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MRC | Criteria | Characteristic |
---|---|---|
AJAF | Unpackaged Unit Length | 9.50 INCHES NOMINAL |
ACUQ | Alternating Current Voltage Rating In Volts | 115 |
FAAZ | Phase | SINGLE |
FREQ | Frequency In Hertz | 400 |
TMDN | Type/Model Designation | CPU194/A |
AJAG | Unpackaged Unit Width | 6.20 INCHES NOMINAL |
AJAH | Unpackaged Unit Height | 6.50 INCHES NOMINAL |
FTLD | Functional Description | PROCESSOR ACCEPTS INPUTS FROM AIRCRAFT FREESTREAM PITOT-STATIC PRESSURE SYSTEM, ANGLE OF ATTACK SENSORS, AIRCRAFT TOTAL TEMPERATURE SENSORS, ENGINE AIR INLET DUCT PITOT-STATIC PRESSURE SYSTEM AND THE ALTIMETER BAROMETRIC SETTING. CORRECTED INPUTS ARE USED TO 1) COMPUTE ACCURATE AIR DATA FOR PRIMARY FLIGHT INSTRUMENTS 2) GENERATE COMMANDS NECESSARY TO CONTROL THE VARIABLE ENGINE INLET GEOMETRY, 3) PROVIDE THE AFCS WITH PITOT PRESSURE, STATIC PRESSURE, AND IMPACT PRESSURE. |
ACUR | Direct Current Voltage Rating In Volts | 26 |
AXQJ | Intelligence Input Method | AIR OR ELECTRICAL |
AXQH | Input Intelligence Type | AIR PRESSURE AND ANGLE OF ATTACK AND AIR TEMPERATURE AND ALTITUDE, GENERAL DATA |
AXQK | Output Intelligence Type | AIR DATA |
AGAV | End Item Identification | F-15S |
SUPP | Supplementary Features | LTECH CHARACTERISTICS: MIL-STD-1750A PROCESSOR, CONTAINS 1553 BUS, BUILT-IN-TEST/3 EXTERNAL FAIL INDICATORS, REQUIRES NO COOLING AIR, PROVIDES PRESSURE SIGNAL OUTPUTS, PROVIDES AIR DATA TO OTHER AIRCRAFT SYSTEMS. |
FEAT | Special Features | THERE ARE 2 DIFFERENT MECHANICAL MOUNTS, 1 USED IN THE EAIC LOCATION AND 1 USED IN THE ADC LOCATION. |
AWZJ | Power Source | EXTERNAL |
MRC | Decoded Requirement | Clear Text Reply |
Guaranteed on-time |
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Customized and |
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Over 5100 |
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Complete Purchasing |