the transmitter -group must meet all the re- quirements of this specif icatin. .= ._ 3.2.1 PARTS AND MATERLALS - Since the entire assembly is built to be . expended, the assembly.shal1 be constructed and the quality of the individ
22、ual parts .shall be such that the unit as-a whole will meet material , electrical i and environmental requirements. L . 3.2.2 CHOICE OF TUBE TYPES - Electronic tubes used in this equipment for electronic equipment. 3.2.3 CONFIGURATION -This equipment shall be of sub-miniaturized con- compatible with
23、 power, mounting, and antenna features provided in the AIM-7D and AIM-7E missiles. shall be chosen from Requirement Z? of MIL-STD-454, General Requirement struction and packaged so as to complement the space, and be 3.2.4 DATA - No data is required by this specification or applicable or order - see
24、6.3. ,. documents referenced in Section 2 unless specified in the contract 3.3 GENERAZ, DESIGN REQU1REMENT.S 3.3.1 Revised March 1966 (IRIG Document 106-66) .Il 3.3.2 GENERAL - This equipment shall be in accordance with this specifi- cation, Specification MIL-E-8189 and the “Telemetry Standards STAN
25、DARD CONDITIONS - The following conditions shall be used for making individual tests on the equipment: Tempera ture Al ti tude Normal Ground Vibra tion None Humidity Room Ambient up to 90% relative humidity Input Power As per paragraph 3.3.9 Room Ambient 3OoC - + 10C 3.3.3 SERVICE CONDITIONS - The e
26、quipment shall operate satisfactorily under any of the following service conditions or natural combi- nations of service conditions, 3.3.3.1 TEMPERATURE - The equipment shall be capable of satisfactory operation when operating at an ambient temperature range from -40F to +160F with an initial 10 min
27、ute soak period at -400F. the equipment shall operate satisfactorily after a 10 minute soak at +160F, except that the power output may drop to not less than 0.4 watts when operated at the upper temperature limit. Likewise, 5 . Provided by IHSNot for ResaleNo reproduction or networking permitted with
28、out license from IHS-,-,-MIL-T-E!33b9B 58 979730b 01521Lb 5 W MIL-T-23369B( AS ) 3-,3,3,2 ALTITUDE The equipment shall be capable of satisfactory operation from sea level to 90,ooO feet of altitude (31.3 to 0,502 inches of mercury), with a soak period for 10 minutes at 90,000 feet, 3,3.3.3 temperatu
29、res up to 125QF for a soak period of one hour. HUMIDITY - The equipment shall be capable of satisfactory - operation under relative humidity conditions up to loo“/, at 3.3.3.4 axis separately in accordance with MIL-STD-810 Mounting A, Test Curves 3C and 4C, Time Duration of 10 minutes, Omitting Reso
30、nance Dwell, VIBRATION - The equipment shall operate satisfactorily under vibration applied along longitudinal, vertical, and horizontal Equipment Class 3, 3.3.3.5 50 gis peak acceleration with a load application rate of 35 gis per milli- second and time duration of not less than 5 milliseconds appl
31、ied along the longitudinal, vertical, and horizontal axis separately. 3.3.3.6 ACCELERATION - The equipment shall be capable of satisfactory operation during and after peak longitudinal acceleration of 40g applied for a minimum of 1 minute; peak longitudinal deceleration of 15g applied for a minimum
32、of 1 minute; and a peak transverse acceler- ation (any direction normal to that line corresponding to longitudinal axis) of 25g applied for a minimum of 1 minute, SHOCK - The equipment: shall be capable of satisfactory operation without damage or maladjustment resulting from impact shock of under an
33、y natural combination of condi lions specif ied in the preceding service conditions for a maximum duration of 12 minutes. 3.3.4 of this equipment, and shall be mounted in the Flight Control Group of AM-7D or AIM-7E missiles by means of provisions included therein, weight of the equipment shall not e
34、xceed 3.1 pounds, FORM FACTOR AND WEIGHT - The form factor of this equipment shall be as follows: The telemetering group shall consist of all units The 3.3.5 OPERATIONAL STABILITY - Paragraph 3.3 . 2 and maintain the characteristics as specified in Paragraphs 3.4.1.4 and 3.4.2.3 for five hours, cont
35、inuously or inter- mittently, without necessity for readjustment of any controls, A *warm- up“ time shall be allowed in each case prior to use of the system in order that the circuits may reach stable operation. shall be as short as possible and shall not exceed a maximum of one-quartt The *warm-up*
