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opa111bm Related Information

Design and Implementation of Full Static Pressure Detection System for Aircraft

5/15/2023 12:07:02 PM

Design and Implementation of Full Static Pressure Detection System for Aircraft [Date: 2005-7-31] Source: Author of Electronic Technology Application: Dai Zhongwanming [Font: Size, Size] Summary: The design of Full Static Pressure Automatic Detection System for Aircraft based on Vibrating Barrel Pressure Sensor is introduced, the structure and working principle of the system are discussed, and the hardware circuit and software design of the system are explained. System Design

opa111bm DataSheet Download Figures and information are for reference only, subject to actual PDF
  • Standard Packaging:One
  • Category:Integrated Circuit (IC)
  • Family:Linear - Amplifiers - InstrumentationOP AmpsBuffer Amps
  • Series:Difet&Reg;
  • Amplifier Type:Instrument
  • Number Of Circuits:One
  • Type Of Output:-
  • Conversion Rate:2 V/&Micro; S
  • Gain – Bandwidth Product:2MHz
  • -3dB Bandwidth:-
  • Current Input Bias:0.5pA
  • Voltage Input Offset:50&Micro; V
  • Current - Power Supply:2.5mA
  • Current - Output/Channel:10mA
  • Voltage Power Supply, Single/Dual (&Plusmn;):&Plusmn; 5 V~18 V
  • Working Temperature:-25&Deg; C~85&Deg; C
  • Installation Type:Through-Hole
  • Packaging/Housing:TO-99-8 Metal Can
  • Supplier Equipment Packaging:TO-99-8
  • Packing:Pipe Fittings

opa111bm DataSheet Download

OPA111BM