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Pressure Transducers APT-20-1000 - Kulite


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dkulite
AIRCRAFT PRESSURE TRANSDUCER
APT-20-1000 (100mV Output) APT-51-1000 Differential (100mV Output) APTE-6-1000 (5V Output) APTE-51-1000 Differential (5V Output)
• High Natural Frequencies
• Unprecedented Stability And Reliability To High Temperatures
Ruggedized Internal Construction
• Leakproof, All Welded Construction
No Leak After Exposure To 2000°F (1093°C)
• Utmost In Safety
Secondary Containment Of Pressure Media
• Fully Qualified
Passed Extensive Environmental Tests
• FAA Authorization TSO-C47
• FAA Manufacturer's Maintenance Facility
SPECIFICATIONS
UNAMPLIFIED APT-SERIES
10VDC Regulated
AMPLIFIED APTE-SERIES
28VDC ± 4V
Excitation
Output
100mV (Typ.)
5VDC Diff. or Single Ended
Power Consumption
100mW (Typ.)
280mW (Typ.)
Input Impedance
1000 Ohms (Min.)
N/A
Output Impedance
2000 Ohms (Max.)
100 Ohms (Max.)
Operating Temperature Range
-65° F to 300° F (-55° C to 150° C)
-65° F to 250° F (-55° C to 120° C)
Weight
Gage and Absolute Versions Differential Version
0.3 Lb. (Max.) 0.45 Lb. (Max.)
0.37 Lb. (Max.)
0.6 Lb. (Max.)
Case Outline Gage and Absolute Versions Differential Version
Case Length May Vary With Range, Measuring Mode, Pressure Port And Connector
Construction Materials
316 SS And 17-4 PH SS
Pressure Range
To Specification 0-15 PSI to 0-5000 PSI (0-1.0 BAR to 0-350 BAR) (Typ.)
Proof Pressure
2 Times Rated Pressure Range
Burst Pressure
5 Times Rated Pressure Range
Insulation Resistance
100 Megohms Min. @ 50VDC
Mounting Torque
75 Inch-pounds (Max.)
75 Inch-pounds (Max.)
Total Error Band
Includes Linearity, Hysteresis, Repeatability, Mounting Error and Vibration Efffects, Thermal Errors Within The Compensated Temperature Range, As Well As Normalization Errors of Zero and Full Scale. (See Fig I and II For Typical Cases)
Resolution
Infinitesimal
MTBF
At Least 30,000 Hours
Fluid Temperature
-65° F to 300° F (-55° C to 150° C)
Storage Temperature Range (Non Operating)_
-65° F to 185° F (-55° C to 85° C)
Altitude-Operating
Up To 51,000 Feet
Media Compatability
JP-4 and JP-5 Grade Aviation Turbine Fuel Per MIL-T-5624, Hydraulic Fluid Per MIL-H-5606, MIL-H-83282, Engine and Transmission Lubrication Oil Per MIL-L-7808 and MIL-L-23699 and Aviation Gasoline Per MIL-G-5572 All Grades
Humidity
100% Relative Humidity
Acceleration
Operational After Being Subjected to "G" Levels of 12 "G"s Per MIL-STD-810C, Method 513.2 Procedure 1
Linear Vibration
50g Peak, Sine 10 to 2000 Hz
Mechanical Shock
100g half Sine Wave 1 msec. Duration
Electromagnetic Interference
apte series: Meets RTCA DO-160 Sections 18, 19, and 21 All Cat. A, Section 20 Cat. U. (With Shielded Cable)
Electrical Spike Protection
apte series: Unit Satisfies Power Input and Voltage Spike Conducted DO-160 Sections 16 and 17. Power Input Test 16 Voltage Spike Conducted test 17
Note: Custom pressure ranges, accuracies and mechanical configurations available.
Continuous development and refinement of our products may result in specification changes without notice - all dimensions nominal. (B)
KULITE SEMICONDUCTOR PRODUCTS, INC. • One Willow Tree Road • Leonia, New Jersey 07605 • Tel: 201 461-0900 • Fax: 201 461-0990 • http://www.kulite.com

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