Parameters |
Mount |
Surface Mount |
Package / Case |
SOT-23-6 |
Number of Pins |
6 |
Pbfree Code |
yes |
Number of Terminations |
6 |
ECCN Code |
EAR99 |
Max Operating Temperature |
85°C |
Min Operating Temperature |
-40°C |
HTS Code |
8542.39.00.01 |
Subcategory |
Power Management Circuits |
Technology |
BICMOS |
Terminal Position |
DUAL |
Terminal Form |
GULL WING |
Peak Reflow Temperature (Cel) |
260 |
Number of Functions |
1 |
Terminal Pitch |
0.95mm |
Time@Peak Reflow Temperature-Max (s) |
40 |
Pin Count |
6 |
Power Supplies |
1.2/5V |
Temperature Grade |
INDUSTRIAL |
Number of Channels |
2 |
Max Supply Voltage |
5.5V |
Min Supply Voltage |
1V |
Analog IC - Other Type |
POWER SUPPLY SUPPORT CIRCUIT |
Power Dissipation-Max |
695mW |
Adjustable Threshold |
NO |
Min Reset Threshold Voltage |
3.51V |
Max Reset Threshold Voltage |
3.69V |
Height Seated (Max) |
1.45mm |
Length |
2.9mm |
Radiation Hardening |
No |
RoHS Status |
RoHS Compliant |
Lead Free |
Lead Free |
MAX6439UTAJRD3+T Overview
The SOT-23-6 package is suitable for it. This device utilizes an analog IC POWER SUPPLY SUPPORT CIRCUIT. There are 2 channels available. Currently, there are 6 pins on it. You can mount this part by using Surface Mount. The minimum supply voltage for this part should not be less than 1V volts. This electrical component is from the Power Management Circuits family. This chip's supplied voltage should not exceed 5.5V volts. This device cannot be activated with a value less than -40°C. The product should be used below 85°C degrees Celsius. Power comes from a 1.2/5V volt source. The pins on it total 6. Reset threshold voltage should be under 3.69V. There should be a minimum reset threshold voltage over 3.51V on the device.
MAX6439UTAJRD3+T Features
Available in SOT-23-6 Package
with 6 Pins
The Min Reset Threshold Voltage at 3.51V
MAX6439UTAJRD3+T Applications
There are a lot of Maxim Integrated MAX6439UTAJRD3+T Battery Management ICs applications.
- Cell phone towers
- Golf carts
- Infotainment/cluster
- Grid power infrastructure
- Estimating the battery’s operational state
- Distributed energy resources
- ADAS ECU
- TFT cluster
- Aviation ground support systems
- ADAS radar