NIIN Output Data
NIIN:
NSN:
Item Name:
SYNCHRO , CONTROL TRANSFORMER
Definition:
A SYNCHRO CONSISTING OF A STATOR AND ROTOR INDUCTIVELY COUPLED. THE ELECTRICAL OUTPUT OF THE ROTOR IS DEPENDENT UPON BOTH THE POSITION OF THE ROTOR AND THE ELECTRICAL INPUT TO THE STATOR FROM A TRANSMITTER SYNCHRO OR A DIFFERENTIAL SYNCHRO. DOES NOT INCLUDE VARIABLE RESISTORS, GONIOMETERS, OR VARIABLE TRANSFORMERS.
Reference/Part Number
| Part Number | CAGE | Status | RNCC | RNVC | DAC | RNAAC | MSDS | SADC |
|---|---|---|---|---|---|---|---|---|
| 23CT4 | 81349 | M | 5 | 1 | E | TX | ||
| CT23-4X2 | 10112 | A | C | 1 | E | ZZ | AF | |
| MIL-S-20708/94 | 81349 | M | 4 | 1 | E | TX | ||
| 23CT4 | 95542 | A | C | 1 | 5 | TX | AF | |
| SM-D-209752-5 | 80063 | A | C | 1 | 5 | TX | AF | |
| 7674821 | 19204 | A | C | 1 | 5 | TX | AF | |
| 7674821 | 81349 | M | 2 | 2 | E | TX | ||
| AY240AA 2 A1 | 55972 | A | C | 1 | 5 | TX | AW | |
| VCT23/36/-4A | 10112 | A | 5 | 9 | 5 | ZZ | ||
| C767482100 | 95542 | A | C | 1 | 5 | TX | AF |
CAGE Information
| Code | Company |
|---|---|
| 10112 | AXSYS TECHNOLOGIES, INC. |
| 81349 | MILITARY SPECIFICATIONS PROMULGATED |
| 95542 | NORTHROP GRUMMAN SYSTEMS CORPORATION |
| 80063 | US ARMY COMMUNICATIONS & ELECTRONICS |
| 19204 | ARMY UNITED STATES DEPARTMENT OF THE |
| 55972 | HONEYWELL INTL INC DEFENSE AVIONICS |
Federal Supply Class
Title
SYNCHROS AND RESOLVERS
Inclusions:
Exclusions:
EXCLUDES SYNCHRO SYSTEMS; SERVO MECHANISMS.
Characteristics (Decoded)
| MRC | Requirements Statement | Clear Text Reply |
|---|---|---|
| ABKK | FLANGE DIAMETER | 2.2490 INCHES MINIMUM AND 2.2500 INCHES MAXIMUM |
| AKAN | SHAFT THREAD CLASS | 3A |
| AJWX | MOUNTING SURFACE TO TERMINAL END DISTANCE | 3.4350 INCHES MINIMUM AND 3.4450 INCHES MAXIMUM |
| ABXF | SHAFT LENGTH | 0.6930 INCHES MINIMUM SINGLE SHAFT AND 0.7190 INCHES MAXIMUM SINGLE SHAFT |
| CQTM | TERMINAL LOCATION | REAR |
| AAVL | PILOT DIAMETER | 0.5900 INCHES MINIMUM AND 0.6000 INCHES MAXIMUM |
| AJVH | MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT | 60.00 |
| AJSL | BODY SIZE | 23 |
| AJWR | SHOULDER LENGTH | 0.2500 INCHES NOMINAL |
| AAVH | SHOULDER DIAMETER | 1.9890 INCHES MINIMUM AND 1.9900 INCHES MAXIMUM |
| CWBH | SHAFT NOMINAL THREAD SIZE | 0.250 INCHES SINGLE SHAFT |
| ABKU | FLANGE THICKNESS | 0.2500 INCHES NOMINAL |
| ABPM | BODY DIAMETER | 1.9900 INCHES MAXIMUM |
| AJVT | ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS | 0.20 INCH-OUNCES MAXIMUM |
| AJWQ | PILOT LENGTH | 0.0460 INCHES NOMINAL |
| AAQL | BODY STYLE | STANDARD ROUND D |
| AJSN | STATOR INPUT VOLTAGE RATING IN VOLTS | 90.0 NOMINAL |
| CQWQ | SHAFT THREAD LENGTH | 0.3100 INCHES NOMINAL SINGLE SHAFT |
| AAZW | SECOND SHOULDER DIAMETER | 1.9985 INCHES MINIMUM AND 1.9995 INCHES MAXIMUM |
| AJYY | SHAFT THREAD SERIES DESIGNATOR | UNF SINGLE SHAFT |
| AJSS | FREQUENCY IN HERTZ | 400.0 NOMINAL |
| AJSQ | STATOR INPUT ELECTRICAL POWER RATING | 240.0 MILLIWATTS MAXIMUM |
| AJSP | STATOR INPUT CURRENT RATING | 6.0 MILLIAMPERES MAXIMUM |
| TTQY | TERMINAL TYPE AND QUANTITY | 7 SCREW |
| AJWV | AFT OF FIRST FLANGE DIAMETER | 1.9985 INCHES MINIMUM AND 1.9995 INCHES MAXIMUM |
| CRSJ | SHAFT TYPE | ROUND, THREADED SINGLE SHAFT |
| CSJY | TRANSFORMATION RATIO | 0.735 ROTOR TO STATOR NOMINAL |
| TEST | TEST DATA DOCUMENT | 81349-MIL-S-16892 SPECIFICATION |
| AJVL | ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | -6.0/+6.0 |
| AAZX | SECOND SHOULDER LENGTH | 0.1700 INCHES NOMINAL |
| AJVG | MAXIMUM FUNDAMENTAL NULL VOLTAGE IN MILLIVOLTS PER VOLT | 30.00 OUTPUT |
| AJVS | ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS | 0.50 INCH-OUNCES MAXIMUM |
| AAFZ | BODY MATERIAL | ALUMINUM |
| ABWV | SHAFT DIAMETER | 0.2402 INCHES MINIMUM SINGLE SHAFT AND 0.2405 INCHES MAXIMUM SINGLE SHAFT |
| ABHP | OVERALL LENGTH | 4.2430 INCHES MINIMUM AND 4.2940 INCHES MAXIMUM |
| AKAF | SHAFT THREAD DIRECTION | RIGHT-HAND SINGLE SHAFT |
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CT23-4X2 ,
CT234X2 ,
5990-00-644-0120 ,
5990006440120 ,
006440120
,
23CT4 ,
CT23-4X2 ,
MIL-S-20708/94 ,
23CT4 ,
SM-D-209752-5 ,
7674821 ,
7674821 ,
AY240AA 2 A1 ,
VCT23/36/-4A ,
C767482100 ,