871137-1 by Drs Sustainment Systems Inc Division with NSN 6615013549253 - Submit a Quote
| Part No. : 871137-1 | Alternate P/N: 8711371 | Manufacturer : Drs Sustainment Systems Inc Division | NSN : 6615-01-354-9253 |
| Item Name : Gyroscope Displacement | CAGE Code : 20418 | FSC : 6615 Automatic Pilot Mechanisms and Airborne Gyro Components |
ASAP Aviation Procurement is pleased to announce that part number 871137-1 of NSN 6615013549253 is now available and in stock. We can get you one of the fastest and most competitive quotes on this part. Part number 871137-1 is a gyroscope displacement manufactured by drs sustainment systems inc division under CAGE Code 20418. Simply fill out the Request for Quote (RFQ) form provided here to get started on your quote.In order to make sure that we get you your quote in a timely manner, please take the time to make sure that all fields are completely filled out, particularly the asterisk-marked (*) fields like Parts Needed By and Quantity (ea).
We will be using your response to these fields to calculate your quote. Within 15 minutes of receiving your RFQ, a member of our sales team will contact you with your quote. ASAP Aviation Procurement, owned and operated by ASAP Semiconductor, is a leading distributor of new and obsolete NSN parts for the aerospace, civil aviation, and defense industries. With our inventory of more than 2 billion parts sourced from over 5000 manufacturers from around the world, we do our level best to become your go-to one-stop shop. And to help us offer you the best streamlined parts procurement experience, we have advanced shipping facilities across USA. 871137-1 drs sustainment systems inc division is in stock.
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Characteristics Data of NSN 6615-01-354-9253, 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 |
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