JANSR2N7424U [INFINEON]
Rad hard, -60V, -48A, single, P-channel MOSFET, R4 in a SMD-2 package - SMD-2, 100 krad(Si) TID, QPL;型号: | JANSR2N7424U |
厂家: | Infineon |
描述: | Rad hard, -60V, -48A, single, P-channel MOSFET, R4 in a SMD-2 package - SMD-2, 100 krad(Si) TID, QPL 开关 脉冲 晶体管 |
文件: | 总25页 (文件大小:337K) |
中文: | 中文翻译 | 下载: | 下载PDF数据表文档文件 |
INCH-POUND
The documentation and process conversion
measures necessary to comply with this revision
shall be completed by 14 May 2012.
MIL-PRF-19500/655E
14 February 2012
SUPERSEDING
MIL-PRF-19500/655D
30 April 2007
PERFORMANCE SPECIFICATION SHEET
SEMICONDUCTOR DEVICE, FIELD EFFECT RADIATION HARDENED
(TOTAL DOSE AND SINGLE EVENT EFFECTS) TRANSISTOR, P-CHANNEL
SILICON, TYPES 2N7424U, 2N7425U, AND 2N7426U,
*
JANTXVR AND F AND JANSR AND F
This specification is approved for use by all Departments
and Agencies of the Department of Defense.
The requirements for acquiring the product described herein shall consist of
this specification sheet and MIL-PRF-19500.
1. SCOPE
*
1.1 Scope. This specification covers the performance requirements for a P-Channel, enhancement-mode,
MOSFET, radiation hardened (total dose and single event effects (SEE)), power transistor. Two levels of product
assurance are provided for each device type as specified in MIL-PRF-19500, with avalanche energy maximum rating
(EAS) and maximum avalanche current (IAS). See 6.5 for JANHC and JANKC die versions.
1.2 Physical dimensions. See figure 1, (surface mount).
1.3 Maximum ratings. TA = +25°C, unless otherwise specified.
Type
PT (1)
TC =
+25°C +25°C
PT
TA =
VDS
VDG
VGS
ID1 (3) (4) ID2 (3) (4)
IS
IDM (5)
A (pk)
TJ
and
TSTG
R θ
(2)
JC
TC =
+100°C
TC
=+25°C
W
W
V dc
V dc
V dc
A dc
A dc
A dc
°C/W
°C
2N7424U
2N7425U
2N7426U
300
300
300
2.5
2.5
2.5
-60
-60
-48
-38
-29
-30
-24
-18
-48
-38
-29
-192
-152
-108
0.42
0.42
0.42
±20
±20
±20
-55
to
+150
-100
-200
-100
-200
(1) Derate linearly by 2.4 W/°C for TC > +25°C.
(2) See figure 2, thermal impedance curves.
(3) The following formula derives the maximum theoretical ID limit. ID is limited by package and internal construction.
(4) See figure 3, maximum drain current graph.
(5) IDM = 4 X ID1 as calculated in note (3).
* Comments, suggestions, or questions on this document should be addressed to DLA Land and Maritime,
ATTN: VAC, P.O. Box 3990, Columbus, OH 43218-3990, or emailed to Semiconductor@dla.mil. Since contact
information can change, you may want to verify the currency of this address information using the ASSIST
Online database at https//assist.daps.dla.mil/.
AMSC N/A
FSC 5961
MIL-PRF-19500/655E
1.4 Primary electrical characteristics at TC = +25°C.
Type
Min
V(BR)DSS
VGS = 0
VGS(TH)1
VDS > VGS
ID = -1.0 mA VDS = 80%
Max IDSS1
GS = 0
Max rDS(on)
VGS = -12V, ID = ID2
(1)
EAS
V
dc
ID = -
1.0mA
of rated
VDS
TJ = +25°C
TJ = +150°C
dc
V dc
V dc
Min
mJ
µA dc
Ω
Ω
Max
-4.0
2N7424U
2N7425U
2N7426U
-60
-100
-200
-2.0
-2.0
-2.0
500
500
500
-25
-25
-25
0.045
0.068
0.154
0.100
0.150
0.360
-4.0
-4.0
(1) Pulsed (see 4.5.1).
2. APPLICABLE DOCUMENTS
2.1 General. The documents listed in this section are specified in sections 3, 4, or 5 of this specification. This
section does not include documents cited in other sections of this specification or recommended for additional
information or as examples. While every effort has been made to ensure the completeness of this list, document
users are cautioned that they must meet all specified requirements of documents cited in sections 3, 4, or 5 of this
specification, whether or not they are listed.
