NSN 5990-00-948-9245

Part Details | RECEIVER SYNCHRO

5990-00-948-9245 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.

Alternate Parts: 994529A, 99-4529A, 994529A, 99-4529A, 994529A, 99-4529A, CRH10AS4F205, CRH-10-AS-4/F205, 10TR9489245, 10TR948-9245, 5013650, 5990-00-948-9245, 00-948-9245, 5990009489245, 009489245

Supply Group (FSG) NSN Assigned NIIN Item Name Code (INC)
59APR 11, 196600-948-924502072 ( SYNCHRO, RECEIVER )
REFERENCE DRAWINGS & PICTURES

STANDARD ROUND C

Cross Reference | NSN 5990-00-948-9245
Part Number Cage Code Manufacturer
99-4529A93712ALLIANT DEFENSE ELECTRONICS SYSTEMSINC DBA LUNDY TECHNICAL CENTER
99-4529A75324KILGORE FLARES COMPANY LLC
99-4529A48ZY0MAS COMPONENTS AND COATINGS LLCDIV MAS COMPONENTS & COATINGS, LLC
CRH-10-AS-4/F20599932MOOG INC.DBA MOOG COMPONENTS GROUP
10TR948-92452X130MOTION DEVICES TECHNOLOGY, INC.
501365053711NAVAL SEA SYSTEMS COMMAND
Technical Data | NSN 5990-00-948-9245
Characteristic Specifications
BODY SIZE10
ROTOR INPUT VOLTAGE RATING IN VOLTS26.0 NOMINAL
ROTOR INPUT CURRENT RATING148.0 MILLIAMPERES NOMINAL
ROTOR INPUT ELECTRICAL POWER RATING600.0 MILLIWATTS NOMINAL
FREQUENCY IN HERTZ400.0 NOMINAL
ZRO RESISTANCE IN OHMS27.50 NOMINAL
PLUS J ZRO REACTANCE IN OHMS174.00 NOMINAL
ZSO RESISTANCE IN OHMS7.70 NOMINAL
PLUS J ZSO REACTANCE IN OHMS30.50 NOMINAL
ZRS RESISTANCE IN OHMS47.00 NOMINAL
PLUS J ZRS REACTANCE IN OHMS16.00 NOMINAL
ROTOR DC RESISTANCE IN OHMS16.60 NOMINAL
STATOR DC RESISTANCE IN OHMS7.30 NOMINAL
PHASE SHIFT ANGLE IN DEG5.000 INPUT TO OUTPUT NOMINAL
RECEIVER ERROR ANGULAR RANGE IN MINUTESM30.0/P30.0
ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS5400.00 MILLIMETER-MILLIGRAMS MAXIMUM
ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS2700.00 MILLIMETER-MILLIGRAMS MAXIMUM
BODY STYLE STANDARD ROUND C
SHOULDER DIAMETER0.8118 INCHES MINIMUM AND 0.8123 INCHES MAXIMUM
PILOT DIAMETER0.4995 INCHES MINIMUM AND 0.5000 INCHES MAXIMUM
OVERALL LENGTH1.6160 INCHES NOMINAL
FLANGE DIAMETER0.9360 INCHES MINIMUM AND 0.9370 INCHES MAXIMUM
FLANGE THICKNESS0.0630 INCHES NOMINAL
UNDERCUT DIAMETER0.8400 INCHES NOMINAL
UNDERCUT WIDTH0.0620 INCHES NOMINAL
PILOT LENGTH0.0380 INCHES NOMINAL
SHOULDER LENGTH0.0620 INCHES NOMINAL
MOUNTING SURFACE TO TERMINAL END DISTANCE1.2410 INCHES MAXIMUM
ALIGNMENT HOLE DEPTH0.0500 INCHES MAXIMUM
ALIGNMENT HOLE BOLT CIRCLE DIAMETER0.6780 INCHES NOMINAL
ALIGNMENT HOLE QUANTITY3
TERMINAL TYPE AND QUANTITY5 WIRE LEAD
TERMINAL LOCATION REAR
BODY MATERIAL ALUMINUM
FRAGILITY FACTOR MODERATELY RUGGED