JANTX1N5811CBUS [MICROSEMI]
Rectifier Diode, 1 Phase, 1 Element, 3A, Silicon, HERMETIC SEALED, GLASS, D-5B, 2 PIN;型号: | JANTX1N5811CBUS |
厂家: | Microsemi |
描述: | Rectifier Diode, 1 Phase, 1 Element, 3A, Silicon, HERMETIC SEALED, GLASS, D-5B, 2 PIN 超快恢复二极管 快速恢复二极管 |
文件: | 总30页 (文件大小:374K) |
中文: | 中文翻译 | 下载: | 下载PDF数据表文档文件 |
The documentation and process conversion
measures necessary to comply with this revision
shall be completed by 28 November 2009.
INCH-POUND
MIL-PRF-19500/742A
28 August 2009
SUPERSEDING
MIL-PRF-19500/742
1 June 2007
PERFORMANCE SPECIFICATION SHEET
* SEMICONDUCTOR DEVICE, DIODE, SILICON, ULTRAFAST RECOVERY, POWER RECTIFIER,
TYPES 1N5802CB, 1N5804CB, 1N5806CB, 1N5807CB, 1N5809CB, AND 1N5811CB,
1N5802CBUS, 1N5804CBUS, 1N5806CBUS, 1N5807CBUS, 1N5809CBUS, AND 1N5811CBUS,
JAN, JANTX, AND JANTXV
* Inactive for new design after 28 September 2009. For new design use -
1N5802, 1N5804, 1N5806, 1N5807, 1N5809, AND 1N5811, 1N5802US,
1N5804US, 1N5806US, 1N5807US, 1N5809US, AND 1N5811US on MIL-PRF-
19500/477.
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 silicon, fast recovery, power rectifier
diodes. Four levels of product assurance are provided for each encapsulated (noncavity double plug diodes utilizing
category 3 metallurgical bonding) device types as specified in MIL-PRF-19500. This category 3 metallurgical
bonding is also known as compression bonds (CB).
* 1.2 Physical dimensions. See figures 1(similar to a DO-7) and 2 (square end-cap surface mount).
1.3 Maximum ratings. Unless otherwise specified, TA = +25°C.
1.3.1 Ratings applicable to all Part or Identifying Numbers (PIN). TSTG = TJ(max) = -65°C to +175°C.
1.3.2 Ratings applicable to individual types.
Col. 1
Col. 2
VRWM
Col. 3
IO(L)
TL = +75°C
L = .25 in.
(6.35 mm)
(2) (3)
Col. 4
IO1
TA =
+55°C
(4) (5) (6)
Col. 5
Col. 6
trr
Col. 7
Col. 8
Col. 9
IFSM at
+25°C
operating at
RθJL
at
L = .375 in.
(9.52 mm)
Types
(1)
RθJEC
(7)
R
θJX
(6)
IO1
tp = 8.3 ms
A(pk)
A
A
ns
°C/W
36
36
36
22
°C/W
13
13
°C/W
154
154
154
52
1N5802CB, CBUS
1N5804CB, CBUS
1N5806CB, CBUS
1N5807CB, CBUS
1N5809CB, CBUS
1N5811CB, CBUS
50
2.5
2.5
2.5
6.0
6.0
6.0
1.0
1.0
1.0
3.0
3.0
3.0
35
35
35
125
125
125
25
25
25
30
30
30
100
150
50
100
150
13
6.5
6.5
6.5
22
22
52
52
See notes on next page.
Comments, suggestions, or questions on this document should be addressed to Defense Supply Center,
Columbus, ATTN: DSCC-VAC, P.O. Box 3990, Columbus, OH 43218-3990, or emailed to
Semiconductor@dscc.dla.mil . Since contact information can change, you may want to verify the currency of
this address information using the ASSIST Online database at http://assist.daps.dla.mil.
AMSC N/A
FSC 5961
MIL-PRF-19500/742A
1.3.2 Ratings applicable to individual types - Continued.
(1) TEC = TL at L = 0 or Tend tab for US suffix devices.
(2) Derate at 24 mA/ºC for TL above +75 ºC for 2.5 amp ratings.
(3) Derate at 60 mA/ºC for TL above +75 ºC for 6.0 amp ratings
(4) Derate at 8.33 mA/ºC for TA above +55 ºC for 1.0 amp ratings.
(5) Derate at 25 mA/ºC for TA above +55 ºC for 3.0 amp ratings
(6) For the 1 and 3 amp ratings at 55ºC, These IO ratings are for a thermally (PC boards or other) mounting
methods where the lead or end-cap temperatures cannot be maintained as shown in col. 3 and where thermal
resistance from mounting point to ambient is still sufficiently controlled where TJ(MAX) in 1.3.1 is not exceeded.