2.2 Government documents.
2.2.1 Specifications, standards, and handbooks. The following specifications, standards, and handbooks form a
part of this document to the extent specified herein. Unless otherwise specified, the issues of these documents are
those cited in the solicitation or contract.
DEPARTMENT OF DEFENSE SPECIFICATIONS
MIL-PRF-19500
DEPARTMENT OF DEFENSE STANDARDS
MIL-STD-750 Test Methods for Semiconductor Devices.
-
Semiconductor Devices, General Specification for.
-
* (Copies of these documents are available online at https://assist.daps.dla.mil/quicksearch/ or
https://assist.daps.dla.mil/ or from the Standardization Document Order Desk, 700 Robbins Avenue, Building 4D,
Philadelphia, PA 19111-5094.)
* 2.3 Order of precedence. Unless otherwise noted herein or in the contract, in the event of a conflict between the
text of this document and the references cited herein, the text of this document takes precedence. Nothing in this
document, however, supersedes applicable laws and regulations unless a specific exemption has been obtained.
2
MIL-PRF-19500/655E
Symbol
Dimensions
Inches
Millimeters
Min
.685
.520
Max
.695
.530
.142
.020
.445
.145
.480
.162
Min
17.40
13.21
Max
17.65
13.46
3.61
0.51
11.30
3.68
BL
BW
CH
LH
.010
.435
.135
.470
.152
0.25
11.05
3.43
11.94
3.86
LW1
LW2
LL1
12.19
4.11
LL2
LS1
LS2
.240 BSC
.120 BSC
6.10 BSC
3.05 BSC
Q1
Q2
.035
.050
0.89
1.27
TERM 1
TERM 2
TERM 3
Drain
Gate
Source
NOTES:
1. Dimensions are in inches.
2. Millimeters are given for information only.
3. The lid shall be electrically isolated from the drain, gate, and source.
4. In accordance with ASME Y14.5M, diameters are equivalent to φx symbology.
FIGURE 1. Dimensions and configuration.
3
MIL-PRF-19500/655E
3. REQUIREMENTS
3.1 General. The individual item requirements shall be as specified in MIL-PRF-19500 and as modified herein.
3.2 Qualification. Devices furnished under this specification shall be products that are manufactured by a
manufacturer authorized by the qualifying activity for listing on the applicable qualified manufacturer's list (QML)
before contract award (see 4.2 and 6.3).
3.3 Abbreviations, symbols, and definitions. Abbreviations, symbols, and definitions used herein shall be as
specified in MIL-PRF-19500 and as follows:
I
AS........Rated avalanche current, nonrepetitive
nC .......nano coulomb.
3.4 Interface and physical dimensions. Interface and physical dimensions shall be as specified in
MIL-PRF-19500, and on figure 1 (SMD2) herein.
3.4.1 Lead finish. Lead finish shall be solderable in accordance with MIL-PRF-19500, MIL-STD-750, and herein.
Where a choice of lead finish is desired, it shall be specified in the acquisition document (see 6.2).
3.5 Electrostatic discharge protection. The devices covered by this specification require electrostatic discharge
protection.
3.5.1 Handling. MOS devices must be handled with certain precautions to avoid damage due to the
accumulation of static charge. However, the following handling practices are recommended.
a. Devices should be handled on benches with conductive handling devices.
b. Ground test equipment, tools and personnel handling devices.
c. Do not handle devices by the leads.
d. Store devices in conductive foam or carriers.
e. Avoid use of plastic, rubber or silk in MOS areas.
f. Maintain relative humidity above 50 percent if practical.
g. Care should be exercised during test and troubleshooting to apply not more than maximum rated voltage to
any lead.
h. Gate must be terminated to source, R ≤ or 100 kΩ, whenever bias voltage is applied drain to source.
3.6 Electrical performance characteristics. Unless otherwise specified herein, the electrical performance
characteristics are as specified in 1.3, 1.4, and table I.
3.7 Electrical test requirements. The electrical test requirements shall be as specified in table I.
3.8 Marking. Marking shall be in accordance with MIL-PRF-19500.
3.9 Workmanship. Semiconductor devices shall be processed in such a manner as to be uniform in quality and
shall be free from other defects that will affect life, serviceability, or appearance.
