1、P FSC-1280 THIS DOCUMENT CONTAINS .;/5 PAGES. MIL-C-85388 12 R 9999906 03611639 1 R L 9- 37-d3 MIL-C-85388(AS) 8 July 1982 MILITARY SPECIFICATION COMPUTER, WEDON ALYING CP- 1444/A This Specification is approved for use by Naval Air Systems Command, Department of the Navy, and is available for use by
2、 all Departments and Agencies of the Department of Defense. 1. SCOPE 1.1 Scope, The equipment, Computer, Weapon Aiming, CP-l444/A (WAC), covered by this specification is a microprocessor based digital controller. It accepts analog, digital, and discrete input signals from various systems within the
3、aircraft and with ballistics data stored within the WAC, on programmable read only rriemory chips, performs the following: a. Lead angle computations for the Head-Up-Display b. Continuously computed impact point computations for the aiming of guns in Air-to-Air operational mode. head-up-display aimi
4、ng of bombs, rockets, and guns in the Air-to-Surface operational modes. heading outputs of the attitude and heading reference system and the Signal Data Converter (SDC). d. Performs an interface function between the Tacan Converter and the Signal Da ta Converter. e. Performs an interface function be
5、tween the UHF Homer Adapter and the Attitude Director Indicator (DI). f. Provides reference voltages and power supplies to other aircraft systems. C. Performs an interface function between the attitude and 1.2 Associated equipment. This equipment shall operate with the asso- ciated equipment listed
6、in 6.4. Beneficial comments (recommendations, additions, deletions) and any pertinent data which may be of use in improving this document should be addressed to: “Commanding Officer, Naval Air Engineer- ing Center, Engineering Specifications and Standards Department (code 93) iakehurst, New Jersey 0
7、8733“, by using the self- addressed Standardization Document Improvement Proposal (DD Form 1426) appearing at the end of this document or by letter. Licensed by Information Handling ServicesMIL-C-85388 12 7979906 0364640 8 U MIL-C-85388(AS) 2. AEPLICABLE DOCUXENTS 2.1 Issues of documents. The follow
8、ing documents of the issue in effect on date of invitation for bids or request for proposal, form a part of this specification to the extent specified herein. SPECIFICATIONS MILITARY MIL-W-5088 - Wiring; Aircraft, Selection and Installation of NIL-E-5272 - Environmental Testing, Aeronautical and Ass
9、ociated Equipment , General Specification for MIL-E-5400 - Electronic Equipment, Airborne, General Specification for MIL-C-6021 - Castings, Classification and Inspection of MIL-M-7793 - Meter, Time Totalizing MIL-E-17555 - Electronic and Electrical Equipment Accessories, and MIL-N-18307 - Nomenclatu
10、re and Identification for Electronic, Repair Parts Aeronautical and Aeronautical Support Equipment Including Ground Support Equipment MIL-T-23103 - Thermal Performance Evaluation, .Airborne Electronic MIL-H-46855 - Human Engineering Requirements for LCiilitary Systems, Equipment and Systems, General
11、 Requirement for Equipment and Facilities STAARDS FEDERAL FED-STD-595 - Colors HILITMY MIL-STD-461 - Electrorcagnetic Interference Characteristics Requirements for Equiprnen t MIL-STD-704 - Aircraft Electric Power Characteristics MIL-STP781C - Reliability Design Qualification & MIL-STD-1472 - Human
12、Engineering Design Criteria for Ulitary MIL-STD-2068 - Reliability Development Tests MIL-STD-45662 - Calibration System Requirements Produc tion Xccep tance Tests Exponentia.1 Dis tribut ion Systems, Equipment and Facilities (Copies of specifications, standards, drawings, and publications required b
13、y contractors in connection with specific procurement func- tions should be obtained from the procuring activity or as directed by the contracting officer.) 2 Licensed by Information Handling ServicesMIL-C-85388 12 M 777770b 0361t641 T R 2.1.2 Other publications. The following documents form a part
14、of this specification to the extent specified herein. Unless otherwise indicated, the issue in effect on &te of invitation for bids or request for proposal shall apply. McDONNELL DOUGLAS CORPORATION MDC A3780 - AV-8A/AV-8%/AV-8C/YAV-8% Vibration, Shock, and Acoustic Design Requirements and Test Proc
15、edures for Aircraft Equipment Installation. (Application for copies should be addressed to the McDonnell Aircraft Company, Box 516, Saint Louis, Missouri 63166) 2.1.3 Order of- precedence. When the requirements of the contract, this specification, or applicable subsidiary specifications are in confl
16、ict, the following precedence shall apply: a. b. Ce Contract. f ication. The contract shall have precedence over any speci- This specification. over all applicable subsidiary specifications. from this specification, or from subsidiary specifications, where applicable, shall be specifically approved
17、in writing by the procuring activity. This specification shall have precedence Any deviation Referenced specifications. have precedence over all applicable subsidiary specifications referenced therin. All referenced specifications shall apply to the extent specified. Any referenced specification sha
18、ll 3. REQUIRFMZNTS 3.1 First article. When specified (see 6-31, the contractor shall furnish sample unit(s) for first article inspection and approval (see 4.3 and 6.3) 3.2 Parts and materials. fillment of major design objectives shall be the prime consideration. In so doing, the following shall gove
19、rn: In the selection of parts and materials ful- a. Microelectronic integrated circuits shall be used as a prime functional element of the equipment. b. Circuits shall be designed to use a minimum of different parts, subassemblies, cards and modules. ci Parizs and materials shall be procured from Qualified Product List (QPL) sources when they exist. e -. U W O 3 - si + O Y O - d m 4 1 - C 27 ua UL ou i2 - V d U 4 *a 50 oc Y4 me - Y I + + o, El O O U 1: i 4 1 1 + O Y O o, rl iiI rl a 1 rl CO o Ud au aJ O 30 Licensed by Information Handling Services
