Part Details | INERTIAL NAVIGATION SYSTEM
6605-01-477-8931 A self-contained, dead-reckoning system that senses acceleration along the pitch, yaw and roll axis of land vehicle, watercraft or aircraft and calculates the distance from a reference point. They can include INERTIAL NAVIGATION UNIT(s); PLATFORM, INERTIAL; power supplies; subsystems; mode selectors; and control displays.
Alternate Parts: 983533610, 9835336-10, SNU 841, SNU 84-1, CN1656, 6605-01-477-8931, 01-477-8931, 6605014778931, 014778931
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 66 | AUG 22, 2000 | 01-477-8931 | 53295 ( INERTIAL NAVIGATION SYSTEM ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 6605-01-477-8931
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 9835336-10 | 98748 | AIR FORCE UNITED STATES DEPARTMENTOF THE |
| SNU 84-1 | 98748 | AIR FORCE UNITED STATES DEPARTMENTOF THE |
| CN1656 | 80058 | JOINT ELECTRONICS TYPE DESIGNATIONSYSTEM |
Technical Data | NSN 6605-01-477-8931
| Characteristic | Specifications |
|---|---|
| OVERALL LENGTH | 18.097 INCHES NOMINAL |
| OVERALL WIDTH | 7.891 INCHES NOMINAL |
| OVERALL HEIGHT | 7.625 INCHES NOMINAL |
| MOUNTING METHOD | SHELF |
| CURRENT TYPE | AC/DC |
| VOLTAGE IN VOLTS | B115.0$$B28.0 |
| FREQUENCY IN HERTZ | 400.0 |
| PHASE | SINGLE |
| SPECIAL FEATURES | SOLID STATE 3 RING LASER GYROSCOPES AND 3 ACCELEROMETERS |
| NUCLEAR HARDNESS CRITICAL FEATURE | HARDENED |
| FUNCTIONAL DESCRIPTION | SENSES AND OUTPUT 3 ORTHOGONAL AXIS OF LINEAR AND ROTATIONAL ACCELERATION,VELOCITY ACCELERATION |
| TYPE/MODEL DESIGNATION | CN1656 |
| REFERENCE DATA AND LITERATURE | DRAWING 9835336 AND TYPE DESIGNATOR CN-1656 |