4
MIL-PRF-19500/655E
4. VERIFICATION
4.1 Classification of inspections. The inspection requirements specified herein are classified as follows:
a. Qualification inspection (see 4.2).
b. Screening (see 4.3).
c. Conformance inspection (see 4.4 and tables I and II).
4.2 Qualification inspection. Qualification inspection shall be in accordance with MIL-PRF-19500 and as specified
herein.
4.2.1 Group E qualification. Group E inspection shall be performed for qualification or re-qualification only. In case
qualification was awarded to a prior revision of the specification sheet that did not request the performance of table III
tests, the tests specified in table III herein that were not performed in the prior revision shall be performed on the first
inspection lot of this revision to maintain qualification.
* 4.2.2 SEE. Design capability shall be tested on the initial qualification and thereafter whenever a major die design
or process change is introduced. Electrical measurements (end-points) shall be in accordance with table III.
5
MIL-PRF-19500/655E
* 4.3 Screening (JANS and JANTXV). Screening shall be in accordance with table E-IV of MIL-PRF-19500, and as
specified herein. The following measurements shall be made in accordance with table I herein. Devices that exceed
the limits of table I herein shall not be acceptable.
Screen (see table E-IV
of MIL-PRF-19500)
(1) (2)
Measurement
JANS level
JANTXV levels
Gate stress test (see 4.3.1)
(3)
(3)
Gate stress test (see 4.3.1)
Method 3470 of MIL-STD-750 (see 4.3.2), Method 3470 of MIL-STD-750 (see 4.3.2),
EAS test EAS test
(3) 3c
9
Method 3161 of MIL-STD-750 (see 4.3.3) Method 3161 of MIL-STD-750 (see 4.3.3)
IGSSF1, IGSSR1, IDSS1
Not applicable
10
Method 1042 of MIL-STD-750, test
condition B
Method 1042 of MIL-STD-750, test condition
B
11
IGSSF1, IGSSR1, IDSS1, rDS(on)1, VGS(th)1
subgroup 2 of table I herein:
IGSSF1, IGSSR1, IDSS1, rDS(on)1, VGS(th)1
subgroup 2 of table I herein
∆IGSSF1 = ± 20 nA dc or ± 100 percent of
initial value, whichever is greater.
∆IGSSR1 = ± 20 nA dc or ± 100 percent of
initial value, whichever is greater.
∆IDSS1 = ± 10 µA dc or ± 100 percent of
initial value, whichever is greater.
12
13
Method 1042 of MIL-STD-750, test
condition A
Method 1042 of MIL-STD-750, test condition
A
Subgroups 2 and 3 of table I herein;
∆IGSSF1 = ± 20 nA dc or ± 100 percent of
initial value, whichever is greater.
Subgroup 2 of table I herein;
∆IGSSF1 = ± 20 nA dc or ± 100 percent of initial
value, whichever is greater.
∆IGSSR1 = ± 20 nA dc or ± 100 percent of
initial value, whichever is greater.
∆IGSSR1 = ± 20 nA dc or ± 100 percent of initial
value, whichever is greater.
∆IDSS1 = ± 10 µA dc or ± 100 percent of
initial value, whichever is greater.
∆IDSS1 = ± 10 µA dc or ± 100 percent of initial
value, whichever is greater.
∆rDS(on)1 = ± 20 percent of initial value.
∆VGS(th)1 = ± 20 percent of initial value.
∆rDS(on)1 = ± 20 percent of initial value.
∆VGS(th)1 = ± 20 percent of initial value.
(1) At the end of the test program, IGSSF1, IGSSR1, and IDSS1 are measured.
(2) An out-of-family program to characterize IGSSF1, IGSSR1, IDSS1 and VGS(th)1 shall be invoked.
* (3) Shall be performed anytime after temperature cycling, screen 3a; JANTXV level does not need to be
repeated in screening requirements.
6
MIL-PRF-19500/655E
4.3.1 Gate stress test. Apply VGS = -24 V minimum for t = 250 µs minimum.
4.3.2 Single pulse avalanche energy (EAS).
a. Peak current ..................................................IAS = ID1
.
b. Inductance .....................................................L = (2*EAS/(ID1)2)*((VBR-VDD)/VBR) mH minimum.
c. Gate to source resistor...................................RGS: 25 Ω ≤ RGS ≤ 200 Ω.
d. Supply voltage ...............................................VDD = -25 V dc, except VDD = -50 V dc for 2N7426U.
e. Initial case temperature..................................TC = +25° C, -5° C, +10° C.
f. Gate voltage ..................................................VGS = -12 V dc.
g. Number of pulses to be applied .....................1 pulse minimum.
