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Standard

Interface Standard, Interface for Micro Munitions
2023-10-06
CURRENT
AS5726A
This standard only defines interconnect, electrical and logical (functional) requirements for the interface between a Micro Munition and the Host. The physical and mechanical interface between the Micro Munition and Host is undefined. Individual programs will define the relevant requirements for physical and mechanical interfaces in the Interface Control Document (ICD) or system specifications. It is acknowledged that this does not guarantee full interoperability of Interface for Micro Munitions (IMM) interfaces until further standardization is achieved.
Standard

Fuze Well Mechanical Interface
2019-09-03
CURRENT
AS5680B
This interface standard applies to fuzes used in airborne weapons that use a 3-in fuze well. It defines: Physical envelope of the fuze well at the interface with the fuze. Load bearing surfaces of the fuze well. Physical envelope of the fuze and its connector. Mechanical features (e.g., clocking feature). Connector type, size, location and orientation. Retaining ring and its mechanical features (e.g., thread, tool interface). Physical envelope of the retaining ring at the interface with the fuze. Physical space available for installation tools. Torque that the installation tool shall be capable of providing. This standard does not address: Materials used or their properties. Protective finish. Physical environment of the weapon. Explosive interface or features (e.g., insensitive munitions (IM) mitigation). Charging tube. Torque on the retaining ring or loads on the load bearing surfaces.
Standard

Validation Methods for MIL-STD-1760B Aircraft Station Interfaces
2017-06-28
CURRENT
AS47641A
This document establishes techniques for validating that an Aircraft Station Interface (ASI) complies with the interface requirements delineated in MIL-STD-1760B Notice 3. For validation of aircraft designed to MIL-STD-1760A Notice 2 AS4764 Issued 1995-04 applies.
Standard

Handbook: Standard Electrical and Logical Interface for Airborne Fuzing Systems
2016-11-18
CURRENT
AIR6234
This Handbook is intended to provide useful information on the application of AS5716A. It is for use by System Program Offices, aircraft prime contractors, avionics and store system designers, system integrators and equipment manufacturers and users. This Handbook was prepared to provide users of the standard of the rationale and principles considered during the development of the standard. It is anticipated that the handbook will serve to assist developers in introducing new technology to achieve compliance with the standard and the underlying principles of the standard. It is intended that the Handbook be used alongside the standard, as it does not contain significant extracts of the standard.
Standard

Interface for Micro Munition (IMM) Handbook
2016-09-16
CURRENT
AIR6114
This document was prepared by the SAE AS-1B1 IMM Task Group to explain and document background information and design decisions made during the development of AS5726. This handbook is published separately to preserve information that is not required or provided in the AS5726 but may be important to system designers to ensure interoperability between the Micro Munition Host and Micro Munition. As a handbook, it cannot be invoked as a requirement in a contract. The structure and numbering of this document mirrors that of AS5726 for the convenience of readers. Headings such as “Requirements” in this handbook should not be interpreted as invoking requirements.
Standard

Interface Standard, Miniature Mission Store Interface
2015-12-19
HISTORICAL
AS5725B
This standard defines implementation requirements for the electrical interface between: a aircraft carried miniature store carriage systems and miniature stores b aircraft parent carriage and miniature stores c surface based launch systems and miniature stores The interface provides a common interfacing capability for the initialization and employment of smart miniature munitions and other miniature stores from the host systems. Physical, electrical, and logical (functional) aspects of the interface are addressed.
Standard

Standard Electrical and Logical Interface for Airborne Fuzing Systems
2012-12-03
CURRENT
AS5716A
This interface standard applies to fuzes/fuzing systems (referred to as fuzing system hereafter) in airborne weapons that use a MIL-STD-1760 type interface. It defines the powers, the discrete signals and the serial data interface for the communications at the interface between the fuzing system and the remainder of the weapon, including the weapon control unit. The Class 1 interface is an electrical only interface that facilitates use of MIL-STD-1760 type platform store interfaces for the fuze to monitor intentional release and defines the fuze interface bus communications protocol to allow sending and receiving data from fuzing systems. Class 2 interfaces add a defined connector and additional interfaces to facilitate the exchange of compatible fuzing systems. Class 3 interfaces add further interface definitions to facilitate the exchange of AS5680A compatible fuzing systems components.
Standard

