1、MIL-G-8523L 14 = 7797706 0434025 T I MIL-G-85 23 1 (AS) i. - + 30 .October 1984 Beneficial comnents (reconmendations , additions, deletions) and any pertinent data wnich may be of use in improving this document should be addressed to: Comnanding Officer, Naval Air Engineering Center, Engineering Spe
2、cifications .and Standards Department (ESSD) Code 93, Lakehurst, NJ 08733, by using the self-addressed Standardization Document Improvement Proposal (DD Form 1426) appearing at the end f- this document or by letter. -_ MILITARY SPECIFICATION GUIDED WEAPON CONTROL GROUP OK-Z93A/AWW This specification
3、 is approved for use by the Naval Air Systems Comnand, Department of the Navy and is available for use by all departments and agencies of the Department of Defense. 1. SCOPE 1.1 Scope. This specification establ ishes the design, performance, and acceptancE?$i rements for the OK-293A/AWW Control Grou
4、p, Guided Weapon, herein after referred to as the control group. The control group consists of Control , Guided Weapon C-9743A/AWW (Joystick) and Converter, Control Signal s C-3248A/AWW (Electronic Package). The control group is to be located in the aircraft and is to interface with the Guided Weapo
5、n Control-Monitor Sets AN/AWW-7B, or AN/AWW-9 (Pod) to provide post-launch cockpit control for retargeting and steering of the WALLEYE Data Link Guided Weapon. The control group al so provides proportional dc vol tage inputs to the AN/ASN-91 computer. 1.2 Associated equipment. The control group oper
6、ates with the associated equipment listed in 6.4. 2. APPLICABLE DOCUMENTS 2.1 Government documents. 2.1.1 Specifications, standards, and handbooks. Unless otherwise specified, the following specifications, and standards of the issue listed in that issue of Department of Defense Index of Specificatio
7、ns and Standards (DoDISS) specified in the solicitation form a part of this specification to the extent specified herein. _. FSC 1430 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-SPEC IF ICATIONS FEDERAL PPP-T-60 PPP-T-76 PPP -B -585 PPP-B-601 PPP
8、-B-621 PPP-B-636 QQ-S-78 1 M I L ITARY MIL-P-116 MIL -E -5400 MIL-T-5422 MIL -T-18303 MIL -N - 18307 M IL-H-46855 STANDARDS MIL ITARY MIL-STD-129 M IL -STD - 147 MIL-STD-454 MIL-G-5231 14 999770b 043402b 1 I 1 C MI L-G-85 23 1 ( AS ) Tape, Packaging , Waterproof Tape, Pressure Sensitive Adhesive Pap
9、er (For Carton Seal ing) Boxes , Wood, Wi rebound Boxes, Wood, C1 eated-Plywood Boxes, Wood, Nailed and Lock-Corner Boxes, Fi berboard Strapping, Steel, and Seals Preservation-Packaging, Methods of Electronic Equipment, Aerospace, General Specification for Testing, Environmental , Aircraft El ectron
10、ic Equipment Test Procedures; Preproduction, Acceptance and Life, for Aircraft Electronic Equipment, Format For Nomenclature and Identification for Electronic, Aeronautical , and Aeronautical Support Equipment Including Support Equipment Human Engineering Requirements for Military System Equipment a
11、nd Faci 1 i ties Marking for Shipment and Storage Palletized Unit Loads (40 x 48“ 4 Way Partial and 4 Way Pallets) Standard. General Requirements for El ectronbc Equipment Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-G-5231 14 W 777770b 043402
12、7 3 I MIL-G-85231 (AS) MIL-STD-461 P M IL -STD-462 MIL-STD-704 MIL-STD-781 MIL-STD-965 MIL-STD- 1188 MI L-STD-1472 Electromagnetic Emission and Susceptibility Requirements for the Control of Electromagnetic Interference El ectromagnetic Interference Characteristics Measurement of Electric Power, Air
13、craft Characteristics and Utilization of Re1 iabil ity Tests, Exponential Distribution Parts Control Program Comercial Packaging of Suppl ies and Equipment Human Engineering Design Criteria for Military Systems Equipment and Faci 1 i ti es 2.1.2 Other Government documents, drawings, and publ ication
14、s. The following other Government documents, drawings, and publications form a part of this specification to the extent specified herein. PUBLICATIONS Naval Air Systems Command NAVA1 R 16-350K293- 1 Guided Weapon Control Group OK-293A/AWW DRAW I NG Naval Air Systems Comand DL 475AS150 Data List for
15、Guided Weapon Control Group OK - 293A/AW W (Copies of specifications, standards, handbooks, drawings and publ ications required by manufacturers in connections with specific acquisition functions should be obtained from the contracting activity or as directed by the contracting officer. 1 2.1.3 Orde
16、r of precedence. of this specification and the references cited herein, the text of this specification shall take precedence. 3. REQUIREMENTS article inspection (see 4.4 and 6.3). In the event of a conflict between the text 3.1 First article. When specified, a sample shall be subjected to first 3 Pr
17、ovided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-G-85231 19 m 777790b 0939028 5 II MIL-G-85 23 1 (AS) t . 3.2 Parts and materials. 3.2.1 Nonstandard parts and material approval Approval for the use of nonstandard parts and materials shall be obtaine
