1、MILITARY SPEC1 FI CAT ION TEST SET, MISSILE INTERFACE (PIITS) TS-3561-( ) /AFIM-23 (V) This specification has been approved by the Naval Air Systems Command, Department of the Navy TABLE OF CONTENTS Title - Page 1 1 1 1 1 1 6 6 7 7 9 14 14 24 24 29 29 29 31 32 32 32 32 34 34 34 34 Provided by IHSNot
2、 for ResaleNo reproduction or networking permitted without license from IHS-,-,-MLL-T-85037 Li7 W 7777906 0257573 T TABLE OF CONTENTS (Continued) Paragraph 6. 6.1 6.2 6.3 6.4 6.5 6.6 6.7 6.8 Intended use. Ordering data Definitions Nomenclature cross-reference Liquid cooler Use of this specification
3、Abbreviations and acronyms Convenience outlet power Table I II 11.1 IV V - VI LIST OF TABLES Title VERIFIED SIGNALS MITS OUTPUTS INTRASTATION SHORTS TEST INTERSTATION SHORTS TEST ACCEPTANCE TEST PLAN FOR MISSILE INTERFACE TEST SET ACCEPTANCE ACTIVITIES SUPPLEMENT. P;IIL-T-85039(AS) Military Specific
4、ation, Test Set. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-NIL-T-85037 47 = 7777706 0257574 1 - MIL -T -85039 (AS) MILITARY SPECIFICATION TEST SET, MISSILE INTERFACE (MITS) TS-3561( ) /AWM-23 (V) This specification has been approved by the Nava
5、l Air Systems Command, Department of the Navy 1. SCOPE 1.2 Classification. The MITS shall consist of the following asCemLbies: a. Assembly, Test Set (see 3.6.1) b. Assembly, Eject Cable (see 3.6.2) C. Assembly, Identifi- (see 3.6.3) cation/Test Access 1.3 Associated equipment. The MITS shall be capa
6、ble of operating with th e cable assembly set of MIL-C-81954(AS). 2. APPLICABLE DOCUMENTS 2.1 General. The following documents, of the issue specified in AS-m3, Applicable Document List for AWCS Test Set AN/AWM-23 (VI , form a part of this specification to the extent specified herein. MIL-T-81734(AS
7、) shall be the applicable general specification for the MITS described herein (see 6.6). SPECIFICATIONS Military MIL-M-7 7 9 3 MIL-C-13777 - - c_ Meter, Time Totalizing Cable , Special Purpose , Electrical, General Spec if i cat ion for 1 Provided by IHSNot for ResaleNo reproduction or networking pe
8、rmitted without license from IHS-,-,-. MIL-T-85039 47 MIL-T -85039 (AS) W 977970b 0257575 3 W MIL-E-17555 MIL-T-1830 3 MI L-N- 1 8 3 O 7 MIL-T-21200 MIL-S-46844 MIL-W-81044 MIL-T-817 3 4 (AS) MIL-C- 8 19 5 4 (AS) Electronic and Electrical Equipment, Accessories,- and Repair Parts; Packaging and Pack
9、ing of Test Procedures, Preproduction, Acceptance, and Life for Aircraft Electronic Equipment, Format for Nomenclature and Identification for Electronic, Aeronautical and Aeronautical Support Equipment including Ground Support Equipment Test Equipment. fr Use with Electronic and Fire Control Systems
10、, General Specification for Solder Bath Soldering of Printed Wiring Assemblies, Automatic Machine Type Wire, Electric, CEosslinked, Polyalkene Insulated, Copper Test Set, Airborne Weapon Control System, AN/AWM-23(V) Cable Assembly Set, Electrical, MATS, Special Purpose Test Set, Missile Interface (M
11、ITS) Supplement. 1 (Confidential) Naval Air Svstems Command (NAVAIR) AS-2695 Interface Specification, F-14A Weapon Control System AN/AWG- (N-3) Interface with the AIM-54A-1 Missile AS-2696 Interface Specification, AIM-54A-1 Guided Missile (Production) Installation and Physical Interface with F-14A A
12、ircraft 2 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-PUBLICATIONS Hughe.s Aircraft Company 3326964 Acceptance Test Procedure, Missile Interface Test Set Tape 481OCP-1XX Computer Program NDRO/Bulk Store DWG 493507-1XX Test Set, Missile Interface