Technical Architecture for Aircraft, Launcher, and Weapon Interoperability (ALWI TA)
2012-08-27
CURRENT
AIR5720A
The technical architecture defined in this document outlines mandatory, emerging, and needed standards to provide interoperability at key interfaces in the aircraft/store system (including an associated NATO Network Enabled Capability environment), as required to support a future plug-and-play aircraft/store integration capability. These standards relate to services and protocols associated with the subject interfaces. Modeling standards to facilitate the Model Driven Architecture® (MDA®) approach to system definition and implementation are also included. Note that the status of referenced standards as reflected in this document is as of August 2007, and document users should check to see if there has been a subsequent change of status relative to applicable standards.
Standard

Multiplex Data Bus Networks for MIL-STD-1760 Stores
2012-08-22
CURRENT
AIR4013C
This SAE Aerospace Information Report (AIR) will examine network aspects of open and shorted stubs, line reflections and bus loading due to network changes. Single network level is assumed, that is, no carriage store hierarchical levels. However, two passive network coupling variants called "branched bus" and "branched stub" will be introduced that possibly could be used in a stores management network. This report assumes familiarity with MIL-STD-1553B.
Standard

Fuze Well Mechanical Interface
2012-07-25
HISTORICAL
AS5680A
This interface standard applies to fuzes used in airborne weapons that use a 3-in fuze well. It defines: Physical envelope of the fuze well at the interface with the fuze. Load bearing surfaces of the fuze well. Physical envelope of the fuze and its connector. Mechanical features (e.g., clocking feature). Connector type, size, location and orientation. Retaining ring and its mechanical features (e.g., thread, tool interface). Physical envelope of the retaining ring at the interface with the fuze. Physical space available for installation tools. Torque that the installation tool shall be capable of providing. This standard does not address: Materials used or their properties. Protective finish. Physical environment of the weapon. Explosive interface or features (e.g., insensitive munitions (IM) mitigation). Charging tube. Torque on the retaining ring or loads on the load bearing surfaces.
Standard

Validation Methods for MIL-STD-1760B Aircraft Station Interfaces
2012-07-12
HISTORICAL
AS47641
This document establishes techniques for validating that an Aircraft Station Interface (ASI) complies with the interface requirements delineated in MIL-STD-1760B Notice 3. For validation of aircraft designed to MIL-STD-1760A Notice 2 AS4764 Issued 1995-04 applies.
Standard

Interface Standard, Miniature Mission Store Interface
2011-05-24
HISTORICAL
AS5725A
This standard defines implementation requirements for the electrical interface between: a aircraft carried miniature store carriage systems and miniature stores b aircraft parent carriage and miniature stores c surface based launch systems and miniature stores The interface provides a common interfacing capability for the initialization and employment of smart miniature munitions and other miniature stores from the host systems. Physical, electrical, and logical (functional) aspects of the interface are addressed.
Standard

Interface Standard, Interface for Micro Munitions
2009-12-02
HISTORICAL
AS5726
This standard only defines interconnect, electrical and logical (functional) requirements for the interface between a Micro Munition and the Host. The physical and mechanical interface between the Micro Munition and Host is undefined. Individual programs will define the relevant requirements for physical and mechanical interfaces in the Interface Control Document (ICD) or system specifications. It is acknowledged that this does not guarantee full interoperability of Interface for Micro Munitions (IMM) interfaces until further standardization is achieved.
Standard

Fuze Well Mechanical Interface
2009-06-10
HISTORICAL
AS5680
This interface standard applies to fuzes used in airborne weapons that use a 3-Inch Fuze Well. It defines: a Physical envelope of the fuze well at the interface with the fuze. b Load bearing surfaces of the fuze well. c Physical envelope of the fuze and its connector. d Mechanical features (e.g. clocking feature). e Connector type, size, location and orientation. f Retaining ring and its mechanical features (e.g. thread, tool interface). g Physical envelope of the retaining ring at the interface with the fuze. h Physical space available for installation tools. i Torque that the installation tool shall be capable of providing. This standard does not address: j Materials used or their properties. k Protective finish. l Physical environment of the weapon. m Explosive interface or features (e.g. insensitive munitions (IM) mitigation). n Charging tube. o Torque on the retaining ring or loads on the load bearing surfaces.
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