NSN 6615-01-354-9253 of Gyroscope Displacement - Parts Details
Alternative NSN: 6615013549253 |
Item Name: Gyroscope Displacement |
FSG: 66 Instruments and Laboratory Equipment |
Federal Supply Class (FSC): 6615 Automatic Pilot Mechanisms and Airborne Gyro Components |
NIIN: 013549253 |
NCB Code: USA (01) |
Manufacturers: Drs Sustainment Systems Inc Division |
ASAP Aviation Procurement, owned and operated by ASAP Semiconductor, is the latest parts procurement platform for the aerospace and aviation industry. Check out high demanding part numbers K130A060-0X, 871137-1 under NSN 6615-01-354-9253 of Gyroscope Displacement manufactured by Drs Sustainment Systems Inc Division.
Federal Supply Class of NSN 6615-01-354-9253 is FSC 6615 contains part details of Automatic Pilot Mechanisms and Airborne Gyro Components. Quote for your desired part numbers.
Part Number's List for NSN 6615-01-354-9253, 6615013549253
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Part No Manufacturer Item Name QTY RFQ K130A060-0X Drs Sustainment Systems Inc Division gyroscope displacement Avl RFQ 871137-1 Drs Sustainment Systems Inc Division gyroscope displacement Avl RFQ
Characteristics Data of NSN 6615013549253MRC Criteria Characteristic BBWD Wheel Power Method ELECTRIC BBWH 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 BBWK Torqued Gimbal Quantity 2 BBWN Instrument Type UNFLOATED BBWF Freedom Axis Quantity 2 BBWG Gimbal Quantity 2 APGF Design Type NONCAGEABLE BBWL Sensing Output/Signal Level Method SINGLE X AND Y PICKOFF FROM A POSITIVE AND A NEGATIVE COMPARATOR AND PICKOFF EXCITATION THRU A TRANSFORMER BBWM Temp Control Method EXTERNALLY APPLIED FREQ Frequency In Hertz 400 FAAZ Phase TWO APQB Unit Type DIRECTIONAL MRC Decoded Requirement Clear Text Reply FEAT Special Features GGYRO 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 BBWJ Gimbal Torque Application Method AC TORQUE MOTOR AGBC Shock Mount NOT PROVIDED ACDC Current Type AC/DC
MRC | Criteria | Characteristic |
---|---|---|
BBWD | Wheel Power Method | ELECTRIC |
BBWH | 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 |
BBWK | Torqued Gimbal Quantity | 2 |
BBWN | Instrument Type | UNFLOATED |
BBWF | Freedom Axis Quantity | 2 |
BBWG | Gimbal Quantity | 2 |
APGF | Design Type | NONCAGEABLE |
BBWL | Sensing Output/Signal Level Method | SINGLE X AND Y PICKOFF FROM A POSITIVE AND A NEGATIVE COMPARATOR AND PICKOFF EXCITATION THRU A TRANSFORMER |
BBWM | Temp Control Method | EXTERNALLY APPLIED |
FREQ | Frequency In Hertz | 400 |
FAAZ | Phase | TWO |
APQB | Unit Type | DIRECTIONAL |
MRC | Decoded Requirement | Clear Text Reply |
FEAT | Special Features | GGYRO 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 |
BBWJ | Gimbal Torque Application Method | AC TORQUE MOTOR |
AGBC | Shock Mount | NOT PROVIDED |
ACDC | Current Type | AC/DC |