MIL-HDBK-244 Revision A:1990
Current
Current
The latest, up-to-date edition.
Guide to Aircraft/Stores Compatibility
Available format(s)
PDF
Published date
06-04-1990
Publisher
€16.67
Excluding VAT
Covers all aspects of aircraft and weapons compatibility; mechanical, electrical, structural, aerodynamic, etc.
| DevelopmentNote |
A NOTICE 1 - Notice of Validation. (09/2014)
|
| DocumentType |
Standard
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| Pages |
145
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| ProductNote |
NEW CHILD NOT 2 2019 IS NOW ADDED
|
| PublisherName |
US Military Specs/Standards/Handbooks
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| Status |
Current
|
The handbook is intended to cover all aspects of aircraft/weapons compatibility: mechanical, electrical, structural, aerodynamic, etc. These are dealt with individually as they relate to various elements of the complete system. The material has been organized to present design guidelines for the five general categories of weapon system components: aircraft, suspension equipment, stores, stores management equipment, and ground support equipment. This information deals with compatibility of the components while the system is on the ground, in flight, and during weapon delivery.
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| DEFSTAN 00-69(PT2)/1(1998) : 1998 | AIRCRAFT/STORE ELECTRICAL INTERCONNECTION SYSTEM - PART 2: DESIGN PRINCIPLES AND PRACTICES FOR, AND GUIDE TO, THE IMPLEMENTATION OF THE AIRCRAFT/STORE ELECTRICAL INTERCONNECTION SYSTEM |
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| MIL-HDBK-516 Revision C:2014 | Airworthiness Certification Criteria |
| MIL-HDBK-1760 Revision A:2004 | Aircraft/Store Electrical Interconnection System |
| MIL-I-8671 Revision D:1994 | Installation of Droppable Stores and Associated Release Systems |
| MIL-HDBK-1763 Base Document:1998 | Aircraft/Stores Compatibility: Systems Engineering Data Requirements and Test Procedures |
| MIL-A-8865 Revision B:1987 | Airplane Strength and Rigidity Miscellaneous Loads |
| MIL-T-8679 Base Document:1954 | TEST REQUIREMENTS, GROUND, HELICOPTER (NO S/S DOCUMENT) |
| STANAG 3558 : 2002 | LOCATION OF ELECTRICAL CONNECTORS FOR AIRCRAFT STORES |
| STANAG 3605 : 0 | COMPATIBILITY OF ARMING SYSTEMS AND EXPENDABLE AIRCRAFT STORES |
| MIL-STD-129 Revision R:2014 | Military Marking for Shipment and Storage |
| MIL-F-8785 Revision C:1980 | Flying Qualities of Piloted Airplanes |
| MIL-STD-2088 Revision B:2007 | Bomb Rack Unit (BRU), Single Store, Aircraft |
| STANAG 3791 : 1999 | INTEROPERABILITY OF NATO AIRCRAFT AND STORES - AOP-11 |
| MIL-STD-704 Revision F:2004 | Aircraft Electric Power Characteristics |
| MIL-A-8863 Revision C:1993 | Airplane Strength and Rigidity Ground Loads for Navy Acquired Airplanes |
| STANAG 3837 : 0 | AIRCRAFT STORES ELECTRICAL INTERCONNECTION SYSTEM |
| MIL-STD-220 Revision C:2009 | Method of Insertion Loss Measurement |
| 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-A-8869 Revision B:1987 | Airplane Strength and Rigidity Nuclear Weapons Effects |
| DOD STD 1686 : 0 | ELECTROSTATIC DISCHARGE CONTROL PROGRAM FOR PROTECTION OF ELECTRICAL AND ELECTRONIC PARTS ASSEMBLIES AND EQUIPMENT (EXCLUDING ELECTRICALLY INITIATED EXPLOSIVE DEVICES)(METRIC) |
| STANAG 3525 : 0 | SAFETY DESIGN REQUIREMENTS - AIRBORNE FUZING SYSTEMS |
| MIL-E-6051 Revision D:1967 | Electromagnetic Compatibility Requirements, Systems (S/S by MIL-STD-464) |
| MIL-A-8870 Revision C:1993 | Airplane Strength and Rigidity Vibration, Flutter, and Divergence |
| MIL-STD-1316 Revision F:2017 | Fuze Design, Safety Criteria for |
| MIL-STD-1760 Revision E:2007 | Aircraft/Store Electrical Interconnection System |
