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Handbook: Standard Electrical and Logical Interface for Airborne Fuzing Systems
- Aerospace Standard
- AIR6234
- Issued
Downloadable datasets available
Annotation ability available
Sector:
Issuing Committee:
Language:
English
Scope
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.
Rationale
SAE AS-1 Technical Committee Aircraft Systems and System Integration, formed SAE AS-1B6, Fuze Systems Task Group, to generate an Aerospace Standard (AS) to support interoperability and interchangeability of airborne weapons and their fuzing systems. This effort was initiated in response to a request made to the SAE AS-1 Technical Committee by the North Atlantic Treaty Organization (NATO) Air Armament Panel for AS-1 to undertake a study or series of studies related to airborne weapons fuzing system standardization.
As a result of this request, Aerospace Standard AS5716 was published in February 2010 and subsequently updated as AS5716A in December 2012, providing definitions for a standard interface for fuzing system incorporated into weapons using MIL-STD-1760, aircraft to weapon interfaces as this is the interface generally employed for all modern airborne weapons of NATO countries.
This Handbook provides background information regarding the rationale and principles of the standard and has been written to give guidance on implementation of the standard.
Recommended Content
| Aerospace Standard | Standard Electrical and Logical Interface for Airborne Fuzing Systems |
| Aerospace Standard | Interface Standard, Common Interface Control Plan |
| Aerospace Standard | Common Launch Acceptability Region Approach Interface Control Document (CLARA ICD) |
Topic
Data Sets - Support Documents
| Title | Description | Download |
|---|---|---|
| Unnamed Dataset 1 | ||
| Unnamed Dataset 2 | ||
| Unnamed Dataset 3 | ||
| Table 1 | Extract from AS5716 ( - Analogue definitions) | |
| Table 2 | Data content for messages with control byte “I” | |
| Table 3 | Structure of the general data frame on the PRES serial data interface | |
| Table 6 | Structure of a PRES subclass AD1 data frame (with data) | |
| Table 7 | Structure of a PRES subclass D1 data frame | |
| Table 8 | Structure of a PRES subclass D2 data frame (initial state) | |
| Table 9 | Structure of a PRES subclass D2 data frame (final state) |
Issuing Committee
AS-1B Aircraft Store Integration Committee
The SAE AS-1 Aircraft Systems & Systems Integration committee addresses all facets of aircraft avionics systems design, maintenance, and in-service experience. It reviews and develops specifications for stores interface, validation requirements, systems integration, mission store validation plans and media terminal design. Also addressed are system test requirements, architecture, security and 1553 data bus standards. The group is comprised of three subcommittees dedicated to creating, preparing, and maintaining all relevant specifications, standards, and requirements for aircraft avionics systems. These subcommittees include:
AS-1A Avionics Networks AS-1B Aircraft-Store Integration AS-1C Avionic Subsystems Participants in the SAE AS-1 committee include OEMs, suppliers, aircraft avionics equipment companies, consulting firms, government and others across the aerospace and defense industries.Reference
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