FEATURES

¢º 0.010% FS Accuracy
¢º 0.003% FS Precision
¢º Color VGA Screen
¢º User Friendly Interface
¢º Simultaneous Display of Ps and Qc or Ps and Pt

OPTIONS

¢º Helicopter Configuration
¢º Military Configuration
¢º Commercial Configurationl
The Model 8201 Air Data Test Set (ADTS) is a dual channel, precision pressure controller that simulates altitude (Ps) and airspeed (Qc) to test various avionics instruments such as altimeters, air data computers, rate of climb meters and vertical speed indicators. The Model 8201 has the capability of generating and measuring two accurate pressures and pressure rates simultaneously. Each channel utilizes high performance silicon sensors to provide high accuracy and excellent long term stability.

Information for both pressure channels is provided on a color VGA display. Key parameters for both channels are displayed simultaneously so that the user is able to enter separate commands for Ps and Qc. When the ADTS is in operation, there are ten different display screens that provide user information. The main screen provides the following information for each channel: channel data, command pressure, actual pressure and pressure units. After progressing through the setup screen, the operator normally will only use the main screen for active operation of the ADTS.

The internal design of the system allows for either two absolute sensors (Ps and Pt) with Qc being derived or the use of sensors for Ps and Qc where Pt is derived. The accuracy of the pressure readings is 0.010 % of full scale for either sensor configuration.

Specifications Units of Measure 8201-H Helicopter 8201-C Commercial 8201-M Military 8201-S Special Ranges
Sensor Accuracy % fs 0.010 0.010 0.010 0.010
Range - Ps Sensor inHgA 1.6 to 32 1.6 to 35 0.3 to 35 0.3 to 32-35
Range - Altitude Feet -1,700 to 65,000 -4,000 to
65,000
-4,000 to 100,000 Selectable
-4000 to 100,000
Range - Pt Sensor Range - Qc Sensor inHgA inHg 1.6 to 38.5
-0.5 to 10
1.6 to 57
-0.5 to 29
1.6 to 103.5
-0.5 to 75
Within 0 to 122 Within -0.5 to 93
Range - Airspeed @ sea level Knots 10 to 400 20 to 650 20 to 1000 20 to 1100
Max. Range - Qc (dependent on Altitude or Ps setting) inHg 4.5 to 36 22 to 55.3 68.5 to 101.8 varies
Resolution - Ps Channel inHg 0.0001 0.0001 0.0001 0.0001
Resolution - Ps Channel Feet 1 1 1 1
Resolution - Pt/Qc Channel inHg 0.0001 0.0001 0.0001 0.0001
Resolution - Pt/Qc Channel Knots 1 1 1 1
Control Stability % f.s.p. 0.002 0.002 0.002 0.002


Copyright ¨Ï 2002 JungJin Pressure Systems All Rights Reserved.