C25d Manual

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  1. C25mshu
  2. Clark C25d Manual
  3. Clark C25d Manual
  4. C25m Aircraft Type
  5. C25m Aircraft

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Aircraft

W T E

C25A – C25M

PO WE R SEM IC O ND UC TO R S

25A AUTOMOTIVE RECTIFIER CELL

Features

!Diffused Junction

!

Low Leakage

B

!

Low Cost

D

!

High Surge Current Capability

!

Die Size 164 mil HEX

E

C

C25mshu

Mechanical Data

!Case: Protected with Silicon Rubber

!Terminal: Slug, Cu with Ag Plated

!Polarity: Indicated by Large Slug On Cathode Side

!Mounting Position: Any

A

C25

Clark C25d Manual

Dim

Min

Max

A

5.46

B

4.82

C

0.75

D

1.0

E

2.2

Aircraft

All Dimensions in mm

Clark C25d Manual

Maximum Ratings and Electrical Characteristics @TA=25°C unless otherwise specified

C25d Manual

C25m Aircraft Type

C25m aircraft

Single Phase, half wave, 60Hz, resistive or inductive load.

C25m Aircraft

For capacitive load, derate current by 20%.

Characteristic

Symbol

C25A

C25B

C25D

C25G

C25J

C25K

C25M

Unit

Peak Repetitive Reverse Voltage

VRRM

Working Peak Reverse Voltage

VRWM

50

100

200

400

600

800

1000

V

DC Blocking Voltage

VR

RMS Reverse Voltage

VR(RMS)

35

70

140

280

420

560

700

V

Average Rectified Output Current

@TC = 150°C

IO

25

A

Non-Repetitive Peak Forward Surge Current

8.3ms Single half sine-wave superimposed on

IFSM

400

A

rated load (JEDEC Method)

Forward Voltage

@IF = 50A

VFM

1.08

V

Peak Reverse Current

IRM

3.0

µA

At Rated DC Blocking Voltage

@TA = 25°C

Typical Thermal Resistance Junction to Ambient

R JA

26

K/W

Operating and Storage Temperature Range

TJ, TSTG

-40 to +150

°C

*Glass passivated forms are available upon request

C25A – C25M

1 of 2

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