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IRHM3064PBF

Description
Power Field-Effect Transistor, 35A I(D), 60V, 0.021ohm, 1-Element, N-Channel, Silicon, Metal-oxide Semiconductor FET, TO-254AA
CategoryDiscrete semiconductor    The transistor   
File Size268KB,8 Pages
ManufacturerInternational Rectifier ( Infineon )
Websitehttp://www.irf.com/
Environmental Compliance  
Download Datasheet Parametric View All

IRHM3064PBF Overview

Power Field-Effect Transistor, 35A I(D), 60V, 0.021ohm, 1-Element, N-Channel, Silicon, Metal-oxide Semiconductor FET, TO-254AA

IRHM3064PBF Parametric

Parameter NameAttribute value
Is it lead-free?Lead free
Is it Rohs certified?conform to
MakerInternational Rectifier ( Infineon )
package instructionFLANGE MOUNT, S-CSFM-P3
Reach Compliance Codecompliant
ECCN codeEAR99
Avalanche Energy Efficiency Rating (Eas)500 mJ
ConfigurationSINGLE WITH BUILT-IN DIODE
Minimum drain-source breakdown voltage60 V
Maximum drain current (ID)35 A
Maximum drain-source on-resistance0.021 Ω
FET technologyMETAL-OXIDE SEMICONDUCTOR
JEDEC-95 codeTO-254AA
JESD-30 codeS-CSFM-P3
Number of components1
Number of terminals3
Operating modeENHANCEMENT MODE
Maximum operating temperature150 °C
Package body materialCERAMIC, METAL-SEALED COFIRED
Package shapeSQUARE
Package formFLANGE MOUNT
Peak Reflow Temperature (Celsius)260
Polarity/channel typeN-CHANNEL
Maximum pulsed drain current (IDM)284 A
Certification statusNot Qualified
surface mountNO
Terminal formPIN/PEG
Terminal locationSINGLE
Maximum time at peak reflow temperature40
transistor applicationsSWITCHING
Transistor component materialsSILICON
PD - 91564D
RADIATION HARDENED
POWER MOSFET
THRU-HOLE (T0-254AA)
Product Summary
Part Number Radiation Level
IRHM7064
100K Rads (Si)
IRHM3064
300K Rads (Si)
IRHM4064
600K Rads (Si)
IRHM8064
1000K Rads (Si)
IRHM7064
JANSR2N7431
60V, N-CHANNEL
REF:MIL-PRF-19500/663
RAD Hard HEXFET
TECHNOLOGY
™
®
QPL Part Number
R
DS(on)
I
D
0.021Ω 35*A JANSR2N7431
0.021Ω 35*A JANSF2N7431
0.021Ω 35*A JANSG2N7431
0.021Ω 35*A JANSH2N7431
TO-254AA
International Rectifier’s RADHard HEXFET
®
technol-
ogy provides high performance power MOSFETs for
space applications. This technology has over a de-
cade of proven performance and reliability in satellite
applications. These devices have been character-
ized for both Total Dose and Single Event Effects (SEE).
The combination of low Rdson and low gate charge
reduces the power losses in switching applications
such as DC to DC converters and motor control. These
devices retain all of the well established advantages
of MOSFETs such as voltage control, fast switching,
ease of paralleling and temperature stability of elec-
trical parameters.
Features:
!
!
!
!
!
!
!
!
!
Single Event Effect (SEE) Hardened
Low R
DS(on)
Low Total Gate Charge
Proton Tolerant
Simple Drive Requirements
Ease of Paralleling
Hermetically Sealed
Ceramic Package
Light Weight
Absolute Maximum Ratings
Parameter
ID @ VGS = 12V, TC = 25°C Continuous Drain Current
ID @ VGS = 12V, TC = 100°C Continuous Drain Current
IDM
PD @ TC = 25°C
VGS
EAS
IAR
EAR
dv/dt
TJ
TSTG
Pulsed Drain Current
Max. Power Dissipation
Linear Derating Factor
Gate-to-Source Voltage
Single Pulse Avalanche Energy
Avalanche Current
Repetitive Avalanche Energy
Peak Diode Recovery dv/dt
Operating Junction
Storage Temperature Range
Lead Temperature
Weight
For footnotes refer to the last page
*Current is limited by pin diameter
35*
35
284
250
2.0
±20
500
35
25
2.5
-55 to 150
Pre-Irradiation
Units
A
W
W/°C
V
mJ
A
mJ
V/ns
o
C
300 ( 0.063 in.(1.6mm) from case for 10s)
9.3 (Typical )
g
www.irf.com
1
8/9/01
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