NSN 6615-01-259-0673
Part Details | DISPLACEMENT GYROSCOPE
6615-01-259-0673 A gyroscope which senses, measures and transmits angular displacement data.
Alternate Parts: 50550, SBU23AA, SBU-23A/A, SBU23AA, SBU-23A/A, MILG83872, MIL-G-83872, 6615-01-259-0673, 01-259-0673, 6615012590673, 012590673
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 66 | JUL 11, 1987 | 01-259-0673 | 20599 ( GYROSCOPE, DISPLACEMENT ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 6615-01-259-0673
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 50550 | 50027 | FLIGHTLINE ELECTRONICS, INC.DBA ULTRA ELECTRONICS, FLIGHTLINE |
| SBU-23A/A | 80058 | JOINT ELECTRONICS TYPE DESIGNATIONSYSTEM |
| SBU-23A/A | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| MIL-G-83872 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
Technical Data | NSN 6615-01-259-0673
| Characteristic | Specifications |
|---|---|
| UNIT TYPE | DIRECTIONAL |
| WHEEL POWER METHOD | ELECTRIC |
| CURRENT TYPE | AC AND DC |
| VOLTAGE IN VOLTS | B115.0$B28.0 |
| PHASE | SINGLE/THREE |
| DIRECT CURRENT RATING IN AMPS | 2.0 |
| FREEDOM AXIS QUANTITY | 2 |
| GIMBAL QUANTITY | 2 |
| AXIS DISPLACEMENT LIMITATION IN DEG | 360 DEGREE ROLL AND +82 DEGREE PITCH |
| DESIGN TYPE | CAGEABLE |
| GIMBAL TORQUE APPLICATION METHOD | EW ANY ACCEPTABLE |
| TORQUED GIMBAL QUANTITY | 2 |
| SENSING OUTPUT/SIGNAL LEVEL METHOD | STANDARD SYNCHRO |
| TEMP CONTROL METHOD | EXTERNALLY APPLIED |
| INSTRUMENT TYPE | UNFLOATED |
| SHOCK MOUNT | PROVIDED |
| OVERALL LENGTH | 10.310 INCHES NOMINAL |
| OVERALL WIDTH | 6.250 INCHES NOMINAL |
| OVERALL HEIGHT | 6.500 INCHES NOMINAL |
| SPECIAL FEATURES | HERMATICLY SEALED CASE, PROVISIONED FOR ROLL AND PITCH, DRIFT WILL NOT EXCEED .25 PER MINUTE AT ROOM TEMPERATURE AND .5 AT TEMPERATURE EXTREMES, SEPARATE BASE, DEVELOPS ELECTRICAL SIGNALS REPRESENTING ROLL AND PITCH TO ATTITUDES INDICATORS AND NAVIGATIONAL EQUIPMENT, CAN REPLACE THE MD-1 AND PB-60 GYROS WHEN THE RESPECTIVE BASES ARE REUSED |