NSN 6605-01-339-9252
Part Details | NAVIGATION INERTIAL REFERENCE UNIT
6605-01-339-9252 An electromechanical and/or electronic device, consisting of sensors, accelerometers, gyroscopes for the pitch, roll and yaw axis, and a processor, to provide velocity and angular position data. May be a component of an INERTIAL NAVIGATION UNIT.
Alternate Parts: 34084500001, 34084500-001, 34084574, 34084500503, 34084500-503, 34084500502, 34084500-502, 34084500001, 34084500-001, ARU63A, ARU-63/A, 6605-01-339-9252, 01-339-9252, 6605013399252, 013399252
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 66 | JUN 04, 1991 | 01-339-9252 | 52472 ( INERTIAL REFERENCE UNIT, NAVIGATION ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 6605-01-339-9252
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 34084500-001 | 94988 | COOPER INDUSTRIES INCCHAMPION AVIATION PRODUCTS |
| 34084574 | 0BFA5 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| 34084500-503 | 0BFA5 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| 34084500-502 | 0BFA5 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| 34084500-001 | 0BFA5 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| ARU-63/A | 80058 | JOINT ELECTRONICS TYPE DESIGNATIONSYSTEM |
Technical Data | NSN 6605-01-339-9252
| Characteristic | Specifications |
|---|---|
| OVERALL LENGTH | 18.100 INCHES NOMINAL |
| OVERALL WIDTH | 8.000 INCHES NOMINAL |
| OVERALL HEIGHT | 9.120 INCHES NOMINAL |
| CURRENT TYPE | DC |
| SPECIAL FEATURES | STRAPDOWN SYSTEM; UTILIZES RING LASER GYROS; DUAL DIGITAL INTERFACE (2 REMOTE TERMINALS); ONE INTERFACES WITH MISSION BUS; ONE INTERFACES WITH EFCS BUS; BUILT-IN BATTERY CHARGER; 28 VDC FROM AIRCRAFT POWER; 28 VDC FROM BATTERY; RACK MOUNTED; ELECTROSTATIC DISCHARGE SENSATIVE |
| FUNCTIONAL DESCRIPTION | THE INERTIAL REFERENCE UNIT UTILIZES A SET OF ACCELEROMETERS AND RING LASER GYROS TO SENSE AIRCRAFT RATES AND ACCELERATIONS, COMPUTES AND PROVIDES AIRCRAFT ATTITUDE, ATTITUDE RATES, TRUE HEADING, VELOCITY, ACCELERATION AND POSITION INFORMATION TO THE C-17 MISSION COMPUTER FOR NAVIGATION AND DISPLAY PURPOSES; ATTITUDE RATES, HEADING, GROUND SPEED, FLIGHT PATH ANGLE, INERTIAL ANGLE OF ATTACK (AOA), AOA RATE, SIDE SLIP ANGLE AND SIDE SLIP ANGLE RATE |
| END ITEM IDENTIFICATION | C-17 AIRCRAFT |
