Special Features
Mounting: hard mounted; material: aluminum alloy case; provides outputs of acceleration, velocity, position, heading, attitude (pitch and roll), attitude rates (pitch, roll, azimuth) and time, pitch and roll synchro (analog), baro inertial altitude (when provided with barometric altitude data); performs rapid reaction, sotred heading alignments, rapid reaction alignment of a degraded accuracy (attitued heading reference system) mode with outputs of heading, attitude, angular rate and acceleration
Description
11.780 inches nominal overall length.
Overall Height
6.530 inches
Overall Width
8.150 inches
Current Type
Ac
End Application
Inertial navigation system f-16, a-10, fb-111, c-130, rf4c, ef-111 aircraft
Voltage In Volts
115.0 and 200.0
Phase
Single
Frequency In Hertz
400.0
Functional Description
Provides a self contained fully automatic strapdown inertial reference for piloting and navigating an aircraft