4.3.3 Thermal impedance. The thermal impedance measurements shall be performed in accordance with method
3161 of MIL-STD-750 using the guidelines in that method for determining IM, IH, tH, tSW, (and VH where appropriate).
Measurement delay time (tMD) = 70 µs max. See table III, group E, subgroup 4 herein.
4.4 Conformance inspection. Conformance inspection shall be in accordance with MIL-PRF-19500.
4.4.1 Group A inspection. Group A inspection shall be conducted in accordance with table E-V of MIL-PRF-19500
and table I herein.
4.4.2 Group B inspection. Group B inspection shall be conducted in accordance with the conditions specified for
subgroup testing in table E-VIA (JANS) and table E-VIB (JANTXV) of MIL-PRF-19500, and as follows. Electrical
measurements (end-points) shall be in accordance with table I, subgroup 2 herein.
4.4.2.1 Group B inspection, table E-VIA (JANS) of MIL-PRF-19500.
Subgroup Method
Condition
B3
B3
B4
1051
2077
1042
Test condition G, 100 cycles
SEM
Intermittent operation life, condition D, 2,000 cycles. No heat sink or forced-air cooling on
the device shall be permitted during the on cycle. ton = 30 seconds minimum.
B5
B5
B5
1042
1042
2037
Accelerated steady-state gate bias, condition B, VGS = rated; TA = +175°C, t = 24 hours
minimum; or TA = +150°C, t = 48 hours minimum.
Accelerated steady-state reverse bias, condition A, VDS = rated; TA = +175°C,
t = 120 hours minimum; or TA = +150°C, t = 240 hours minimum.
Bond strength, test condition A.
7
MIL-PRF-19500/655E
4.4.2.2 Group B inspection, table E-VIB (JANTXV) of MIL-PRF-19500.
Subgroup Method
Condition
B2
B3
1051
1042
Test condition G, 25 cycles.
Intermittent operation life, condition D, 2,000 cycles. No heat sink or forced-air cooling on
the device shall be permitted during the on cycle. ton = 30 seconds minimum.
4.4.3 Group C inspection. Group C inspection shall be conducted in accordance with the conditions specified for
subgroup testing in table E-VII of MIL-PRF-19500 and as follows. Electrical measurements (end-points) shall be in
accordance with table I, subgroup 2 herein.
Subgroup Method
Condition
C5
C6
3161
1042
See 4.3.3, RθJC(max) = 0.42°C/W
Intermittent operation life, condition D, 2,000 cycles. No heat sink or forced-air cooling on
the device shall be permitted during the on cycle. ton = 30 seconds minimum.
4.4.4 Group D inspection. Group D inspection shall be conducted in accordance with table E-VIII of
MIL-PRF-19500 and table II herein.
4.4.5 Group E inspection. Group E inspection shall be conducted in accordance with the conditions specified for
subgroup testing in table E-IX of MIL-PRF-19500 and as specified in table III herein. Electrical measurements (end-
points) shall be in accordance with table I, subgroup 2 herein.
4.5 Methods of inspection. Methods of inspection shall be as specified in the appropriate tables and as follows.
4.5.1 Pulse measurements. Conditions for pulse measurement shall be as specified in section 4 of
MIL-STD-750.
8
MIL-PRF-19500/655E
TABLE I. Group A inspection.
