PDF Datasheet | Request Info 

• As the inertial navigation standard by which others are measured, Honeywell produces the QA2000. It is the predominant sensor used in today's commercial and military aircraft strap-down inertial navigation systems. The long-term stability and superior reliability characteristics of the QA2000 make it the best value inertial-grade accelerometer available on the market toady. 

• As with the entire Q-Flex family of accelerometers, the QA2000 features a patented Q-Flex etched-quartz-flexure seismic system. An amorphous quartz proof-mass structure provides excellent bias, scale factor, and axis alignment stability.

• The integral electronics develops an acceleration-proportional output current providing both static and dynamic acceleration measurement. By use of customer supplied output load resistor, appropriately scaled for the acceleration range of the application, the output current can be converted into a voltage. 

• The QA2000 also includes a current-output, internal temperature sensor. By applying temperature-compensating algorithms, bias, scale factor, and axis misalignment performance are dramatically improved. 

FEATURES

APPLICATIONS

• Sets the standard for inertial navigation 

• Excellent turn-on repeatability and stability performance 

• Environmentally rugged 

• Analog output 

• Field-adjustable range 

• Three fastener precision mounting flange 

• Internal temperature sensor for thermal compensation 

• Dual built-in test

• Space Navigation and Control

• Inertial Grade Navigation 

Input range

±60 g

Bias 

<4 mg

Scale factor 

1.33 mA/g ±10%

Axis misalignment

<2 mrad

Resolution/Threshold

<1 µg

Bandwidth

>300 Hz

Operating temperature range

-55 to +95°C

Shock

250 g

Vibration

15 g peak sine, 20-2000 Hz

Input Voltage

±13 to ±18 VDC

Quiescent current

<16 mA per supply

Quiescent power

<480 mW @ ±15 VDC

Weight

71 grams

Size

1.0 in. dia. x 0.97 in. high

Case material

Stainless Steel