This standard defines the mechanical interface and specifies provisions for the electrical and environmental connectors between the host aircraft (“platform”) and a turreted electro-optic/infrared (EO/IR) sensor.
Rationale:
This document was created to standardize the mechanical interface between aircraft and Electro-Optic (EO)/Infrared (IR) sensors. This activity was initiated at the request of the U.S. Navy in 2009.
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Related Topics:
Fiber optics
Fixed-wing aircraft
Unmanned aerial vehicles
Radio frequency
Center of gravity (CG)
Connectors and terminals
Metal finishing
Also known as: SAE AS 6169
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