MIL-STD-750
Inspection
1/
Limits
Symbol
Unit
Method
2071
Condition
Min
Max
Subgroup 1
Visual and mechanical
inspection
Subgroup 2
Thermal Impedance 2/
3161
3407
See 4.3.3
Z θ
°C/W
JC
Breakdown voltage
drain to source
VGS = 0V,
ID = -1 mA dc,
bias condition C
V (BR)DSS
2N7424U
2N7425U
2N7426U
-60
-100
-200
V dc
V dc
V dc
Gate to source
voltage (threshold)
3403
3411
3413
3421
VGS(TH)1
-2.0
-4.0
±100
-25
V dc
nA dc
µA dc
VDS ≥ VGS
,
ID = -1 mA dc
Gate current
Drain current
IGSS1
VGS = ±20V dc, bias condition
C, VDS = 0V
VGS = 0V dc, bias condition C,
VDS = 80 percent of rated VDS
IDSS1
,
Static drain to source
on state resistance
2N7424U
VGS = -12V dc, condition A,
pulsed (see 4.5.1), ID = ID2
rDS(ON)1
0.045
0.068
0.154
Ω
Ω
Ω
2N7425U
2N7426U
Static drain to source
on state resistance
2N7424U
3421
4011
VGS = -12V dc, condition A,
pulsed (see 4.5.1), ID = ID1
rDS(ON)2
0.048
0.071
0.159
Ω
Ω
Ω
2N7425U
2N7426U
Forward voltage
VGS = 0V dc, condition A, pulsed
(see 4.5.1), ID = ID1
VSD
2N7424U
2N7425U
2N7426U
-3.0
-3.3
-3.0
V dc
V dc
V dc
See footnotes at end of table.
9
MIL-PRF-19500/655E
TABLE I. Group A inspection - Continued.
Inspection 1/
Subgroup 3
MIL-STD-750
Condition
Symbol
Limits
Min Max
Unit
Method
High temperature
operation
TC = TJ = +125°C
Gate current
3411
3413
3421
IGSS2
nA dc
VGS = ±20V dc, bias condition C, VDS
0V
=
±200
Drain current
VGS = 0V dc, bias condition C,
VDS = 80 percent of rated VDS
IDSS2
-0.25
mA dc
Static drain to source on-
state resistance
2N7424U
VGS = -12V dc, condition A,
pulsed (see 4.5.1), ID = ID2
rDS(ON)3
0.085
0.135
0.35
Ω
Ω
Ω
2N7425U
2N7426U
Gate to source voltage
(threshold)
3403
VGS(TH)2
-1.0
V dc
VDS ≥ VGS, ID = -1 mA dc
TC = TJ = -55°C
Low temperature
operation
Gate to source voltage
(threshold)
3403
3472
VGS(TH)3
-5.0
V dc
VDS ≥ VGS(TH)3, ID = -1 mA dc
Subgroup 4
Switching time test
ID = ID1, VGS = -12 V dc, RG = 2.35 Ω,
VDD = 50 percent of rated VDS
Turn-on delay time
2N7424U
tD(on)
35
35
37
ns
ns
ns
2N7425U
2N7426U
Rise time
2N7424U
tr
150
170
141
ns
ns
ns
2N7425U
2N7426U
Turn-off delay time
2N7424U
tD(off)
200
190
148
ns
ns
ns
2N7425U
2N7426U
Fall time
tf
2N7424U
200
190
220
ns
ns
ns
2N7425U
2N7426U
See footnotes at end of table.
10
MIL-PRF-19500/655E
TABLE I. Group A inspection - Continued.
Inspection 1/
MIL-STD-750
Condition
Symbol
Limits
Unit
Method
3475
Min
Max
Subgroup 4 - continued
ID = rated ID2, VDD = 15 V (see 4.5.1)
gFS
Forward transconductance
2N7424U
18
15
14
S
S
S
2N7425U
2N7426U
Subgroup 5
Safe operating area
test (high voltage)
3474
See figure 4
tp = 10 ms min. VDS = 80 percent of
max. rated VDS
Electrical measurements
Subgroup 6
See table I, subgroup 2
Not applicable
Subgroup 7
Gate charge
3471
Condition B
On-state gate charge
2N7424U
QG(ON)
QGS
QGD
trr
300
290
300
nC
nC
nC
2N7425U
2N7426U
Gate to source charge
2N7424U
70
72
65
nC
nC
nC
2N7425U
2N7426U
Gate to drain charge
2N7424U
91
90
58
nC
nC
nC
2N7425U
2N7426U
Reverse recovery time
3473
di/dt = -100 A/µs, VDD ≤ -50 V
ID = ID1
2N7424U
2N7425U
2N7426U
270
300
738
ns
ns
ns
1/ For sampling plan, see MIL-PRF-19500.
2/ This test required for the following end-point measurements only:
Group B, subgroups 3 and 4 (JANS).
Group B, subgroups 2 and 3 (JANTXV).
Group C, subgroups 2 and 6.
Group E, subgroup 1.
11
MIL-PRF-19500/655E
TABLE II. Group D inspection.
