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MRC | Criteria | Characteristic |
---|---|---|
AGAV | III END ITEM IDENTIFICATION | AN/ASQ-184,B-1B AIRCRAFT |
ELEC | VOLTAGE IN VOLTS | 26.0 AND 115.0 |
FTLD | III FUNCTIONAL DESCRIPTION | PRIME SENSOR FOR AIRCRAFT VELOCITY,DELTA VELOCITY,ATTITUDE AND HEADING INFO. AND PROVIDES ALL FUNCTIONS NECESSARY FOR INERTIAL NAVIGATION INCLUDING SELF-CONTAINED ALIGNMENT AND GENERATION OF PRESENT POSITION DATA; PRIMARY INPUT/OUTPUT INTERFACE IS MIL-STD-1553B MUX BUS WHICH PERMITS COMMUNICATION WITH AN AVIONICS PROCESSOR (AP) |
FREQ | FREQUENCY IN HERTZ | 400.0 |
ABHP | OVERALL LENGTH | 18.100 INCHES NOMINAL |
FEAT | SPECIAL FEATURES | ADDITIONAL POWER 28 VDC; ROLL 876.5 LBS SQUARE INCH, YAW 953.4 LBS SQUARE INCH, PITCH 245.5 LBS SQUARE INCH |
ABKW | OVERALL HEIGHT | 7.900 INCHES NOMINAL |
ABMK | OVERALL WIDTH | 7.900 INCHES NOMINAL |
ACDC | CURRENT TYPE | AC |
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