18、d by the contractor as specified in MIL-E-5400. 3.2.2 Basic conformance. Parts and materials selected for use in the equipment shall be in accordance with MIL-E-5400. Parts shall be selected from those conforming to MIL-STD-965, unless the parts selected will not perform as required in the intended
19、applications and environments specified herein in which case 3.2.1 shall be used to select and obtain approval for nonstandard parts. 3.2.3 Interchangeabil ity. The control group shall meet the interchange- ability requirements of MIL -t-5400. Drawing DL 475AS150 shall be the standard for measuring
20、interchangeabil ity of all app1,icable units, assembl ies, subassemblies, and parts. accordance with DL 4/SASlSO except insofar as errors of omission or comnission on the drawings may be incompatible with the requirements of this specifica- tion. group manufactured meet all the performance requireme
21、nts of this speci fi Ca ti on. 3.3 Design and construction. The control group shall be manufactured in In any case it is a condition of final acceptance that the control 3.3.1 Dimensions. The dimensions of the control group shall be not greater than specified in table I, 3.3.2 Total Wei ht. Total we
22、ight of control group shall be not greater than 3.18 poun +kilograms). s 3.3.3 Re1 iability. 3.3.3.1. Operational stability. The control group shall meet the performance requirements of thi s specification when operated continuously or intermittently for a period of at least one MTBF (752 hours) wit
23、hout the necessity for readjustment of any controls which are inaccessible to the operator during normal use. 1 ife of 5,000 hours with mfnimum servicing and replacement of parts. group shall have a minimum of iS2 h ours of mean (operating) time between failures when tested and accepted as specified
24、 in 4.5.3. 3.3.3.2 Operating life. The control group shall have a.tota1 operating 3.3.3.3 Re1 iabil ity in Mean-Time-Between-Failure (MTBF) . The control 3.3.4 Maintainability. Maintainability provisions shall be incorporated within the design to provide for service, access and repair of all assembl
25、ies. Normal routine testing of the control group shall be accomplished using Government furnished Distribution Box J-3416A/AW (see 3.6) and the standard test equipment normally avail able in intermediate maintenance shops. 4 Provided by IHSNot for ResaleNo reproduction or networking permitted withou
26、t license from IHS-,-,-MIL-G-5231 14 7777906 0363787 W MIL-G-85231 (AS) 3.3.5 Transportabil i,ty. The control group shall be transportable by air, rail, truck and ship when mounted in a shipping container as specified in Section 5. TABLE 1. Dimensions Components Length Width Height Joys ti c k 8.375
27、 inches 3.75 inches 2.25 inches Electronics Package 5.0 inches 4,s inches 5.25 inches 3.3.6 Nameplates and identification marking. Serial number assignment, namepl ate approval , and identification marking shall be in accordance with MIL-N-18307 3.3.6.1 Identification plates. Identification plates f
28、or the joystick 3.3.6.2 Decals, nameplates and markings locations. Al 1 decals, and electronics package shall in accordance with DL 475AS150. nameplates, and markings shall be afflxed to the control group in accordance with DL 475AS150. activity for the control group specified in the contract or pur
29、chase order. The contractor shall serial ize sequentially all control groups whfch are Specified in the contract. 3.3.6.3 Serial numbers. Serial numbers will be assigned by the procuring 3.3.7 Clor and finish. Color and finish of the control group shall be in accordance with DL 4lSE 150 and MIL-E-54
30、00. 3.3.8 Interference control The generation of electromagnetic interference by the control group and the vulnerabil ity of the control group to electromagnetic interference shall be controlled within the 1 fmits of MIL-Si-461 for CLass Al equipment. EM1 testing shall be accomplished under standard
31、 conditions specified in 3.3.10 and in accordance with the procedures of MIL-STD-462 to demonstrate compliance with the MIL-STD-461. 3.3.9 Safety. Safety requirements shall be in accordance with MIL-E-5400 6- 3.3.9.1 Human perfomance/Human engineering. The control group and all component parts there
32、of, shall be designed in accordance with MIL-STD-1472. Recoqnlzed principles of human engineering as specified in MIL-H. 16855 shall be fllowed during design. 3.3.10 Standard conditions. The following conditions shall establ ish normal pertormance characteristics under standard cond making laborator
33、y bench tests. a. Temperature Room ambient (25 I5“C) b. Altitude Normal ground be used to tions and for Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-G-85231 1Ll 7979706 0363988 T MIL -6-85 23 1 (AS ) c. Vibration None d. Humfdty Room ambient u