This equates to RθJX ≤ 154ºC/W for the 1N5802CB-1N5806CB and RθJX ≤ 52ºC/W for the 1N5807CB-
1N5811CB in col. 9. Also see application notes in 6.4.1 thru 6.4.4.
(7) US suffix devices only.
1.4 Primary electrical characteristics. Unless otherwise specified, TA = +25°C.
I
R1 at VR = VRWM
IR2 at VR = VRWM
Types
VBR at 100 µA
Pulse ≤ 20 ms
TA = +25°C
TA = +125°C
Pulsed VR ≤ 20ms
µA
Pulsed VR ≤ 20ms¸
V
µA
1N5802CB, CBUS
1N5804CB, CBUS
1N5806CB, CBUS
1N5807CB, CBUS
1N5809CB, CBUS
1N5811CB, CBUS
60
110
160
60
110
160
1.0
1.0
1.0
5.0
5.0
5.0
175
175
175
525
525
525
2
MIL-PRF-19500/742A
Dimensions
1N5802CB, 1N5804CB, 1N5806CB 1N5807CB, 1N5809CB, 1N5811CB
Inches Millimeters Inches Millimeters
Min Min
Ltr.
Notes
Max
.085
.250
.032
1.30
Min
Max
2.16
6.35
0.81
33.02
Max
.142
.300
.042
1.30
Min
Max
3.61
7.62
1.07
33.02
BD
BL
LD
LL
.065
.125
.027
.700
1.65
3.18
0.69
.115
.130
.037
.900
2.92
3.30
0.94
4
3
3
17.78
22.86
NOTES:
1. Dimensions are in inches.
2. Millimeters are given for general information only.
3. Dimension BL shall include the entire body including slugs and sections of the lead over which
the diameter is uncontrolled. This uncontrolled area is defined as the zone between the edge of
the diode body and extending .050 inch (1.27 mm) onto the leads.
4. Dimension BD shall be measured at the largest diameter.
5. In accordance with ASME Y14.5M, diameters are equivalent to φx symbology.
* FIGURE 1. Physical dimensions (similar to a DO-7).
3
MIL-PRF-19500/742A
Dimensions
D-5A
D-5B
1N5802CBUS, 1N5804CBUS,
1N5806CBUS
1N5807CBUS, 1N5809CBUS,
1N5811CBUS
Ltr.
Inches
Max
Millimeters
Inches
Millimeters
Notes
Min
.091
.168
Min
Max
2.62
5.08
0.71
Min
Max
.148
.225
.028
Min
Max
3.76
5.72
0.71
BD
BL
ECT .019
.103
.200
.028
2.31
4.27
0.48
0.08
.137
.200
.019
.003
3.48
5.08
0.48
0.08
S
.003
NOTES:
1. Dimensions are in inches.
2. Millimeters are given for general information only.
3. Dimensions are pre-solder dip.
4. Minimum clearance of glass body to mounting surface on all orientations.
5. Cathode marking to be either in color band, three dots spaced equally, or a color dot on the face
of the end tab.
6. Color dots will be .020 inch (0.51 mm) diameter minimum and those on the face of the end tab
shall not lie within .020 inch (0.51 mm) of the mounting surface.
7. In accordance with ASME Y14.5M, diameters are equivalent to φx symbology.
* FIGURE 2. Physical dimensions of surface mount family (square body surface mount).
4
MIL-PRF-19500/742A
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 http://assist.daps.dla.mil/quicksearch/ or
http://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.
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:
EC. . . . . . . . . . . . . . End-cap.
I(BR) . . . . . . . . . . . . .Current for testing breakdown voltage.
Vfr . . . . . . . . . . . . . . Forward recovery voltage.
3.4 Interface and physical dimensions. The interface and physical dimensions shall be as specified in
MIL-PRF-19500, and figures 1 and 2 herein.
3.4.1 Diode construction. These devices shall be metallurgically bonded-thermally-matched-noncavity-double plug
construction, utilizing a category III bond, in accordance with MIL-PRF-19500. Full area metallurgical bond is
required. (i.e. slug tungsten or moly to die). No point contacts are allowed. Silver button dumet design is prohibited.
US version devices shall be structurally identical to the non-surface mount devices except for lead terminations.
3.4.2 Lead finish. Unless otherwise specified, lead or end-cap finish shall be solderable in accordance with
MIL-PRF-19500, MIL-STD-750, and herein. When solder alloy is used for finish, the maximum lead temperature is
limited to 175°C maximum. Where a choice of finish is desired, it shall be specified in the acquisition document (see
6.2).