36、 time hour , I 6 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-T-23369B( AS) 3.3.5.2 All-*tuning and-operating controls of the equipment shall be operating OF non-operting the setting or position of any control -shall not be altered by any of t
37、he specified service conditions, -such that 6when ehe equipment is properly installed and either 3.3.6 OPERATING AND NON-OPERATING LIFE - The equipment shall have a Navy. individual conditions of packaged storage, ready storage, inf light readi- ness, captive flight, and free flight, 3.3.6.1 NON-OPE
38、RATING LIFE - The equipment shall have a minimum non- ject to the provisions of 3.3.6 above. The24 months may include periods of packaged storage under the conditions of 3.3.3, and periods of unpack- aged s torage or -installed in the missile under depot or shipboard conditions. The equipment shall
39、meet the requirements of MIL- STD- 210 with respect to temperature extremes and duration except lower temperature extreme shall be -65OF. . 3.3.6.2 Navy acceptance. 50 hours of operation-under conditions of 3.3.3. minimum-total life of-24 months, from date of acceptance by the The 24 month period ma
40、y include varying periods of life under the operating life of 24 months from date of Navy acceptance, sub- OPERATING LIFE - The equipment shall be capable of operating anytime during the 24 month period beginning from the date of The 24 month period shall provide a total of at least 3.37 INTERCONNEC
41、TION CABLES - The equipment shall be capable of satis- factory operation using the cables provided as part of the missile and this equipment. The equipment shall operate satisfactorily when used in conjunction with aircraft wiring which has been installed in accord- ance with Specification MIL-W-508
42、8. 3.3.8 CABLES AND CONNECTORS - The cables and connectors included herein shall facilitate interconnection with the AIM-7D and AIM-7E missile cable in the most efficient manner possible, consistent with the missile design. Special miniature multi-pin connectors may be used to f aci 1 i ta te input
43、and output power connes tions . 3.3.9 INPUT POWER REQUIREMENTS - The equipment shall operate satis- power in excess of the amount indicated: factorily from the following power sources and shall not require D.C. Source Nominal Vol tage B+ +255 VDC at 55 ma +25 VDC +25 VDC at 600 ma fil ament D.C. VOL
44、TAGE LIMITS - The voltage limits for B+ shall be 255 + 5 VDC; however, the equipment shall not be damaged by voltages 3.3:g.l Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-T-233bB 58 a 0b 0352338 7 a as high as 285 VnC. a filament: supply of 24
45、 to 26 VDC, The equipment shall operate satisfactorily with 3.3.9.2 GROUND INPUT - The equipment shall be such that the negative of the primary DC power source may be grounded externally. 3.3.10 OVERLOAD PROTECTION - Overload protection for the equipment need not be provided in the equipment. 3.3.11
46、 resume normal operation when the vol tage returns within the limits of 3.3.9 above. 3.3.12 MOISTURE AND FUNGUS RESISTANT TREATMENT - Moisture and fungus UNDER VOLTAGE PROTECTION - The equipment shall not be damaged by vol tages below the minimum specified and shalL automatically resistant treatment
47、 is not required for this equipment. 3.3.13 NAMEPLATES AND NOMENCLATURE - Application for nomenclature and marking of equipment for identification shall be in accordance with Specification MIL-N-18307. 3,3,14 the subassembly level, 3.3.15 PROVISIONS FOR MAINTENANCE AND FIELD TESTING - Provisions for
48、 Specification MIL-E-8189 as far as possible, consistent with the nature of this equipment, transmitter, Unit 1 or the 3.9 Kc modulator, Unit 2. INTERCHANGEABILITY - The equipment shall be designed to meet the interchangeability requirements of Specification MIL-E-8189 to maintenance and field testi
49、ng shall meet the requirements of No field maintenance shall be performed on the VHF 3.3.16 bility to interference within the limits specified in MIL-STD-461. interference shall conform with specifications set forth in LRIG Document 106-66 when operated in any service or load conditions specified herein. INTERFERENCE - Every effort shall be made, Consistent with its size and function, to m
