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  • MIL-T-18232 Revision B:1968

    Withdrawn A Withdrawn Standard is one, which is removed from sale, and its unique number can no longer be used. The Standard can be withdrawn and not replaced, or it can be withdrawn and replaced by a Standard with a different number.

    TARGET, AERIAL, POWERED, DESIGN AND CONSTRUCTION OF GENERAL SPECIFICATION FOR

    Available format(s):  PDF

    Withdrawn date:  28-06-2018

    Language(s):  English

    Published date: 

    Publisher:  US Military Specs/Standards/Handbooks

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    Abstract - (Show below) - (Hide below)

    Covers the general requirements of the Naval Air Systems Command Headquarters (NAVAIR) for the design and construction of aerial powered targets, other than converted aircraft targets.

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    Committee FSC 1550
    Document Type Standard
    Product Note NEW CHILD NOT 1 2018 IS NOW ADDED.
    Publisher US Military Specs/Standards/Handbooks
    Status Withdrawn

    Standards Referencing This Book - (Show below) - (Hide below)

    MIL HDBK 5 : G_VOL2 METALLIC MATERIALS AND ELEMENTS FOR AEROSPACE VEHICLE STRUCTURES
    MIL L 7808 : K (1) LUBRICATING OIL, AIRCRAFT TURBINE ENGINE, SYNTHETIC BASE
    MIL-I-8500 Revision D:1980 INTERCHANGEABILITY AND REPLACEABILITY OF COMPONENT PARTS FOR AEROSPACE VEHICLES
    MIL-STD-129 Revision R:2014 Military Marking for Shipment and Storage
    MIL-C-18263 Revision F:1971 COLOR, EXTERIOR, NAVAL AIRCRAFT, REQUIREMENTS FOR
    MIL-STD-704 Revision F:2004 AIRCRAFT ELECTRIC POWER CHARACTERISTICS
    MIL-STD-130 Revision N:2007 IDENTIFICATION MARKING OF U.S. MILITARY PROPERTY
    MIL-P-26366 Revision A:1962 PROPELLER SYSTEMS, AIRCRAFT, GENERAL SPECIFICATION FOR
    MIL L 23699 : E LUBRICATING OIL, AIRCRAFT TURBINE ENGINES, SYNTHETIC BASE
    MIL-A-8591 Revision H:1990 AIRBORNE STORES, SUSPENSION EQUIPMENT AND AIRCRAFT-STORE INTERFACE (CARRIAGE PHASE); GENERAL DESIGN CRITERIA FOR
    MIL-H-25475 Revision B:1971 HYDRAULIC SYSTEM, MISSILE, DESIGN, INSTALLATION TESTS AND DATE REQUIREMENTS, GENERAL REQUIREMENTS FOR
    MIL-W-8160 Revision D:1961 WIRING, GUIDED MISSILE, INSTALLATION OF, GENERAL SPECIFICATION FOR
    MIL-T-7743 Revision F:1993 TESTING, STORE SUSPENSION AND RELEASE EQUIPMENT, GENERAL SPECIFICATION FOR
    MIL-R-7705 Revision B:1975 RADOME, GENERAL SPECIFICATION FOR
    MIL T 5624 : R TURBINE FUEL, AVIATION, GRADES JP 4 AND JP 5
    MIL-E-6051 Revision D:1967 ELECTROMAGNETIC COMPATIBILITY REQUIREMENTS, SYSTEM
    MIL-A-8870 Revision C:1993 AIRPLANE STRENGTH AND RIGIDITY VIBRATION, FLUTTER, AND DIVERGENCE
