NSN 6615-01-354-9253
Part Details | DISPLACEMENT GYROSCOPE
6615-01-354-9253 A gyroscope which senses, measures and transmits angular displacement data.
Alternate Parts: K130A0600X, K130A060-0X, 8711371, 871137-1, K130A0600X, K130A060-0X, K130A06003, K130A060-03, K130A0600X, K130A060-0X, 6615-01-354-9253, 01-354-9253, 6615013549253, 013549253
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 66 | MAR 07, 1992 | 01-354-9253 | 20599 ( GYROSCOPE, DISPLACEMENT ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 6615-01-354-9253
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| K130A060-0X | 98255 | DRS SUSTAINMENT SYSTEMS, INC. |
| 871137-1 | 20418 | DRS SUSTAINMENT SYSTEMS, INC.Use CAGE Code 98255 for cataloging |
| K130A060-0X | 20418 | DRS SUSTAINMENT SYSTEMS, INC.Use CAGE Code 98255 for cataloging |
| K130A060-03 | 88818 | KEARFOTT CORPORATIONDBA KEARFOTT |
| K130A060-0X | 88818 | KEARFOTT CORPORATIONDBA KEARFOTT |
Technical Data | NSN 6615-01-354-9253
| Characteristic | Specifications |
|---|---|
| UNIT TYPE | DIRECTIONAL |
| WHEEL POWER METHOD | ELECTRIC |
| CURRENT TYPE | AC/DC |
| FREQUENCY IN HERTZ | 400.0 |
| PHASE | TWO |
| FREEDOM AXIS QUANTITY | 2 |
| GIMBAL QUANTITY | 2 |
| AXIS DISPLACEMENT LIMITATION IN DEG | NON-G-SENSITIVE DRIFT NOT TO EXCEED 25 DEG/R AND G-SENSITIVE DRIFT SHALL BE 10 DEG/HR/G MAXIMUM ABOUT THE INPUT AXIS WITHIN THE PLANE |
| DESIGN TYPE | NONCAGEABLE |
| GIMBAL TORQUE APPLICATION METHOD | AC TORQUE MOTOR |
| TORQUED GIMBAL QUANTITY | 2 |
| SENSING OUTPUT/SIGNAL LEVEL METHOD | SINGLE X AND Y PICKOFF FROM A POSITIVE AND A NEGATIVE COMPARATOR AND PICKOFF EXCITATION THRU A TRANSFORMER |
| TEMP CONTROL METHOD | EXTERNALLY APPLIED |
| INSTRUMENT TYPE | UNFLOATED |
| SHOCK MOUNT | NOT PROVIDED |
| SPECIAL FEATURES | GYRO IS A 2 DEG OF FREEDOM,DRY FLEXURE SUSPENDED TUNED ROTOR GYRO,HERMETICALLY SEALED,WITH SPECIAL ROTATING FLEXURE SUSPENSION MOUNTED TO ONE END OF ROTATING SHAFT. THE FLEXURE SUPPORTS AND PIVOTS THE INERTIAL FLYWHEEL,A COMPENSATOR IS TUNED TO ELIMINATE PIVOT RESTRAINTS,THE OTHER SHAFT END IS DRIVEN BY A SYNCHRONOUS MOTOR. THE VARIABLE INDUCTANCE PICKOFF PROVIDES ELECTRICAL SIGNALS IN PROPORTION TO CASE DISPLACEMENT ANGLES ABOUT ITS 2 ORTHOGONAL AXES |