MIL-H-25475 Revision B:1971
Withdrawn
Withdrawn
Hydraulic Systems, Missile Design, Installation and Tests, General Requirements for (No S/S Document)
Available format(s)
PDF
Published date
04-29-1971
Publisher
Withdrawn date
09-09-1993
US$20.00
Excluding Tax where applicable
Details design, installation, and testing of the above systems.
| DocumentType |
Standard
|
| Pages |
36
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Withdrawn
|
This specification covers the design, installation, and testing of missile hydraulic systems.
| MIL V 81940 : B | VALVE, SAMPLING AND BLEED, HYDRAULIC, TYPE LI SYSTEMS |
| MIL F 8815 : D | FILTER AND FILTER ELEMENTS, FLUID PRESSURE, HYDRAULIC LINE, 15 MICRON ABSOLUTE AND 5 MICRON ABSOLUTE, TYPE 11 SYSTEMS; GENERAL SPECIFICATION FOR |
| MIL F 83861 : B | FILTER ELEMENTS, NONCLEANABLE, FLUID PRESSURE, HYDRAULIC LINE, 5 AND 15 MICRON ABSOLUTE, TYPE 1I, SYSTEMS GENERAL SPECIFICATION FOR |
| MIL-D-8684 Revision B:1959 | Data and Tests, Engineering, Contact Requirements for Air Launched Guided Missile Systems (No S/S Document) |
| MIL-H-8775 Revision D:1976 | Hydraulic System Components, Aircraft and Missiles General Specification for (S/S by SAE-AS8775) |
| MIL-R-8931 Revision A:1994 | Reservoirs,Aircraft and Missile, Hydraulic, Separated Type |
| MIL F 83860 : C | FILTER ELEMENTS, NONCLEANABLE, FLUID PRESSURE, HYDRAULIC LINE, 5 MICRON ABSOLUTE, TYPE II, SYSTEMS, GENERAL SPECIFICATION FOR |
| MIL-D-8685 Revision B:1967 | Data and Tests, Engineering, Contract Requirements for Guided Missile Target Systems (No S/S Document) |
| MIL-T-7081 Revision D:1965 | TUBE, ALUMINUM ALLOY, SEAMLESS, ROUND, DRAWN 6061, AIRCRAFT HYDRAULIC QUAL ITY (S/S BY SAE-AMS-T-7081) |
| MIL-F-45764 Revision C:1990 | Fluid Lines and Fittings for Missiles and Related Ground Equipment: Fabrication and Installation of (No S/S Document) |
| MIL-T-18232 Revision B:1968 | Targets, Aerial, Powered, Design and Construction of General Specification for (No S/S Document) |
| MIL R 25534 : A NOTICE 1 | ROCKET MOTOR, AERONAUTICAL, QUALIFICATION TEST FOR |
| MIL-STD-1606 Revision A:1983 | TECHNICAL INFORMATION REQUIREMENTS FOR AIR LAUNCHED GUIDED MISSILE PROPOSALS (NO S/S DOCUMENT) |
| MIL R 25532 : A | ROCKET MOTOR, AERONAUTICAL, QUALIFICATION TEST FOR |
| MIL-STD-130 Revision N:2007 | Identification Marking of U.S. Military Property |
| MIL-F-18280 Revision F:1995 | Fittings, Flareless Tube, Fluid Connection (S/S by SAE-AS18280) |
| MIL-T-6845 Revision D:1985 | TUBING, STEEL, CORROSION-RESISTANT (S30400), AEROSPACE VEHICLE HYDRAULIC SYSTEM 1/8 HARD CONDITION (S/S BY SAE-AMS-T-6845) |
| MIL J 5513 : C | JOINT, HYDRAULIC SWIVEL |
| MIL C 25427 : A | COUPLING ASSEMBLY, HYDRAULIC, SELF-SEALING, QUICK DISCONNECT |
| MIL-M-7997 Revision C:1981 | Motor, Aircraft Hydraulic, Constant Displacement General Specification for |
