NSN 6615-00-940-0778
Part Details | DISPLACEMENT GYROSCOPE
6615-00-940-0778 A gyroscope which senses, measures and transmits angular displacement data.
Alternate Parts: 107981, 1079-8-1, 538753519, 53-87535-19, C704101025, 6615-00-940-0778, 00-940-0778, 6615009400778, 009400778
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 66 | NOV 30, 1965 | 00-940-0778 | 20599 ( GYROSCOPE, DISPLACEMENT ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 6615-00-940-0778
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 1079-8-1 | 72314 | BAE SYSTEMS INFORMATION ANDELECTRONIC SYSTEMS INTEGRATION I |
| 53-87535-19 | 76301 | BOEING COMPANY, THEDBA BOEING |
| C704101025 | 88818 | KEARFOTT CORPORATIONDBA KEARFOTT |
Technical Data | NSN 6615-00-940-0778
| Characteristic | Specifications |
|---|---|
| UNIT TYPE | VERTICAL |
| WHEEL POWER METHOD | ELECTRIC |
| CURRENT TYPE | AC |
| VOLTAGE IN VOLTS | 115.0 |
| FREQUENCY IN HERTZ | 400.0 |
| PHASE | SINGLE |
| FREEDOM AXIS QUANTITY | 2 |
| GIMBAL QUANTITY | 2 |
| AXIS DISPLACEMENT LIMITATION IN DEG | PORM 82 DEG FOR PITCH AXIS |
| DESIGN TYPE | CAGEABLE |
| GIMBAL TORQUE APPLICATION METHOD | GT ANY ACCEPTABLE |
| TORQUED GIMBAL QUANTITY | 2 |
| TEMP CONTROL METHOD | SELF-CONTAINED |
| INSTRUMENT TYPE | UNFLOATED |
| SHOCK MOUNT | NOT PROVIDED |
| OVERALL LENGTH | 6.353 INCHES NOMINAL |
| OVERALL DIAMETER | 3.893 INCHES NOMINAL |
