Type E-1 Electrical Media Interface Characteristics
- Aerospace Standard
The physical media interface: This slash sheet specifies the characteristics of the electrical interface to the physical bus media.
The minimum and maximum timing requirements for operation of this implementation of the LTPB.
The data coding used to encode and decode the data for transmission.
The default values to be loaded into the timers of the LTPB interface at power-up prior to intervention by the host processor.
|Aerospace Standard||S400 Copper Media Interface Characteristics Over Extended Distances|
|Aerospace Standard||IEEE-1394b Interface Requirements for Military and Aerospace Vehicle Applications|
Data Sets - Support Documents
|TYPE E-1||ELECTRICAL MEDIA INTERFACE CHARACTERISTICS|
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.