34、p to 90 percent relative e. Input power voltage +28 Io.1 VDC, +4 a.01 VDC, -4 k0.01 VDC, +5 10.1 VDC (Panel Vol tage) 3.3.11 Service conditions. The control group shall meet the performance requirements of thi s specification under any of the environmental service conditions or combination of these
35、conditions as specified in MIL-E-5400 for class 1 equipment, except as modified herein. 3.3.11.1 Vibration. The control group shall meet the performance requirements o? thi s specification during and after being subjected to the vibration environment specified in 4.5.1, The performance characteristi
36、cs specified in 4.5.1.3 shall apply. temperature-al ti tude combination requirements of MIL-E-5400 for C1 ass 1 equ i pmen t. 3.3.11.2 Temperature-al titude. the control group shall meet the 3.3.11.3 Shock. 3.3.11.3.1 Operational. The control group shall meet the performance requirements after shock
37、 testing in accordance with MIL-E-5400 except that the amplitude for the joystick shall be 2Og in longitudinal axis, 229 in the lateral axis, and 35g fn the vertical axis. The amplitudes for the electronic package shall be 2Og fn longitudinal axis, 309 in the lateral axis, and 469 in the vertical ax
38、is. Figure 5 specifies the appropriate axes. of MIL-E-5400 except that the amplitudes for the joystick shall be 409 longitudinal, 409 lateral, and 479 vertical. electronic package shall be 409 longitudinal requirements ompecification when subjected to the humidity exposure in accordance with MIL-T-5
39、422. 3.3.11.3,2 Crash safety. The control group shall meet the requirements The amp1 itudes for the 409 lateral , and 559 vertical. 3.3.11.4 Humfdity. The control group shall meet the performance 3.3.11.5 Salt spray. The control group shall meet the performance requirements ot this specification whe
40、n subjected to the salt spray exposure in accordance with MIL-T-5422. 3*3.11.6 Explosion. The control group shall meet the performance requirements 07 this specification when subjected to the explosion tests in accordance with MIL-T-5422. 3.3.12 Warm u time. There is no warm-up time required for the
41、 control group prior temperatures bel ow -2O“C, when the temperature is from +54“C to -20C. At three minutes warm-up is required. 6 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-G-5231 IL1 W 9997906 0363989 1 MIL-G-85231( AS) 3.3.13 Electrical
42、power inputs, grounds and loads 3.3.131 Operating power. The control group shall meet all applicable requirements of MIL-STO-704 and shall give specified performance when energized from the fol lowing power sources having characteristics and 1 imi ts as specified in MIL-STD-704. The input power requ
43、ired to operate the control 1 er shall be as fol 1 ows : a. t28.0 10.1 volts dc to pin H of 58 (category A, 75 watts) b. c. d. +5.0 10.1 volts dc to pin D of 5102 (1,5 watts) +4.0 _+0.01 volts dc to pin G of 5101 (24 mw) -4.0 20.01 volts dc to pin F of 5101 (24 mw) 3.3.13.2 Ground and load condition
44、s, The input power (see 3.3.13.1) requires certa7n ground and 1 oad conditions as fol lows : a. Ground pin F of 38 b, 100 ohms 11 percent from pin A of J8 to ground c. Ground pin J of 5101 3.3.13.3 Interface connections. See figure 1 for the interface connections of the joystick and electronics pack
45、age. 3.4 Performance. The performance of the control group shall be as specified below plus any and all performance requfrements specified on DL 475AS150. (Detail function and description for the control group is covered in NAVAIR 16-35OK293-1.) ments shall apply under both standard and extreme serv
46、ice conditions. reduced performance requirements for service conditions are acceptable, such variations shd11 be as specified below: a. Under standard conditions (see 3.3.10), the control group shall provide the regulated outputs as specified in table II, b. Under service conditions (see 3.3.11), th
47、e control group shall provide the adjusted and regulated outputs specified in table III. The resistance between J102-F and 5101-5 on the joystick assembly shall be 10 megohms minimm. Unless otherwise specified herein, these require- When c. 3.5 Detail requirements. 3.5.1 Control , Guided Weapon C-97
48、43A/AWW (joystick)., The joystick shall be manufactured in accordance with OL 475AS150 and the requirements spec1 fied In 3.5.1.1 through 3.5.1.4.4. 7 . Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-G-85231 LY = 797970b 03k3770 8 E M IL-G-85231
49、 (AS) ROTARY SWITCH CABLE SCHEMATIC (REF! t6VDC PWR GND-a- TEST 4 0 - +ZSVDCA I b? U a EL x - C.O. t28v M S I (Y CMD OVRD 28V SIG OUT D OUTPUT +;“ EL OT - FSK BIT+, - U 2 - FSK BIT,*-t- K)L FSK BIT+ N FSK BIT+ w FSK BiT-t-( T FSK BIT- 5 FSK BIT- ,A E TEST PURPOSE ONLY (OUTPUT) d D TEST PURPOSE ONLY (INPUT) + V SYNC (TEST PURPOSE ONLY) j oysti ck and el ectroni c package. a EXTERNAL CONNECTION TO A/C FIGURE 1. Electrical
