Whether you are in search of military and defense parts, aerospace parts, or other similar product solutions, Satellite To Submarine Parts is your one-stop shop. Thank you for your interest in part number 153003-03-01, a Ge Aviation Systems Ltd item that is listed alongside the description “Gyroscope Displacement” and the NSN 6615013264636. To guarantee a swift procurement process for NSN part number 153003-03-01, be sure to request a quote by filling out and submitting the RFQ form below, and one of our experts will offer a customized solution for your comparisons in response.
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We list everything with as much relevant information as possible to ensure that customers can swiftly identify and procure the exact products they need. For instance, while part number 153003-03-01 is manufactured by Ge Aviation Systems Ltd, it is specifically done so under CAGE Code 35351, a unique identifier assigned to a particular facility by the DLA that supplies to various government or defense agencies. Additionally, using the first digits of the NSN 6615-01-326-4636, one can also determine that this part falls under FSC 6615 Automatic Pilot Mechanisms and Airborne Gyro Components. Keeping this in mind, initiate the purchasing process today to see why so many customers depend on us for the NSN items they require.
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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