| Mfg Part Number: SBU-23A-A | Alternate P/N: SBU23AA | Manufacturer: Joint Electronics Type Designation |
| NSN : 6615-01-326-4636 | NIIN : 013264636 | Item Name : Gyroscope Displacem |
| CAGE Code : 80058 | FSC : 6615 Automatic Pilot Mechanisms and Airborne Gyro Components |
Thank you for taking an interest in the various military NSN parts and aerospace parts we offer on our website. You have currently taken interest in part number SBU-23A-A, a Joint Electronics Type Designation item produced under CAGE Code 80058. For further identification purposes, part number SBU-23A-A is also listed with the NSN 6615013264636, and it is organized under Federal Supply Class (FSC) 6615 Automatic Pilot Mechanisms and Airborne Gyro Components for ease of procural. By filling out and submitting the form provided below, you will be able to receive purchasing options on this item directly from our staff. For us to best tailor our presented solution to your unique needs and restrictions alike, we ask that you please offer our team details like your desired quantity, target pricing, and expected fulfillment timeframe. We can even accommodate many time constraints and limitations that customers may face, so be sure to let us know of any requests when you submit an RFQ form for part number SBU-23A-A.
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| MRC | Criteria | Characteristic |
|---|---|---|
| ELEC | Voltage In Volts | 115.0 OR 28.0 |
| ACUT | Direct Current Rating In Amps | 2 |
| BBWD | Wheel Power Method | ELECTRIC |
| BBWG | Gimbal Quantity | 2 |
| BBWK | Torqued Gimbal Quantity | 2 |
| BBWM | Temp Control Method | EXTERNALLY APPLIED |
| BBWH | Axis Displacement Limitation In Deg | 360 DEGREE ROLL AND +82 DEGREE PITCH |
| BBWJ | Gimbal Torque Application Method | SYNCHRO MOTOR |
| BBWN | Instrument Type | UNFLOATED |
| ABMK | Overall Width | 6.250 INCHES NOMINAL |
| ABKW | Overall Height | 6.500 INCHES NOMINAL |
| FAAZ | Phase | SINGLE/THREE |
| FEAT | 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 FOR USE BY THE ATTITUDE INDICATORS AND NAVIGATIONAL EQUIPMENT, REPLACES THE MD-1 AND PB-60 AUTOPILOT GYRO EHEN THE RESPECTIVE BASES ARE USED |
| APGF | Design Type | CAGEABLE |
| BBWF | Freedom Axis Quantity | 2 |
| BBWL | Sensing Output/Signal Level Method | STANDARD SYNCHRO |
| MRC | Decoded Requirement | Clear Text Reply |
| ACDC | Current Type | AC AND DC |
| APQB | Unit Type | DIRECTIONAL |
| AGBC | Shock Mount | PROVIDED |
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