AD844S

量产

Aerospace 60 MHz, 2000V/µS Op Amp

产品技术资料帮助

ADI公司所提供的资料均视为准确、可靠。但本公司不为用户在应用过程中侵犯任何专利权或第三方权利承担任何责任。技术指标的修改不再另行通知。本公司既没有含蓄的允许,也不允许借用ADI公司的专利或专利权的名义。本文出现的商标和注册商标所有权分别属于相应的公司。

Viewing:

概述

  • Wide Bandwidth: 60 MHz at Gain of -1
  • Wide Bandwidth: 33 MHz at Gain of -10
  • Very High Output Slew Rate
  • 20 MHz Full Power Bandwidth typical, 20 V p-p, RL = 500 Ω
  • Fast Settling
  • Differential Gain Error: 0.03% at 4.4 MHz
  • Differential Phase Error: 0.158 at 4.4 MHz
  • Low Quiescent Current: 6.5 mA typical

The AD844 is a high speed monolithic operational amplifier fabricated using Analog Devices' junction isolated complementary bipolar (CB) process. It combines high bandwidth and very fast large signal response with excellent dc performance. Although optimized for use in current to voltage applications and as an inverting mode amplifier, it is also suitable for use in many non-inverting applications.

The AD844 can be used in place of traditional op amps, but its current feedback architecture results in much better ac performance, high linearity and an exceptionally clean pulse response.

This type of op amp provides a closed-loop bandwidth which is determined primarily by the feedback resistor and is almost independent of the closed-loop gain. The AD844 is free from the slew rate limitations inherent in traditional op amps and other current-feedback op amps. Peak output rate of change can be over 2000 V/µs for a full 20 V output step. Settling time is typically 100 ns to 0.1%, and essentially independent of gain. The AD844 can drive 50 Ohm loads to ±2.5 V with low distortion and is short circuit protected to 80 mA.

AD844S
Aerospace 60 MHz, 2000V/µS Op Amp
pdp-image-unavailable
添加至 myAnalog

将产品添加到myAnalog 的现有项目或新项目中(接收通知)。

创建新项目
提问

参考资料

数据手册 1

了解更多
添加至 myAnalog

Add media to the Resources section of myAnalog, to an existing project or to a new project.

创建新项目

软件资源

找不到您所需的软件或驱动?

申请驱动/软件

工具及仿真模型

VRMS/dBm/dBu/dBV计算器

功率测量和信号强度的标准单位之间的换算工具。

打开工具

最新评论

需要发起讨论吗? 没有关于 AD844S的相关讨论?是否需要发起讨论?

在EngineerZone®上发起讨论

近期浏览