MIL-STD-2131 Revision A:1991
Current
Current
The latest, up-to-date edition.
Launcher, Ejection, Guided Missile, Aircraft, General Design Criteria for
Available format(s)
PDF
Language(s)
English
Published date
16-12-1991
Publisher
€16.67
Excluding VAT
Specifies requirements for an ejection launcher providing carriage and power ejection of an airborne guided missile from tactical aircraft in flight.
| DocumentType |
Standard
|
| Pages |
41
|
| ProductNote |
NEW CHILD NOT 1 2019 IS NOW ADDED
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Current
|
The purpose of this document is to provide guidelines for establishing general criteria for the design, development, construction, maintenance and testing of an ejection launcher.
| DEFSTAN 00-970(PT0)/9(2012) : 2012 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/17(2016) : 2016 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/7(2011) : 2011 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/14(2014) : 2014 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/15(2015) : 2015 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/12(2014) : 2014 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/11(2013) : 2013 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/13(2014) : 2014 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/8(2011) : 2011 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/10(2013) : 2013 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/16(2015) : 2015 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| MIL-I-8671 Revision D:1994 | Installation of Droppable Stores and Associated Release Systems |
| MIL HDBK 5 : G_VOL2 | METALLIC MATERIALS AND ELEMENTS FOR AEROSPACE VEHICLE STRUCTURES |
| MIL-I-8500 Revision D:1980 | Interchangeability and Replaceability of Component Parts for Aerospace Vehicles |
| MIL-STD-2088 Revision B:2007 | Bomb Rack Unit (BRU), Single Store, Aircraft |
| MIL-STD-704 Revision F:2004 | Aircraft Electric Power Characteristics |
| MIL-STD-970 Base Document:1987 | STANDARDS AND SPECIFICATIONS, ORDER OF PREFERENCE FOR THE SELECTION OF (NO S/S DOCUMENT) |
| MIL-STD-130 Revision N:2007 | Identification Marking of U.S. Military Property |
| L-P-383 Base Document:1967 | Plastic Material, Polyester Resin, Glass Fiber Base, Low Pressure Laminated |
| MIL-A-8591 Revision H:1990 | Airborne Stores, Suspension Equipment and Aircraft-Store Interface (Carriage Phase); General Design Criteria for (S/S by MIL-STD-8591) |
| MIL-STD-810 Revision G:2008 | ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS |
| MIL-H-6875 Revision H:1989 | Heat Treatment of Steel, Process for (S/S by SAE-AMS-H-6875) |
| MIL-T-7743 Revision F:1993 | Testing, Store Suspension and Release Equipment, General Specification for |
| MIL-A-22771 Revision D:1984 | Aluminum Alloy Forgings, Heat Treated (S/S by SAE-AMS-A-22771) |
| MIL F 18264 : D | FINISHES: ORGANIC, WEAPONS SYSTEM, APPLICATION AND CONTROL OF |
| MIL-STD-1760 Revision E:2007 | Aircraft/Store Electrical Interconnection System |
| MIL S 5002 : D | SURFACE TREATMENTS AND INORGANIC COATINGS FOR METAL SURFACES OF WEAPONS SYSTEMS |
| QQ-A-367 Revision H:1973 | Aluminum Alloy Forgings (S/S by SAE-AMS-QQ-A-367) |
| ASME B46.1 : 2009 | SURFACE TEXTURE (SURFACE ROUGHNESS, WAVINESS, AND LAY) |
| MIL-STD-2175 Revision A:1993 | CASTINGS, CLASSIFICATION AND INSPECTION OF (S/S BY SAE-AMS-STD-2175) |
