JANSR2N7424U [INFINEON]

Rad hard, -60V, -48A, single, P-channel MOSFET, R4 in a SMD-2 package - SMD-2, 100 krad(Si) TID, QPL;
JANSR2N7424U
型号: JANSR2N7424U
厂家: Infineon    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  
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 k, 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 .  
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  
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  
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  
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 ,  
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  

相关型号:

JANSR2N7425U

Rad hard, -100V, -38A, single, P-channel MOSFET, R4 in a SMD-2 package - SMD-2, 100 krad(Si) TID, QPL
INFINEON

JANSR2N7426

RADIATION HARDENED POWER MOSFET THRU-HOLE (TO-254AA)
INFINEON

JANSR2N7426U

RADIATION HARDENED POWER MOSFET SURFACE MOUNT (SMD-2)
INFINEON

JANSR2N7430T1

Power Field-Effect Transistor, 70A I(D), 60V, 0.012ohm, 1-Element, N-Channel, Silicon, Metal-oxide Semiconductor FET, TO-254AA
FAIRCHILD

JANSR2N7431D

Power Field-Effect Transistor, 35A I(D), 60V, 0.021ohm, 1-Element, N-Channel, Silicon, Metal-oxide Semiconductor FET, HERMETIC SEALED, CERAMIC, TO-254AA, 3 PIN
INFINEON

JANSR2N7432

100V 100kRad Hi-Rel Single N-Channel TID Hardened MOSFET in a TO-254AA package
ETC

JANSR2N7432U

100V 100kRad Hi-Rel Single N-Channel TID Hardened MOSFET in a SMD-2 package
ETC

JANSR2N7434

Power Field-Effect Transistor, 31A I(D), 250V, 0.123ohm, 1-Element, N-Channel, Silicon, Metal-oxide Semiconductor FET, TO-254AA,
INFINEON

JANSR2N7438

Formerly Available As FSL913A0R4, Radiation Hardened, SEGR Resistant, P-Channel Power MOSFETs
INTERSIL

JANSR2N7438

Power Field-Effect Transistor, 7A I(D), 100V, 0.3ohm, 1-Element, P-Channel, Silicon, Metal-oxide Semiconductor FET, TO-205AF, HERMETIC SEALED, METAL CAN-3
FAIRCHILD

JANSR2N7439

Formerly Available As FSL923A0R4, Radiation Hardened, SEGR Resistant, P-Channel Power MOSFETs
INTERSIL

JANSR2N7440

Formerly Available as FSS913A0R4, Radiation Hardened, SEGR Resistant, P-Channel Power MOSFETs
INTERSIL