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pressure values, without any significant warm-up time.
DMA-Aero
Internal 4 hour battery
for safety and versatility
Local back-lit display and
color coded keypad for
laboratory use
Rugged splash proof case
with wheels, stowable
handle and removable lid
Universal power input with
28 VDC Option
USB port for memory
stick
ARINC429, IEEE488 and
Altitude encoder interfaces
available as options
Low power consumption for
high accuracy and reliability
Terminal connector
and RS232 port
Optional Touch Screen Remote Control.
Includes USB port for test program
storage on USB memory
A wide range of pitot-static adaptors and
adaptor kits are available from DMA
Vacuum supply for
static adaptors
Manual vents for
Static and Pitot
Multiple line switching:
4 static, 4 pitot
2 Channels of independent
pressure control for Static and Pitot
Hand terminal provides intuitive
user interface with back-lit
display and color coded keypad
DMA-Aero
MPS34C Standard Specifications
Ongoing development results in specifications
being subject to change without notice
DMA-Aero Representative
11 Old Sugar Hollow Road
Danbury, CT 06812
Tel: 203 790-8371
Fax: 203 743-2051
E-mail: sales@dma-aero.com
Web: www.dma-aero.com
STANDARD TEST FUN CTION S
Pressure/vacuum generation
Automatic leak check
Controlled venting to ambient
Altitude/airspeed input
Static/dynamic(Qc)/total pressure input
Altitude/airspeed rates input
Mach Number input
EPR generation
TAS / IAS toggle, TAS temperature correction
Altitude offset correction
30 user test programmed profiles of
26 steps each
Ultra low speed (2 to 200 kts) for improved accuracy
and stability
USB port for USB memory device to store
results and download test programs
Audible indication when approaching set point
DISPLAYED UNI TS
Altitude: ft, m
Airspeed: kts, km/h, mph
Pressure: InHg, hPa, kPa, Pa, psi, mmHg
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DISPLAY AND KEYPAD
Integral display and keypad in splash proof and
shock protected front panel.
Back lit LCD displays all test parameters.
Hand held remote control unit: 4 x 20
characters LCD with 50 ft extension cable.
CALIBR ATION
One year interval, performed using software.
PHYSICAL SPECIFI CATION S
Weight: 75 lbs. (34 kg.)
Dimensions: L 24.6 x W 19.7 x H 11.7 in.
(L 625 x W 500 x H 300 mm)
Connections: Quick release Hansen fittings.
ENVIRON MENTAL
Temperature range
Operating: -5°C to +50°C
Storage: -20°C to +70°C
Splashproof and shockproof.
CE compliant.
POW ER SUPPLY
Universal power supply: 90-240 VAC; 50-400 Hz.
110 VA
4 hours operation internal rechargeable battery
WARR ANTY
Unit: 2 Years
Pumps: 5000 running hours
OPTION S
A. 28 V d.c. Power supply: (18 to 30 V d.c.)
B. ARINC429 monitoring interface
C. IEEE488 GPIB control (RS232 is standard)
D. PDA and software for wireless
remote control
E. 5+3 multiple isolator (Airbus version)
F. ADWIN PC Control software
L. Touch Screen Remote Control
– Custom Pitot/Static connections available
Ass ociated products
Pitot-static adaptors
Pressure indicators/transfer standards
901
Parame ter
Range Res olution
Acc urac y
Control
Meas ure Control Meas ure Setpoint stabili ty
Stat ic
Altitude (ft) -3,000→99,999 -3,000→80,000 1 1
± 2 @ SL
± 4 @ 30,000
± 15 @ 60,000
± 2
Vertical
speed
Standard (ft/min) 0→6,000 0→6,000 5 @ < 1,500
[2] 1 ± 10 ± 1% of reading
± 10 ± 1%
High rate option [1] (ft/min) 0→30,000 0→30,000 of reading
Static
(inHg abs)
(hPa abs)
0.3→33.3
10→1130
0.8→33.3
71→1130
0.001
0.01
0.001
0.01
± 0.003
± 0.1
± 0.002
± 0.07
Pitot
Airspeed
Standard [3] (kts) 10→850 [3] 10→850 [3] 1 @ < 50
0.1 @ > 50 0.1
± 0.5 @ 50
± 0.1 @ > 500
± 1
Ultra low speed function [4] (kts) 2→200 2→200 0.1 @ > 20 ± 0.001 inHg ± 0.001 inHg
Airspeed slew rate (kts/min) 0→800 0→800 10 10 ± 10 ± 1% of reading ± 5%
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
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