13、DWG T493507-11-1 MITS Test Position DWG 493513-1XX Cable Assembly, MATS HMS 2-1132 Matepial Specification, Wire (Bus), Solid Copper Conductor, General Purpose (200 “C Service) HMS 2-1144 Material Specification, Wire, Electrical, Polytetrafluorethylene Insulated, Hookup and General Purpose (for 392F
14、service) HMS 2-1377 HMS 2-1480 HMS 2-1513 HMS 2-1514 HMS 2-1551 Material Specification, Cable-Multicanductor, Hook-up and General Purpose (for 392F service) Material Specification, Wire and Cable, Multiconductor, Hook-up, Fluorocarbon-TFE Insulated, 600 volts RMS (275F service) Material Specificatio
15、n, Wire and Cable, Cabling and Harnessing Usage, Polyalkene Insulated, 600 volts RMS (275F servi ce ) Material Specification, Wire and Cable, Cabling and Harnessing Usage, Polyalkene Insulated, 100 volts RMS (275F service) Material Specification, Wire, Electrical Polyvinylidene, Flouride Insulated 3
16、 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-T-85039 q 7999906 0257577 7 -: MIL-T -85039 (AS) IIMS 2-1563 EIMS 2-1619 HMS 22-1672 FS 31050-038 GS 30620-781 DP 30847-008 DP 31050-918 DP 31050-919 DP 50062 HP 11-39 EIP 31-17 HP 31-23 Material S
17、pecification, Wire, Electrical Polytetrafluorethylene Insulated, 600 and 1000 volts rms (for 392F service) Material Specification, Wire and Cable, Electrical, Polyimide-Fluorocarbon Insulated (for 392“ F service) Material Specification, Gold-Silicon Solder Alloy Finish Specification, AN/AWM-23 Groun
18、d Support Equipment General Specification for Identification and Marking of AN/AWM-23 Ground Support Equipment Detail Process Specification, Engineering Modification of Printed Circuit Boards Detail Process Specification, REMCAM Fabrication Procedure Detail Process Specification, Assembly of Repaira
19、ble Multilayer Circuit Strips (REMCAM) Detail Process Specification, Modification of REMCAM Circuit Boards Hughes Process, Welding, Resistance for the Assembly of Electronic Modules Hughes Process, Printed Circuit. Board, Lead-Tin Plated, Projecting Contact Pin Type, Production of Hughes Process, Pr
20、inted Wiring Board, Requirements for 4 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-T -85039 (AS) Microelectronic Devices Used in Avionics Equipment, Procedures for Selection and Approval of List of Standard Drawings used by the NAVAL AIR Syst
21、ems Command List of Specifications and Standards (Book Form) Approved by the Naval Air Systems Command Electromagnetic (Radiation) Environment Considerations for Elect $9 rl +I II 1 O +I a* +I +I m O O om O0 In 17 Provided by IHSNot for ResaleNo reproduction or networking permitted without license f
22、rom IHS-,-,-MIL-T-85037 47.- 7777906 0257573 3 = mL-T-85039(As) a, k 3 c, id I-l u G a, z Q I I I I I 1 I I I I s . rl in O O m Co 03 A h A . ul * . M -r A A w Y I I I 2 a, E-i a, a, +J Id p: 18 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-T-8
23、5039 (AS) Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-T-5037 LI7 m 777770b 0257593 5 m MIL-T-85039 (AS) n a a, 5 E: F: O u v H 3 c1 Id k 9 U 2 a d Id rn Id PI B ul m A . 3 Y IB Id .A ma, lm mrl a, Fi Id a B a, Fi Id a B al rd 5 JJ 20 Provided
24、 by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-T-85039 (AS) !h . i? 4 rd LI 3 u a d m II Id bi 3 a, k 3 rl u I= a, z -td o - h h N N X X * N N U *- do ow III m m +I +I I II . . I II o cri +I +I a a u II g c1 O ci Na Xe3 xm w* O ci ;9 Ui we x I I .FI v1