    MIL I 18464 : G NOTICE 1 INSIGNIA AND MARKINGS FOR NAVAL WEAPONS SYSTEMS
    MIL-E-7016 Revision F:1976 ELECTRIC LOAD AND POWER SOURCE CAPACITY, AIRCRAFT ANALYSIS OF
    MIL-D-21625 Revision G:1993 DESIGN AND EVALUATION OF CARTRIDGES FOR CARTRIDGE ACTUATED DEVICES
    MIL E 5400 : T ELECTRONIC EQUIPMENT, AEROSPACE, GENERAL SPECIFICATION FOR
    MIL-STD-838 Revision C:1983 LUBRICATION OF MILITARY EQUIPMENT
    MIL-I-7171 Revision D:1993 INSULATION BLANKET, THERMAL ACOUSTICAL
    MIL T 6396 : E TANKS, AIRCRAFT PROPULSION FLUID SYSTEM, INTERNAL REMOVABLE, NON-SELF-SEALING
    MIL-H-18325 Revision B:1959 HEATING AND VENTILATING SYSTEMS, AIRCRAFT, GENERAL SPECIFICATION FOR
    MIL-F-17874 Revision B:1965 FUEL SYSTEMS, AIRCRAFT, INSTALLATION AND TEST OF
    MIL-G-5572 Revision F:1969 GASOLINE, AVIATION, GRADES 80/87, 100/130, 115/145
    MIL E 7729 : LATEST
    MIL-HDBK-217 Revision F:1991 RELIABILITY PREDICTION OF ELECTRONIC EQUIPMENT
    MIL-C-8678 Base Document:1984 COOLING REQUIREMENTS OF POWER PLANT INSTALLATIONS
    MIL-H-8775 Revision D:1976 HYDRAULIC SYSTEM COMPONENTS, AIRCRAFT AND MISSILES GENERAL SPECIFICATION FOR
    MIL-T-5422 Revision F:1971 TESTING, ENVIRONMENTAL, AIRCRAFT ELECTRONIC EQUIPMENT
    MIL-D-8804 Revision B:1993 DE-ICING SYSTEM, PNEUMATIC BOOT, AIRCRAFT, GENERAL SPECIFICATION FOR
    MIL-P-25062 Revision B:1964 PARACHUTE RECOVERY SYSTEM, MISSILE AND DRONE, GENERAL REQUIREMENT FOR DEVELOPMENT OF
    MIL-P-116 Revision J:1988 PRESERVATION, METHODS OF
    MIL-J-8667 Revision A:1970 JET ASSISTED TAKE OFF SYSTEMS - DESIGN AND INSTALLATION OF, IN NAVAL AIRCRAFT
    MIL-E-8189 Revision H:1975 ELECTRONIC EQUIPMENT, MISSILES, BOOSTERS AND ALLIED VEHICLES, GENERAL SPECIFICATION FOR
    MIL-I-18802 Revision A:1962 INSTALLATION OF FUEL AND OIL LINES, AIRCRAFT
    MIL H 5606 : G HYDRAULIC FLUID, PETROLEUM BASE; AIRCRAFT; MISSILE AND ORDNANCE
    MIL T 5579 : 0 TANK, SELF-SEALING OIL, AIRCRAFT
    MIL F 18372 : 0 FLIGHT CONTROL SYSTEMS, DESIGN, INSTALLATION AND TEST OF, AIRCRAFT (GENERAL SPECIFICATION FOR)
    MIL V 5636 : C VALVE, LUBRICATING OIL COOLER, PETROLEUM BASE TEMPERATURE REGULATING WITH SURGE PROTECTION
    MIL-B-5087 Revision B:1964 BONDING, ELECTRICAL AND LIGHTING PROTECTION, FOR AEROSPACE SYSTEMS
    MIL R 22449 : NOTICE 1 REQUIREMENTS (CERTIFICATION) FOR PYROTECHNIC ITEMS
    MIL-F-7179 Revision G:1993 FINISHES, COATINGS, AND SEALANTS FOR THE PROTECTION OF AEROSPACE WEAPONS SYSTEM
    MIL-S-7742 Revision D:1991 SCREW THREADS, STANDARD, OPTIMUM SELECTED SERIES, GENERAL SPECIFICATION FOR
    MIL-C-5637 Revision B:1964 COOLER, LUBRICATING OIL, PETROLEUM BASE, AIRCRAFT ENGINE, TUBULAR
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