Inspection
1/ 2/ 3/
Symbol
Pre-irradiation
limits
Post-irradiation limits
F 4/
Unit
MIL-STD-750
R and F
R
Method
Conditions
Min
Max
Min
Max
Min
Max
Subgroup 1
Not
applicable
Subgroup 2
TC = + 25°C
Steady-
state total
dose
1019
1019
VGS = -12 V;
VDS = 0 V
irradiation
(V bias)
GS
5/
Steady-
state total
dose
VGS = 0 V;
VDS = 80 percent
of rated VDS
irradiation
(preirradiation)
(V bias)
DS
5/
End-point
electricals
Breakdown
voltage,
drain to
3407
3403
VGS = 0 V;
ID = -1 mA;
bias condition C
V(BR)DSS
source
2N7424U
-60
-60
-60
V dc
V dc
V dc
2N7425U
2N7426U
-100
-200
-100
-200
-100
-200
Gate to
VGS(th)1
VDS ≥ VGS
,
source
voltage
ID = -1 mA
(threshold)
2N7424U
-2.0
-2.0
-2.0
-4.0
-4.0
-4.0
-2.0
-2.0
-2.0
-4.0
-4.0
-4.0
-2.0
-2.0
-2.0
-5.0
-5.0
-5.0
V dc
V dc
V dc
2N7425U
2N7426U
Gate
current
3411
3411
3413
VGS = -20 V,
VDS = 0 V,
bias condition C
IGSSF1
IGSSR1
IDSS
-100
100
-25
-100
100
-25
-100
100
-25
nA
dc
Gate
current
VGS = +20 V,
VDS = 0 V,
bias condition C
nA
dc
Drain
current
VGS = 0 V,
VDS = 80 percent
µA
dc
of rated V
DS
(preirradiation),
bias condition C
See footnotes at end of table.
12
MIL-PRF-19500/655E
TABLE II. Group D inspection - Continued.
Pre-irradiation
limits
Post-irradiation limits
F 4/
Max
Unit
Inspection
1/ 2/ 3/
MIL-STD-750
Symbol
R and F
R
Method
3405
Conditions
Min
Max
Min
Max
Min
Subgroup 2
continued
TC = + 25°C
Static drain
to source
on-state
VGS = -12 V,
VDS(on)
ID = ID2
,
condition A,
pulsed (see
4.5.1)
voltage
2N7424U
2N7425U
2N7426U
-1.35
-1.35
-1.35
-1.632
-2.88
V dc
V dc
V dc
-1.632
-2.772
-1.632
-2.772
Forward
voltage
4011
VGS = 0 V,
VSD
ID = ID1
,
source drain
diode
bias condition C
2N7424U
-3.0
-3.3
-3.0
-3.0
-3.3
-3.0
-3.0
-3.3
-3.0
V dc
V dc
V dc
2N7425U
2N7426U
1/
2/
For sampling plan see MIL-PRF-19500.
Group D qualification may be performed prior to lot formation. Wafers qualified to these group D QCI
requirements may be used for any other specification utilizing the same die design.
At the manufacturer’s option, group D samples need not be subjected to the screening tests, and may
be assembled in its qualified package or in any qualified package that the manufacturer has data to
correlate the performance to the designated package.
3/
4/
5/
The “F” designation represents devices which pass end-points at R and F designated total-ionizing-dose
(TID)
Separate samples shall be pulled for each bias.
13
MIL-PRF-19500/655E
* TABLE III. Group E inspection (all quality levels) for qualification or re-qualification only.
Sample
MIL-STD-750
Conditions
Inspection
Subgroup 1
Method
plan
45 devices
c = 0
Temperature cycle
Hermetic seal
1051
1071
Condition G, 500 cycles
See table I, subgroup 2
Fine leak
Gross leak
Electrical measurements
Subgroup 2 1/
45 devices
c = 0
Steady-state gate bias
Electrical measurements
Steady-state reverse bias
Electrical measurements
Subgroup 4
1042
1042
Condition B, 1,000 hours
See table I, subgroup 2
Condition A, 1,000 hours
See table I, subgroup 2
sample size
N/A
Thermal impedance curves
Subgroup 10
See MIL-PRF-19500.
Commutating diode for safe
operating area test procedure
for measuring dv/dt during
reverse recovery of power
MOSFET transistors or
insulated gate bipolar
transistors
3476
Test conditions shall be derived by the
manufacturer.
