SBU-23A-A Manufactured by Joint Electronics Type Designation - Order Online

Part Number:  SBU-23A-A
Alternate P/N:  SBU23AA
Item Name :  gyroscope displacem
CAGE Code:  80058
INC Code:  20599
Country:  USA
NCB Code:  01
FSG:  66 Instruments and Laboratory Equipment
The NSN Part SBU-23A-A Gyroscope Displacem is ready-to-ship today! Please request a quote by filling out the form. All fields are important. The NSN number for SBU-23A-A is 6615-01-326-4636. The manufacturer of this part is Joint Electronics Type Designation. A dedicated customer service executive will contact you within 15 minutes of receiving the RFQ.

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Disclaimer: This is a quotation for the goods listed above. This quotation is meant as an estimate and does not reflect a final bill or invoice. All quotations are subject to change until acceptance by ASAP Semiconductor of a binding Purchase Order, and quotations may be withdrawn or revised at the sole discretion of ASAP Semiconductor. This quotation is subject to the ASAP Semiconductor Terms & Conditions available at https://www.asapsemi.com/customer-terms-and-conditions/ . All United States Government and Department of Defense bids are quoted as CAGE code 6RE77 from ASAP Semiconductor’s Anaheim, California facility. Any quotation from ASAP Semiconductor without 6RE77 is void.

Characteristics Data of NSN 6615-01-326-4636, 6615013264636

MRCCriteriaCharacteristic
ELECVoltage In Volts115.0 OR 28.0
ACUTDirect Current Rating In Amps2
BBWDWheel Power MethodELECTRIC
BBWGGimbal Quantity2
BBWKTorqued Gimbal Quantity2
BBWMTemp Control MethodEXTERNALLY APPLIED
BBWHAxis Displacement Limitation In Deg360 DEGREE ROLL AND +82 DEGREE PITCH
BBWJGimbal Torque Application MethodSYNCHRO MOTOR
BBWNInstrument TypeUNFLOATED
ABMKOverall Width6.250 INCHES NOMINAL
ABKWOverall Height6.500 INCHES NOMINAL
FAAZPhaseSINGLE/THREE
FEATSpecial FeaturesHERMATICLY 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
APGFDesign TypeCAGEABLE
BBWFFreedom Axis Quantity2
BBWLSensing Output/Signal Level MethodSTANDARD SYNCHRO
MRCDecoded RequirementClear Text Reply
ACDCCurrent TypeAC AND DC
APQBUnit TypeDIRECTIONAL
AGBCShock MountPROVIDED

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