| MIL-I-8672 Revision B:1969 | Installation and Test of Aircraft Pyrotechnic Equipment in Aircraft, General Specification for (No S/S Document) |
| STANAG 3898 : 2009 | AIRCRAFT STORES INTERFACE MANUAL (ASIM) - AOP-12 |
| MIL I 23659 : C | INITIATOR, ELECTRIC, GENERAL DESIGN SPECIFICATION |
| MIL-STD-1512 Base Document:1972 | ELECTROEXPLOSIVE SUBSYSTEMS, ELECTRICALLY INITIATED, DESIGN REQUIREMENTS AND TEST METHODS (S/S BY MIL-HDBK-1512) |
| MIL-I-8671 Revision D:1994 | Installation of Droppable Stores and Associated Release Systems |
| MIL C 38999 : J | CONNECTOR, ELECTRICAL, CIRCULAR, MINIATURE, HIGH DENSITY, QUICK DISCONNECT (BAYONET THREADED & BREECH COUPLING) ENVIRONMENT RESISTANT, REMOVABLE CRIMP & HERMETIC SOLDER CONTACTS |
| DOD HDBK 263 : LATEST | ELECTROSTATIC DISCHARGE CONTROL HANDBOOK FOR PROTECTION OF ELECTRICAL AND ELECTRONIC PARTS, ASSEMBLIES AND EQUIPMENT (EXCLUDING ELECTRICALLY INITIATED EXPLOSIVE DEVICES)METRIC |
| STANAG 3575 : 0 | AIRCRAFT STORES EJECTOR RACKS |
| MIL-E-5007 Revision D:1973 | Engine, Aircraft, Turbojet and Turbofan, General Specification for |
| STANAG 3556 : 0 | AIRCRAFT STORE EJECTOR CARTRIDGES |
| MIL-STD-461 Revision G:2015 | Requirements for the Control of Electromagnetic Interference Characteristics of Subsystems and Equipment |
| MIL F 15733 : G | FILTERS & CAPACITORS, RADIO FREQUENCY INTERFERENCE |
| STANAG 3726 : 1996 | BAIL (PORTAL) LUGS FOR THE SUSPENSION OF AIRCRAFT STORES |
| MIL-A-8868 Revision B:1987 | Airplane Strength and Rigidity Data and Reports (No S/S Document) |
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| MIL STD 1763 : A | AIRCRAFT STORES CERTIFICATION PROCEDURES |
| MIL-A-8867 Revision C:1987 | Airplane Strength and Rigidity Ground Tests |
| MIL-D-81303 Revision A:1966 | DESIGN AND EVALUATION OF CARTRIDGES FOR STORES SUSPENSION EQUIPMENT |
| MIL-A-8861 Revision B:1986 | Airplane Strength and Rigidity Flight Loads |
| MIL-A-8866 Revision C:1987 | Airplane Strength and Rigidity Reliability Requirements, Repeated Loads, Fatigue and Damage Tolerance |
| MIL-STD-1472 Revision G:2012 | Human Engineering |
| MIL-STD-1319 Revision A:1976 | ITEM CHARACTERISTICS AFFECTING TRANSPORTABILITY AND PACKAGING AND HANDLING EQUIPMENT DESIGN (S/S BY MIL-HDBK-1319) |
| STANAG 3899 : 0 | GROUND FIT AND COMPATIBILITY CRITERIA FOR AIRCRAFT STORES |
| MIL-D-8708 Revision C:1991 | Demonstration: Aircraft Weapon Systems, General Specification for |
| MIL A 87221 : 0 | AIRCRAFT STRUCTURES, GENERAL SPECIFICATION FOR REQUEST FOR ISSUE OTHER THAN DOD MUST BE SENT VIA; ASD/ENES, WRIGHT-PATTERSON AFB OH 45433-6503 |
| MIL-STD-462 Revision D:1993 | MEASUREMENT OF ELECTROMAGNTIC INTERFERENCE CHARACTERISTICS (S/S BY MIL-STD-461) |
| MIL-B-81006 Revision B:1968 | Bomb, Free Fall, Demonstration of Dispersion Requirements for |
| MIL-H-8501 Revision A:1961 | Helicopter Flying and Ground Handling Qualities, General Requirements for (No S/S Document) |
| MIL-B-5087 Revision B:1964 | Bonding, Electrical, and Lightning Protection, for Aerospace Systems (S/S by MIL-STD-464) |
| MIL-S-8698 Base Document:1954 | STRUCTURAL DESIGN REQUIREMENTS, HELICOPTERS (ASG) (NO S/S DOCUMENT) |
| MIL-STD-1289 Revision D:2003 | AIRBORNE STORES, GROUND FIT AND COMPATIBILITY REQUIREMENTS |
| STANAG 3842 : 2008 | RAIL LAUNCHED MISSILE/LAUNCHER MECHANICAL INTERFACE |
| MIL-M-8856 Revision B:1990 | Missiles, Guided, Structural Integrity General Specification for |
| MIL-A-8860 Revision B:1987 | Airplane Strength and Rigidity, General Specification for |
| MIL-STD-1553 Revision B:1978 | Digital Time Division Command/Response Multiplex Data Bus |
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