IRHF7430SE_15 Datasheet, PDF (1/8 Pages) International Rectifier – Simple Drive Requirements

RADIATION HARDENED
POWER MOSFET
THRU-HOLE (TO-39)
PD-91863E
IRHF7430SE
JANSR2N7464T2
500V, N-CHANNEL
REF: MIL-PRF-19500/675
RAD Hard^™ HEXFET^® TECHNOLOGY
Product Summary
Part Number Radiation Level RDS(on)
IRHF7430SE 100K Rads (Si) 1.77Ω
I D QPL Part Number
2.5A JANSR2N7464T2
International Rectifier’s RADHard^TM HEXFET^® MOSFET
technology provides high performance power MOSFETs
for space applications. This technology has over a
decade of proven performance and reliability in satellite
applications. These devices have been characterized
for both Total Dose and Single Event Effects (SEE). The
combination of low RDS(on) 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 electrical parameters.
TO-39
Features:
n Single Event Effect (SEE) Hardened
n Ultra Low RDS(on)
n Low Total Gate Charge
n Neuton Tolerant
n Simple Drive Requirements
n Ease of Paralleling
n Hermetically Sealed
n Light Weight
Absolute Maximum Ratings
Pre-Irradiation
Parameter
Units
ID @ VGS = 12V, TC = 25°C Continuous Drain Current
ID @ VGS = 12V, TC = 100°C Continuous Drain Current
IDM
Pulsed Drain Current À
PD @ TC = 25°C
Max. Power Dissipation
Linear Derating Factor
2.5
1.6
A
10
25
W
0.2
W/°C
VGS
Gate-to-Source Voltage
±20
EAS
Single Pulse Avalanche Energy Á
154
IAR
Avalanche Current À
2.5
EAR
Repetitive Avalanche Energy À
2.5
dv/dt
Peak Diode Recovery dv/dt Â
8.0
V
mJ
A
mJ
V/ns
TJ
TSTG
Operating Junction
Storage Temperature Range
Lead Temperature
-55 to 150
°C
300 (0.063 in. (1.6mm) from case for 10 sec.)
Weight
0.98 (Typical)
g
For footnotes refer to the last page
www.irf.com
1
07/25/12