22 devices
c = 0
14
MIL-PRF-19500/655E
* TABLE III. Group E inspection (all quality levels) - for qualification or re-qualification only - Continued.
Qualification
MIL-STD-750
and large lot
Inspection
quality
Method
Conditions
conformance
inspection
Subgroup 11
3 devices
SEE 2/ 3/ 4/
1080
See figure 5.
, IGSSR1, and I
Electrical measurements
5/
I
in accordance with table I,
DSS1
GSSF1
subgroup 2
Fluence = 3E5 ±20 percent ions/cm2
SEE irradiation
2N7424U
Flux = 2E3 to 2E4 ions/cm2/sec, temperature = +25 ±5 °C
Surface LET = 28 MeV-cm2/mg ±5%,
range = 42.8 µm ±7.5%, energy = 283.3 MeV ±7.5%
In-situ bias conditions: VDS = -60 V and VGS = +5 V
VDS = -50 V and VGS = +10 V
VDS = -35 V and VGS = +15 V
(typical 4.53 MeV/nucleon at Brookhaven National Lab
Accelerator)
2N7425U
2N7426U
2N7424U
In-situ bias conditions: VDS = -100 V and VGS = +10 V
VDS = -70 V and VGS = +15 V
VDS = -60 V and VGS = +20 V
(nominal 4.53 MeV/nucleon at Brookhaven National Lab
Accelerator)
In-situ bias conditions: VDS = -200 V and VGS = +15 V
(nominal 4.53 MeV/nucleon at Brookhaven National Lab
Accelerator)
Surface LET = 37 MeV-cm2/mg ±5%,
range = 39 µm ±5%, energy = 305 MeV ±5%
In situ bias conditions: VDS = -55 V and VGS = +0 V
VDS = -45 V and VGS = +5 V
VDS = -35 V and VGS = +10 V
VDS = -30 V and VGS = +15 V
(typical 3.77 MeV/nucleon at Brookhaven National Lab
Accelerator)
2N7425U
In situ bias conditions: VDS = -100 V and VGS = +5 V
VDS = -70 V and VGS = +10 V
VDS = -50 V and VGS = +15 V
VDS = -40 V and VGS = +20 V
(nominal 3.77 MeV/nucleon at Brookhaven National Lab
Accelerator)
15
MIL-PRF-19500/655E
* TABLE III. Group E inspection (all quality levels) - for qualification or re-qualification only - Continued.
Qualification
MIL-STD-750
and large lot
Inspection
Subgroup 11 - continued
2N7424U
quality
conformance
inspection
Method
Conditions
3 devices
Surface LET = 59.9 MeV-cm2/mg ±5%,
range = 32.8 µm ±5%, energy = 345 MeV ±5%
In situ bias conditions: VDS = -40 V and VGS = 0 V
VDS = -35 V and VGS = +5 V
(typical 2.72 MeV/nucleon at Brookhaven National Lab
Accelerator)
2N7425U
In situ bias conditions: VDS = -60 V and VGS = 0 V
(typical 2.72 MeV/nucleon at Brookhaven National Lab
Accelerator)
Electrical measurements
5/
IGSSF1, IGSSR1, and IDSS1 in accordance with table I, subgroup 2
1/
2/
A separate sample for each test shall be pulled.
Group E qualification of SEE testing may be performed prior to lot formation. Qualification may be extended
to other specification sheets utilizing the same structurally identical die design.
Device qualification to a higher level LET is sufficient to qualify all lower level LETs.
The sampling plan applies to each bias condition.
Examine IGSSF1, IGSSR1 and IDSS1 before and following SEE irradiation to determine acceptability for each bias
condition. Other test conditions in accordance with table I, subgroup 2, may be performed at the
manufacturer’s option.
3/
4/
5/
16
MIL-PRF-19500/655E
FIGURE 2. Thermal impedance curve.
17
MIL-PRF-19500/655E
2N7424U
2N7425U
2N7426U
FIGURE 3. Maximum drain current versus case temperature graphs.
18
MIL-PRF-19500/655E
FIGURE 4. Safe operating area graph.
19
MIL-PRF-19500/655E
* FIGURE 4. Safe operating area graph - Continued.
20
MIL-PRF-19500/655E
* FIGURE 4. Safe operating area graph - Continued.