| MIL P 15024 : E | PLATES, TAGS AND BANDS FOR IDENTIFICATION OF EQUIPMENT |
| MIL-STD-889 Revision C:2016 | Galvanic Compatibility of Electrically Conductive Materials |
| MIL-C-85485 Revision A:1983 | CABLE, ELECTRIC, FILTER LINE, RADIO FREQUENCY ABSORPTIVE |
| MIL-F-7190 Revision B:1985 | Forging, Steel, for Aircraft/Aerospace Equipment and Special Ordinance Applications (S/S by SAE-AMS-F-7190) |
| MIL-STD-838 Revision C:1983 | LUBRICATION OF MILITARY EQUIPMENT |
| MIL C 38999 : J | CONNECTOR, ELECTRICAL, CIRCULAR, MINIATURE, HIGH DENSITY, QUICK DISCONNECT (BAYONET THREADED & BREECH COUPLING) ENVIRONMENT RESISTANT, REMOVABLE CRIMP & HERMETIC SOLDER CONTACTS |
| MIL-STD-1568 Revision D:2015 | Materials and Processes for Corrosion Prevention and Control in Aerospace Weapons Systems |
| MIL-STD-1587 Revision D:2017 | Material and Process Requirements for Aerospace Weapons Systems |
| MIL-STD-882 Revision E:2012 | System Safety |
| MIL-STD-461 Revision G:2015 | Requirements for the Control of Electromagnetic Interference Characteristics of Subsystems and Equipment |
| MIL-B-7883 Revision B:1968 | Brazing of Steels, Copper, Copper Alloys, Nickel Alloys, Aluminum and Aluminum Alloys (Future Acquisition should specify one AWS-C3.4, AWS-C3.5, AWS-C3.6 and AWS-C3.7) |
| MIL C 5541 : E | CHEMICAL CONVERSION COATINGS ON ALUMINUM AND ALUMINUM ALLOYS |
| MIL-HDBK-235-1 Revision C:2010 | Military Operational EME Profiles Part 1D General Guidance |
| MIL A 8625 : F | ANODIC COATINGS FOR ALUMINUM AND ALUMINUM ALLOYS |
| MIL-D-81303 Revision A:1966 | DESIGN AND EVALUATION OF CARTRIDGES FOR STORES SUSPENSION EQUIPMENT |
| MIL-A-21180 Revision D:1984 | Aluminum-Alloy Castings, High Strength (S/S by SAE-AMS-A-21180) |
| MIL-STD-1472 Revision G:2012 | Human Engineering |
| MIL-H-6088 Revision G:1991 | Heat Treatment of Aluminum Alloys (S/S by SAE-AMS-H-6088) |
| MIL H 5606 : G | HYDRAULIC FLUID, PETROLEUM BASE; AIRCRAFT; MISSILE AND ORDNANCE |
| MIL-H-46855 Revision B:1979 | Human Engineering Requirements for Military Systems Equipment and Facilities (S/S by MIL-STD-46855) |
| MIL-STD-462 Revision D:1993 | MEASUREMENT OF ELECTROMAGNTIC INTERFERENCE CHARACTERISTICS (S/S BY MIL-STD-461) |
| QQ-P-416 Revision F:1991 | Plating, Cadmium (Electrodeposited) (S/Sby SAE-AMS-QQ-P-416) |
| MIL-C-8837 Revision B:1983 | Coating, Cadmium (Vacuum Deposited) (S/S by SAE-AMS-C-8837) |
| MIL-B-5087 Revision B:1964 | Bonding, Electrical, and Lightning Protection, for Aerospace Systems (S/S by MIL-STD-464) |
| MIL-W-5088 Revision L:1991 | Wiring, Aerospace Vehicle (Future Design Should Refer to SAE-AS50881) |
| MIL L 46010 : D | LUBRICANT, SOLID FILM, HEAT CURED, CORROSION INHIBITING |
| MIL-F-83142 Revision A:1969 | Forging, Titanium Alloys, Premium Quality (See Notice 5 for Replacement Information) |
| MIL-F-7179 Revision G:1993 | Finishes, Coatings, and Sealants for the Protection of Aerospace Weapons Systems (S/S by MIL-STD-7179) |
| MIL T 31000 : 0 | TECHNICAL DATA PACKAGES - GENERAL SPECIFICATION FOR |
Summarise
Access your standards online with a subscription
-
Simple online access to standards, technical information and regulations.
-
Critical updates of standards and customisable alerts and notifications.
-
Multi-user online standards collection: secure, flexible and cost effective.
Important note : Users cannot be edited or removed once added to your Multi user PDF.