NAVY MIL-L-85762 A-1988 LIGHTING AIRCRAFT INTERIOR NIGHT VISION IMAGING SYSTEM (NVIS) COMPATIBLE《飞机夜视成像系统兼容照明设备》.pdf
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1、INCH-POLIND1MIL-L-85762A26 August 1988SUPERSEDESMIL-L-8576224 January 1986MILITARY SPECIFICATIONLIGHTING, AIRCRAFT, INTERIOR, NIGHT VISIONIMAGING SYSTEM (NVIS) COMPATIBLEThis specification is approved for use by all Departments andAgencies of the Department of Defense.1. SCOPE1.1 =. This specificati
2、on establishes performance, general COflfi9UratiOn,test and acceptance requirements for NVIS (see 6.5.1) compatible aircraft interiorlighting. It is applicable to all systems, subsystems, component equiPment andhardware which Drovide the lightinq environment in aircraft crewstations andcompartments
3、where NVIS are employed.1.2 Purpose. The purpose of this specification is to provide performancerequirements and testing methodology to ensure effective and standardized aircraftinterior lighting for NVIS compatibility.1.3 Classification. Night Vision Imaging System (NVIS) compatible aircraftInterio
4、r lighting shall be of the following types and classes, as specified (See6.2.b).Type I Lighting compatible with any Direct View Image NVIS(see 6.5.1.1) utilizing generation 111 Imageintensifier tubes.Type 11 Lighting compatible with any Projected Image NVIS(see 6.5.1.2) utilizing generation III Imag
5、eintensifier tubes.Class A Lighting compatible with NVIS utilizing 625 nmminus blue objective lens filters (see 6.5.1.3) with thespecification; of Figure 1.I Class B Liahtina compatible with NVIS utilizing 665 nmmius biue objective lens filters (see-6.5.1.4) with thespecifications of Figure 2.Benefl
6、c!al comments (recommendations, additions, deletions) and any pertinent datawhich may be of use in improving this document should be addressed to: SystemsEngineering and Standardization Department (Code 93), Naval Air Engineering CenterLakehurst, NJ 08733, by using the self-addressed Standardization
7、 OocumentImprovement Proposal (DD Form 1426) appearing at the end of this document or byletter.AMSC NO. N4524 FSC 6220DISTRIBUTION STATEMENT A. Approved for public release; distribution is unlimited.Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL
8、-L-85762A2. APPLICABLE DOCUMENTS2.1 Government documents.2.1.1 Specificatiens,standards, and handbooks. The following specifications,standards, and handbooks form a part of this specification to the extent specifiedherein. Unless otherwise specified, the issues of these documents shall be thoseliste
9、d in the issue of the Department of Defense Index of Specifications andStandards (DoOISS) and supplement thereto, cited in the solicitation (see 6.2.c).SPECIFICATIONSMIL-R-22MIL-L-5057MIL-B-5087MIL-N-5088MIL-E-6051MIL-L-6503MIL-C-6781MIL-E-7080MIL-P-7788MIL-M-8650MIL-H-881OMIL-M-18012MIL-L-18276MIL-
10、I-18373MIL-S-2271OResistors, Variable (Wire-wound, Power Type),General Specification forLight, Instrument, Individual, GeneralSpecification forBonding, Electrical, Lightning Protection forAerospace SystemsWiring, Aerospace VehicleElectromagnetic Compatlbllity Requirements, SystemsLighting Equipment,
11、 Aircraft, General SpecificationFor Installation ofControl Panel Aircraft Equipment, Rack or ConsoleMountedElectric Equipment, Aircraft, Selection andInstallation ofPanels, Information, Integrally IlluminatedMockups, Aircraft, Construction ofHandles, Control, AircraftMarkngs for Aircrew Station Disp
12、lays Design andConfiguration ofLighting, Aircraft Interior, Installation ofInstruments and Navigation Equipment, AircraftInstallation ofSwitches, Code Indicating Wheel (Printed Circuit),(Thumbwheel and Pushbutton), General Specificationfor2Provided by IHSNot for ResaleNo reproduction or networking p