21
MIL-PRF-19500/655E
2N7424U
Typical SEE Response
-70
-60
-50
-40
-30
-20
-10
0
LET=28±5%
Range=42.8µm±5%
Energy=283.3MeV±7.5%
LET=37±5%
Range=39µm±5%
Energy=305MeV±5%
LET=59.9±5%
Range=32.8µm±5%
Energy=345MeV±5%
0
5
10
15
20
VGS Bias (Volts)
2N7425U
Typical SEE Response
-120
-100
-80
-60
-40
-20
0
LET=28±5%
Range=42.8µm±5%
Energy=283.3MeV±7.5%
LET=37±5%
Range=39µm±5%
Energy=305MeV±5%
LET=59.9±5%
Range=32.8µm±5%
Energy=345MeV±5%
0
5
10
15
20
VGS Bias (Volts)
* FIGURE 5. Typical single event effects safe operating area graphs.
22
MIL-PRF-19500/655E
2N7426U
Typical SEE Response
-250
-200
-150
-100
-50
LET=28±5%
Range=42.8µm±5%
Energy=283.3MeV±7.5%
LET=37±5%
Range=39µm±5%
Energy=305MeV±5%
0
0
5
10
15
20
VGS Bias (Volts)
* FIGURE 5. Typical single event effects safe operating area graphs - Continued.
23
MIL-PRF-19500/655E
5. PACKAGING
5.1 Packaging. For acquisition purposes, the packaging requirements shall be as specified in the contract or order
(see 6.2). When packaging of materiel is to be performed by DoD or in-house contractor personnel, these personnel
need to contact the responsible packaging activity to ascertain packaging requirements. Packaging requirements are
maintained by the Inventory Control Point's packaging activities within the Military Service or Defense Agency, or
within the Military Service’s system commands. Packaging data retrieval is available from the managing Military
Department's or Defense Agency's automated packaging files, CD-ROM products, or by contacting the responsible
packaging activity.
6. NOTES
(This section contains information of a general or explanatory nature that may be helpful, but is not mandatory.
The notes specified in MIL-PRF-19500 are applicable to this specification.)
6.1 Intended use. Semiconductors conforming to this specification are intended for original equipment design
applications and logistic support of existing equipment.
6.2 Acquisition requirements. Acquisition documents should specify the following:
a. Title, number, and date of this specification.
b. Packaging requirements (see 5.1).
c. Lead finish (see 3.4.1).
d. Product assurance level and type designator.
* e. For acquisition of RHA designated devices, table II, subgroup 1 testing of group D herein is optional.
If subgroup 1 is desired, it must be specified in the contract.
* 6.3 Qualification. With respect to products requiring qualification, awards will be made only for products which are,
at the time of award of contract, qualified for inclusion in Qualified Manufacturers List (QML 19500) whether or not
such products have actually been so listed by that date. The attention of the contractors is called to these
requirements, and manufacturers are urged to arrange to have the products that they propose to offer to the Federal
Government tested for qualification in order that they may be eligible to be awarded contracts or orders for the
products covered by this specification. Information pertaining to qualification of products may be obtained from DLA
Land and Maritime, ATTN: VQE, P.O. Box 3990, Columbus, OH 43218-3990 or e-mail vqe.chief@dla.mil. An online
listing of products qualified to this specification may be found in the Qualified Products Database (QPD) at
https://assist.daps.dla.mil.
6.4 Cross-reference list. The following table shows the generic P/N and its associated military P/N (without JAN
and RHA prefix).
Generic P/N
Military P/N
IRHNA9064
IRHNA9160
IRHNA9260
2N7424U
2N7425U
2N7426U
6.5 JANC die versions. The JANHC and JANKC die versions of these devices are covered under performance
specification sheet MIL-PRF-19500/657.
24
MIL-PRF-19500/655E
6.6 Changes from previous issue. The margins of this specification are marked with asterisks to indicate where
changes from the previous issue were made. This was done as a convenience only and the Government assumes
no liability whatsoever for any inaccuracies in these notations. Bidders and contractors are cautioned to evaluate the
requirements of this document based on the entire content irrespective of the marginal notations and relationship to
the last previous issue.
Custodians:
Army - CR
Air Force - 85
DLA - CC
Preparing activity:
DLA - CC
(Project 5961-2012-013)
*
NOTE: The activities listed above were interested in this document as of the date of this document. Since
organizations and responsibilities can change, you should verify the currency of the information above using the
ASSIST Online database at https://assist.daps.dla.mil/ .
25
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