| MIL-H-38360 Revision B:1966 | Hose Assemblies, Tetrafluoroethylene, High-Temperature, High Pressure, 3000 PSI, Hydraulic and Pneumatic (S/S by SAE-AS604 and SAE-AS1339) |
| MIL-W-8160 Revision D:1961 | WIRING, GUIDED MISSILE, INSTALLATION OF, GENERAL SPECIFICATION FOR (S/S BY MIL-W-5088) |
| MIL H 25579 : E | HOSE ASSEMBLY, TETRAFLUOROETHYLENE, HIGH TEMPERATURE MEDIUM PRESSURE, GENERAL REQUIREMENTS FOR |
| MIL A 5498 : D | ACCUMULATORS, HYDRAULIC, CYLINDRICAL 3000 PSI, AIRCRAFT |
| AN929 Revision 14:2017 | Cap Insert, Assembly, Pressure Seal, Flared Tube Fitting |
| MS24334 Revision E:1992 | Coupling Assembly, Hydraulic, Self-Sealing, Flareless Fitting to Internal Thread Boss |
| MS21919 Revision E:1981 | Clamp, Loop Type, Cushioned, Support |
| MS33620 Revision B:1964 | CHART, HOSE SELECTION (S/S BY SAE-AIR797) |
| MS33656 Revision J:1987 | FITTING END, STANDARD DIMENSIONS FOR FLARED TUBE CONNECTION AND GASKET SEAL (S/S BY SAE-AS4395) |
| WW-T-700-4 Revision F:1983 | TUBE, ALUMINUM ALLOY, DRAWN, SEAMLESS, 5052 (S/S BY SAE-AMS-WW-T-700/4) |
| MS33566 Revision B:1975 | FITTINGS, INSTALLATION OF FLARELESS TUBE, STRAIGHT-THREADED CONNECTORS (S/S BY SAE-AS33566) |
| MIL-G-5514 Revision G:1993 | Gland Design; Packings, Hydraulic, General Requirements for |
| MIL H 6083 : E | HYDRAULIC FLUID, PETROLEUM BASE, FOR PRESERVATION AND OPERATION |
| MS33583 Revision C:1993 | TUBING END DOUBLE FLARE, STANDARD DIMENSIONS FOR (S/S BY SAE-AS33583) |
| MIL-F-5509 Revision D:1978 | Fitting, Flared Tube, Fluid Connection (see Notice 2 for Additional Superseding Information) |
| MS33584 Revision C:1990 | TUBING END STANDARD DIMENSIONS FOR FLARED (S/S BY SAE-AS4330) |
| MIL-STD-100 Revision G:1997 | ENGINEERING DRAWINGS (S/S BY ASME-Y14.100, ASME-Y14.24, ASME-Y14.35M, AND ASME-14.34M) |
| MIL V 5523 : D | VALVE, RELIEF, HYDRAULIC PRESSURE |
| MS33611 Revision A:1983 | TUBE BEND RADII (S/S BY SAE-AS33611) |
| MIL G 8348 : H | GAGE, ASSEMBLIES, AIR PRESSURE, DIAL INDICATING CHUCK TYPE SELF CONTAINED |
| MIL H 5606 : G | HYDRAULIC FLUID, PETROLEUM BASE; AIRCRAFT; MISSILE AND ORDNANCE |
| MIL-STD-1247 Revision D:2009 | Markings, Functions and Hazards Designations of Hose, Pipe, and Tube Lines for Aircraft Missile, and Space Systems |
| MIL-B-5087 Revision B:1964 | Bonding, Electrical, and Lightning Protection, for Aerospace Systems (S/S by MIL-STD-464) |
| MIL-T-7081 Revision D:1965 | TUBE, ALUMINUM ALLOY, SEAMLESS, ROUND, DRAWN 6061, AIRCRAFT HYDRAULIC QUAL ITY (S/S BY SAE-AMS-T-7081) |
Summarise
US$20.00
Excluding Tax where applicable
Please Login or Create an Account so you can add users to your Multi user PDF Later.
Important note : All end users must be registered with an Account prior to user licenses being assigned.
Users cannot be edited or removed once added to your Multi user PDF.