13、ermitted without license from IHS-,-,-MIL-S-22885 -MIL-K-25049 -MIL-L-25467 -MIL-L-25866 -MIL-L-27160 -MIL-T-27493 -MIL-S-38039 -MIL-D-87157 -STANDARDSMIL-STD-130 -MIL-STD-143 -MIL-STD-150 -MIL-STD-203 -MIL-STD-250 -MIL-STD-411 -MIL-STD-461 .-MIL-STO-462 -MIL-STD-704 -MIL-STD-882 -MIL-L-85762ASwitch
14、, Push Button,Specification for11 uminated, GeneralKnobs, Control, Electronic Equipment, AircraftLighting, Integral, Red Aircraft Instrument, GeneralSpecification forLight, Emergency Exit, Aircraft LEU 1-ALighting, Instrument, Integral, White GeneralSpecification ForTransformer, Variable, Single Pha
15、se, 400 Cycles,General Specification forSystems, Illuminated, Warning, Caution, andAdvisory, General Specification forDisplay, Diode, Light Emitting, Solid State,General Specification forIdentification Marking of U.S. Military PropertyStandards and Specifications, Order of Precedencefor the Selectio
16、n OfPhotographic LensesAircrew Staton Controls and Displays; Assignment,Location, and Actuation of, for Fixed Wing AircraftAircrew Station Controls and Displaysfor RotaryWing AircraftAircrew Station SignalsElectromagnetic Emission and SusceptibilityRequirements for the Control of ElectromagneticInte
17、rferenceElectromagnetic Interference Characteristics,Measurement ofAircraft Electrical Power CharacteristicsSystem Safety Program.Requirements3Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL,-STD-1333-MIL-STD-1472 -MIL-STD-1776 -HANDBOOKSMIL-L-85
18、762AAircrew Station Geometry for Military AircraftHuman Engineering Design Criteria for MilitarySYstems, Equipment and FacilitiesAircrew Station and Passenger AccommodationsUSAF, AFSC Design Handbook,DH 1-3(Unless otherwise indicated, copies of federal and military specifications,standards, and hand
19、books are available from the Naval Publications and Forms.Center, (ATTN: NPODS), 5801 Tabor Avenue, Philadelphia,.PA 19120-5099 ./-”2.2 Order of precedence. In the event of a conflict between”-the text of thisspecification and the references cited herein, the text.of this specification shalltake pre
20、cedence. Nothing in this specification, however, shall supersedeapplicable laws and regulations unless a specific exemption has been obtained.3. REQUIREMENTS3.1 Description. This specification defines the performance requirements andtest procedures applicable to NVIS compatible lighting systems for
21、new or modifiedaircraft lighting equipment and crewstations when specified in the weapon systemdesign specification.3.2 Selection of specifications and standards. Specifications and standardsfor necessary commodities and services not specified herein or in the individualequipment specifications shal
22、l be selected in accordance with MIL-STO-143.3.3 First article. When specified In the contract or purchase order (see6.2.d), a sample shall be subjected to first article inspection (see 4.4 and 6.4).3.4 =. When required by the acquiring activity (see 6.2.g) prior toincorporation into production or r
23、edesigned aircraft, an aircrew station mockupshall be prepared and made available by the contractor to ensure compliance withthe NVIS compatibility and lighting system, subsystem or component requirementsspecified herein. When inspected in accordance with 4.8.1, 4.8.2, and 4.8.3 the .aircrew station
24、 mockup shall conform to all of the requirements of thisspecification as applicable. There shall be no evidence of degraded NVISresolution in the presence of aircraft interior lighting when the observer islooking outside of, or transitioning from inside to outside of the aircraft.3.4.1 US Navy and U
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