5990-00-503-0587 SYNCHRO,RECEIVER Index 5990-00-503-0589 SYNCHRO,TRANSMITTER

National Stock Number:
5990-00-503-0588

Federal Supply Class:
5990

National Item Identification Number:
005030588

Description:
SYNCHRO,RECEIVER

Detail:
A SYNCHRO CONSISTING OF A STATOR AND ROTOR INDUCTIVELY COUPLED. THE ROTOR IS FREE TO TURN IN ACCORDANCE WITH THE ELECTRICAL INPUT FROM A TRANSMITTER SYNCHRO OR A DIFFERENTIAL SYNCHRO. DOES NOT INCLUDE VARIABLE RESISTORS, GONIOMETERS, VARIABLE TRANSFORMERS, OR ITEMS WITH DIALS.


Manufacturer Information:
2330-1B55972HONEYWELL INTL INC DEFENSE AVIONICS SYSTEMS
2330-1B96774HONEYWELL INTERNATIONAL INC.
512291J23667SMITHS DETECTION INC.
512291J27914HONEYWELL INTERNATIONAL INC DBA HONEYWELL
512291J55972HONEYWELL INTL INC DEFENSE AVIONICS SYSTEMS
512291J96774HONEYWELL INTERNATIONAL INC.
IF59364HONEYWELL INTERNATIONAL INC.
IF77068ALLIED-SIGNAL INC DBA ALLIED-SIGNAL AEROSPACE CO ELECTRODYNAMICS DIV
MIL-S-2335-8-1F81349MILITARY SPECIFICATIONS PROMULGATED BY MILITARY DEPARTMENTS/AGENCIES UNDER AUTHORITY OF DEFENSE STANDARDIZATION MANUAL 4120 3-M


Techincal Specification:
ROTOR INPUT VOLTAGE RATING IN VOLTS115.0 NOMINAL
ROTOR INPUT CURRENT RATING133.0 MILLIAMPERES NOMINAL
ROTOR INPUT ELECTRICAL POWER RATING3.2 WATTS NOMINAL
FREQUENCY IN HERTZ60.0 NOMINAL
TERMINAL TYPE AND QUANTITY6 SCREW
BODY SIZE23
BODY MATERIALALUMINUM ALLOY
ZRO RESISTANCE IN OHMS183.00 NOMINAL
PLUS J ZRO REACTANCE IN OHMS847.00 NOMINAL
ZSO RESISTANCE IN OHMS176.00 NOMINAL
PLUS J ZSO REACTANCE IN OHMS475.00 NOMINAL
ZRS RESISTANCE IN OHMS392.00 NOMINAL
PLUS J ZRS REACTANCE IN OHMS136.00 NOMINAL
ROTOR DC RESISTANCE IN OHMS136.00 NOMINAL
STATOR DC RESISTANCE IN OHMS204.00 NOMINAL
TRANSFORMATION RATIO0.783 STATOR TO ROTOR NOMINAL
PHASE SHIFT ANGLE IN DEG10.000 INPUT TO OUTPUT NOMINAL
MAXIMUM TEMP RISE25.0 DEG CELSIUS
RECEIVER ERROR ANGULAR RANGE IN MINUTES-90.0 TO 90.0
TORQUE GRADIENT PER ANGULAR DEG0.060 INCH-OUNCES NOMINAL
BODY STYLESTANDARD ROUND, REAR MOUNTING FLANGE
SHOULDER DIAMETER1.2500 INCHES NOMINAL
PILOT DIAMETER1.0625 INCHES NOMINAL
SECOND SHOULDER DIAMETER1.9000 INCHES NOMINAL
SECOND SHOULDER LENGTH0.7000 INCHES NOMINAL
OVERALL LENGTH3.7330 INCHES MAXIMUM
FLANGE DIAMETER2.2500 INCHES MAXIMUM
FLANGE THICKNESS0.2500 INCHES NOMINAL
BODY DIAMETER1.9500 INCHES NOMINAL
PILOT LENGTH0.1250 INCHES NOMINAL
SHOULDER LENGTH0.0250 INCHES NOMINAL
SECOND SHOULDER FACE TO REAR FLANGE DISTANCE1.7000 INCHES NOMINAL
ALIGNMENT HOLE DEPTH0.1560 INCHES MAXIMUM
ALIGNMENT HOLE BOLT CIRCLE DIAMETER0.8440 INCHES NOMINAL
ALIGNMENT HOLE QUANTITY3
SHAFT TYPEROUND, TAPERED, THREADED, UNDERCUT SINGLE SHAFT
SHAFT DIAMETER1.8200 INCHES MINIMUM SINGLE SHAFT
SHAFT LENGTH0.2600 INCHES NOMINAL SINGLE SHAFT
SHAFT UNDERCUT WIDTH0.0200 INCHES NOMINAL SINGLE SHAFT
SHAFT TAPERED END MINOR DIAMETER0.8000 INCHES NOMINAL SINGLE SHAFT
SHAFT TAPER ANGLE IN DEG8.0 SINGLE SHAFT
SHAFT TIP LENGTH0.1500 INCHES NOMINAL SINGLE SHAFT
SHAFT TAPER LENGTH0.1100 INCHES NOMINAL SINGLE SHAFT
SHAFT UNDERCUT DIAMETER0.0990 INCHES NOMINAL SINGLE SHAFT
SHAFT THREAD SERIES DESIGNATORUNF SINGLE SHAFT
SHAFT NOMINAL THREAD SIZE0.112 INCHES SINGLE SHAFT
SHAFT THREAD CLASS2B SINGLE SHAFT
SHAFT THREAD DIRECTIONRIGHT-HAND SINGLE SHAFT
TERMINAL LOCATIONREAR
SHAFT END PLAY0.0150 INCHES MAXIMUM
SHAFT MAXIMUM RUNOUT0.0010 INCHES
SCHEMATIC DIAGRAM DESIGNATOR1 Y-ROTOR, 1 STATOR
FRAGILITY FACTORMODERATELY RUGGED
SPEC/STD CONTROLLING DATA
MANUFACTURERS CODE81349
NON-DEFINITIVE GOVERNMENT SPEC/STD REFERENCEMIL-S-2335-8-1F


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