Fuze Well Mechanical Interface
- Aerospace Standard
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.
Materials used or their properties.
Physical environment of the weapon.
Explosive interface or features (e.g., insensitive munitions (IM) mitigation).
Torque on the retaining ring or loads on the load bearing surfaces.
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|Aerospace Standard||Network End-to-End Data Link Evaluation System Transceiver Health Monitoring|
|Aerospace Material Specification||Hose, Aircraft Fueling, Acrylonitrile Butadiene (NBR) Rubber Textile Reinforced, Chloroprene Covered Noncollapsing|
Data Sets - Support Documents
|Unnamed Dataset 1|
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.
|AS5716||Standard Electrical and Logical Interface for Airborne Fuzing Systems|
|ASMEY14.5M||This document is not part of the subscrption.|
|FED-STD-H28A||This document is not part of the subscrption.|
|MIL-DTL-38999L||This document is not part of the subscrption.|
|MS27467L||This document is not part of the subscrption.|