25、Ei H c rn a a, LI LI -rl -rl 4p9 Fr Fr c, u a- m w ci u ai -n w ci u a, -n w 21 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-T-85037 97 .7777706 0257575 7 MIL -T -85039 (AS) I II a c a til I I (v rl v . II 4, a, !-I 3 ci a rl u 8 l3 2 k c k 3
26、ci 2 en sing 4ctive Frequency ED Prelaunch Phase Lock Ind. (MOAT) Detection Signai (MOAT) ro MOAT output ( MOAT ) Az Steering Signal Vsh El Steering Signal V sg MOAT MOAT VCLO Control Voltage (MOAT) MOAT Flipper Output (MOAT) AP MOAT Command O u tpu t ( MOAT Front Receiver C Monitor (MOAT) XMTR PA O
27、utput (MOAT 1 MIL-T-85039 IAS/) I- ._ -y- /- TABLE II MITS OUTPUTS ominal 2.0 VDC 8.0 VDC ,3.0 VDC 2.0 VDC 5.0 VDC 5.0 VDC 2.0 VDC 3.0 VDC 4.0 VDC 5.0 VDC 1.0 VDC 5.0 VDC -5.0 VD( 4ccuracy C5% (0.60 VDC) 512% (1.0 VDC 520% (0.6 VDC +lo% (1.2 VDC 520% (1.0 VDC) +20% (1.0 VDC) +20% (0.4 VDC) f20% (0.6
28、 VDC) +20% (0.8 VDC) Remarks MITS ID Signai IDTA ID Signai 520% (1.0 VDC) +20% (0.2 VDC +lo% (0.5 VDC +25% (1.25 VDC Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-T-5039 LI9 I 997990b 0257579 b I MIL-T- 85039(AS) I tem 1 2 3 4 5 6 7 8 9 10 11 1
29、2 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 32 33 -_ TABLE III INTRASTATION SHORTS TEST Umbilical Pin 190 192 168 149 128 102 117 ,135 118 136 175 64 101 83 3 2 85 65 84 .152 151 150 6 97 112 129 1 58 185 115 18 137 1 O0 Signal Name ACM Active Launch Single Target Track Enable Semi-Ac
30、tive Channel Select C Semi-Active Channel Select B Semi-Active Channel Select A Programmed Phase g-Bias B3 Programmed Phase g-Bias B2 Programmed Phase g-Bias Bl h-Bias H2 h-Bias H3 Tail Attack Gr Semiactive Set High Altitude h-Bias H1 Act. Trans. Bias Set B Act. Trans. Bias Set A Spare Spare Spare P
31、relaunch Address C-1 Prelaunch Address B-1 Prelaunch Address A-1 Doppler g-bias Prelaunch Message C Prelaunch Message B Prelaunch Message A 8/4-Second Signal (MOAT) Transmitter RF ON Command (MOAT) Center Channel Target Simulator (MOAT) Parameter Re set External Slaving Command Timer Zero Set Prelau
32、nch Velocity Servo Enable 26 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-Item 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 - MIL-T-85037 LI7 W 7777906 0257600 7 W _ MIL-T-85039 (AS) TABLE IV INTERSTATION SHORTS TEST Umbilical 162 16 1 13 159 158 173 36
33、 25 1 o9 77 147 74 55 201 Eject A Eject B Signal Name El Vrg Program Test (NAT) Pitch Initial Condition Adaptive Roll Initial Condition RIG Driver Test (MOAT) Roll IC ISM Unlock Battery Activate ISM Relock J SHP K ,SHP I ,SHP Launch Power A Launch Power B Target Doppler Reference Frequency Eject Sig
34、nal A Eject. Signal B 27 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-T-5037 L17 m 7977706 0257601 O W MIL-T-85039 (AS) 3.6.2 Eject cable assembly. The eject cable assembly shall provide the electrical interface between the eject cartridge con
35、nector and the TSA 3.6.3 IDTA assembly. The IDTA assembly when used with the TSA e3ect cable assembly shall provide the additional missile ID required t perform the interstation shorts test (Table IV), and a dynamic load test for the missile 100 Vdc power. The IDTA shall also provide test access to the missile interface connector pins. shall provide fault indication for dynamic load test of the missile 100 Vdc power. The IDTA 28 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-
