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Datalogger for IAQ Analysis
HD37AB1347
Datalogger for indoor air quality analysis (IAQ). Measurement of airspeed, temperature, relative humidity, atmospheric pressure, CO² and CO.
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Pressure Pump / Vacuum Pump
Model Model 82
The Mensor Model 82 is a pump and/or compressor set that complements a pressure controller and fits on or under a bench, in a rack, or on a table. The compressor is an oil-less pump with a maximum pressure of 50 psi with a open flow of 1.5 cfm. The vacuum pump is also oil-less and can achieve 28.5 inHG of vacuum with an open flow of 0.8 cfm. In avionics terms, this set is capable of 60,000 feet of altitude and airspeeds in excess of 1000 knots. Both units are shock mounted to reduce noise and vibration. Each unit has a power switch/breaker and can be run independently. This same configuration can also be produced in a standard 19 inch, 4U (7” high) rack mount chassis or desktop version.
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Active Air Speed Transmitter
HD103T.0
Active air speed transmitter with hotwire sensor. Probe with 5m cable. Speed 0.1…5 m/s. Outputs for temperature and airspeed.
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Air Data Calibrator
ADC-2500V3
TestVonics ADC-2500V3 Air Data Calibrator is a high accuracy pitot static air dat calibrator. The calibrator is capable of controlling and measuring Altitude and Airspeed pressures with the highest degree of accuracy. The control and measurement ranges and accuracies of the calibrator meet and/or exceed requirements for both commercial and military applications . Currently all USAF PMEL organizations are standardizing their ADC-2500 calibrators to V3.
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Air Data Test Sets
For calibrating altimeters, airspeed indicators, rate-of-climbindicators and other avionic instruments.
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All Measurements 3 Channel Portable Data Logger
DO9847
Combinations of all measurements in 3 channel portable datalogger: RH, temperature, pressure, airspeed, light, voltage and current.
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Air Data
Testing altitude and airspeed components in commercial and military air data applications are critical for the safety and performance of an aircraft. Mensor air data test set and indicators provide the high accuracy necessary for these applications. Air Data Test Sets control altitude /altitude rate and airspeed /airspeed rate, for testing altimeters and airspeed indicators or air data computers in a dynamic way that simulates actual flying conditions. Air data Indicators measure Altitude /Altitude Rate and Airspeed /Airspeed Rate for applications where conditions are externally controlled.
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Mach Airspeed Test Fixture
TA-6055A
The TA-6055A is a Mach Airspeed Test Fixture built to support the testing and repair of the 2082 and 2083 series of Servoed Mach Airspeed Indicators (SMASI) used in some Boeing aircraft. These mach airspeeds are synchro driven and require a coarse and fine input for altitude and a third input for airspeed. This test fixture was designed around the test procedure and is interfaced with our TA-1001 panel which provides for two of the synchro sources and two Angle Position Indicators (API).
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Portable Testing Kit for Gulfstream Aircraft
ES-429TK-101
The ES-429TK-101 Portable Testing Kit (for Gulfstream aircraft) enables you to simulate Airspeed, Altitude and Radio Height values over an ARINC 429 bus. The ES-429TK-101 Portable Testing Kit consists of a DAS-429UNET/RT10, battery and the Exc429Tester application that runs on the host computer, a laptop or desktop PC running Windows. Using the ES- 429TK-101 Portable Testing Kit with a laptop provides a portable testing system.
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Standard Airspeeds
These airspeed indicators have unrestrained movements.These instruments are actuated by ram air and ambient atmospheric pressure obtained from the aircraft pitot and static pressure systems. A moveable pointer and a fixed dial indicate airspeed with the zero index at the 12 o??lock position. Temperature compensation is internal and there is no external zero adjustment. Pointer damping is internally adjustable.
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Restrained Airspeeds
These airspeed indicators have restrained movements.These instruments are actuated by ram air and ambient atmospheric pressure obtained from the aircraft pitot and static pressure systems. A moveable pointer and a fixed dial indicate airspeed with the zero index at the 12 o’clock position. Temperature compensation is internal and there is no external zero adjustment. Pointer damping is internally adjustable.
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True Airspeeds
These true speed indicators are differential pressure indicators that measure the difference between static and total pressure produced by ram air from the pitot. The indicated airspeed can be corrected for changes in altitude by turning the knob to align the outside air temperature with the altitude. The moveable airspeed scale will then show the actual, or true, airspeed.
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Airspeed Warning Switches
Supply Voltage: 10÷30 Volts DC Current Rating: 200 mA max Switching Power: 5 A max 30VDC Temperature Range: -40° C to 120° C Pressure Fitting: 1/8" plastic Weight: 3.2 oz.
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TSO'd Airspeed
Airspeed Indicator is intended for use on an aircraft to indicate the speed relative to the air at sea level and at any other altitude, to indicate the equivalent speed corresponding to the actual force of the air.
