Features
Highest performance accelerometer available
Excellent turn-on repeatability and stability performance
Analog output
Three fastener precision mounting flange
Field-adjustable range
Dual built-in self test
Internal temperature sensor for thermal compensation

Description
We produce the ACC4030 for the highest inertial navigation-grade performance available in today's market. With high inherent quality, reliability, and long-term performance ACC4030 Accelerometer, ACC4030 can be applied in many applications including spacecraft navigation and control systems.

ACC4030 provides an acceleration-proportional output current providing both static and dynamic acceleration measurement. Through the use of a customer supplied output load resistor, appropriately scaled for the acceleration range of the application, the output current can be converted into a voltage. The ACC4030 includes a current-output, internal temperature sensor. Through the use of a temperature-compensating algorithm; Bias, scale factor, and axis misalignment performance is dramatically improved.

Specifications
NO. Performance Parameter Unit
1 Bias(K0) <+/-4 mg
2 Scale Factor(K1) 1.2~1.46 mA/g
3 Second Order Nonlinear Coefficient(K2) about-1.5 ??g/g2
4
Three-month Stability (I??) Bias Stability
(??K0) <30 ??g
Scale Factor Stability (??K1/ K1) <40 ppm
5 Bias Temperature Coefficient(??K0) <+/-25 ??g/degree
6 Scale Factor Temperature Coefficient(??K1/ K1) <+/-40 ppm/degree
7 Range Positive (+IA) max >60 g
Negative (-IA) max >|-60|
8 Misalignment Angle <|+/-1500| urad
9 Insulated Resistance(Ri) >100 M??
10 MeanTime Between Failures ??30000 h
11 Operationg Temperature -40-100degree
12 Shock 100 g
13 Vibration Peak Sine 15 @ 20-2000 Hz g