5
MIL-PRF-19500/742A
3.5 Marking. Devices shall be marked as specified in MIL-PRF-19500.
3.5.1 Marking of US version. For US version only, all marking may be omitted from the device except for the
cathode marking. All marking which is omitted from the body of the device shall appear on the label of the initial
container.
3.5.2 Polarity. The polarity shall be indicated with a contrasting color band to denote the cathode end. Alternately,
for surface mount (US) devices, a minimum of three evenly spaced contrasting color dots around the periphery of the
cathode end may be used. No color coding will be permitted.
3.6 Electrical performance characteristics. Unless otherwise specified herein, the electrical performance
characteristics are as specified in 1.3, 1.4, and table I herein.
3.7 Electrical test requirements. The electrical test requirements shall be the subgroups specified in table I herein.
3.8 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. 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 herein.
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 II tests, the tests specified in table II herein that were not performed in the prior revision shall be performed on
the first inspection lot to this revision to maintain qualification.
4.2.2 JANHC and JANKC die. Qualification shall be in accordance with appendix G of MIL-PRF-19500 and as
specified herein.
6
MIL-PRF-19500/742A
* 4.3 Screening (JANTXV and JANTX levels only). Screening shall be in accordance with appendix E, 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
appendix E, table
E-IV of
JANTXV and JANTX level
MIL-PRF-19500)
(1) 3c
9
Thermal impedance (see 4.3.1)
Not required
10
Method 1038 of MIL-STD-750, condition A
11
Required
IR1 and VFM1
12
Required, see 4.3.2
(2) 13
Subgroup 2 of table I herein;∆IR1 ≤±100
percent of initial reading or ±250 nA dc
(1N5802, 1N5804, 1N5806) or ±1 µA dc
(1N5807, 1N5809, 1N5811), whichever is
greater.
∆VFM1 ≤ ±0.05 V dc.
Scope-display evaluation (see 4.5.2).
(1) Shall be performed anytime after temperature cycling, screen 3a; and does not need to be repeated in
screening requirements.
(2) Z
is not required in screen 13, if already previously performed.
θJX
4.3.1 Thermal impedance. The thermal impedance measurements shall be performed in accordance with method
3101 of MIL-STD-750 using the guidelines in that method for determining IM, IH, tH, and K factor where appropriate.
Measurement delay time (tMD) = 70 µs max. The limits will be statistically derived. See table E-IX of MIL-PRF-19500,
group E, subgroup 4 and table II, subgroup 4 herein. See figures 3, 4, 5, and 6 for thermal impedance.
* 4.3.2 Free air power burn-in conditions. Power burn-in conditions (ACOL or dc) as follows: Test conditions shall
be in accordance with method 1038 of MIL-STD-750, condition B (see 4.5.3, 4.5.3.1). Adjust TA, IO, or IF to achieve
TJ = 135°C minimum, 175°C maximum.
a. ACOL: VR = rated VRWM; f = 60 Hz; IO (min) = col. 4 of 1.3.2, (see 4.5.3).
b. DC: IF (min) = col. 4 of 1.3.2.
With approval of the qualifying activity and preparing activity, alternate burn-in criteria (hours, bias conditions, TJ,
mounting conditions) may be used. A justification demonstrating equivalence is required. In addition, the
manufacturing site’s burn-in data and performance history will be essential criteria for burn-in modification approval.
7
MIL-PRF-19500/742A
4.4 Conformance inspection. Conformance inspection shall be in accordance with MIL-PRF-19500 and as
specified herein.
4.4.1 Group A inspection. Group A inspection shall be conducted in accordance with MIL-PRF-19500, and table I
herein.
* 4.4.2 Group B inspection. Group B inspection shall be conducted in accordance with the tests and conditions
specified for subgroup testing in appendix E, table E-VIb (JAN, JANTX, and JANTXV) of MIL-PRF-19500 and herein.
Electrical measurements (end-points) shall be in accordance with table I, subgroup 2 herein.
* 4.4.2.1 Group B inspection, appendix E, table E-VIb (JAN, JANTX, and JANTXV of MIL-PRF-19500).
Subgroup
B3
Method Condition
1027
IO = IO1 rated minimum (see col. 4 of 1.3.2); adjust IO to achieve T = 150° C
J
minimum, apply V = rated V
RWM
(see col. 2 of 1.3.2), f = 50 - 60 Hz (see
R
4.5.3.1). TA = 55°C max. For irradiated devices, include trr as an end-point
measurement.
4.4.3 Group C inspection. Group C inspection shall be conducted in accordance with the conditions specified for
subgroup testing in appendix E, table E-VII of MIL-PRF-19500. Electrical measurements (end-points) shall be in
accordance with table I, subgroup 2 herein.
* 4.4.3.1 Group C inspection, appendix E, table E-VII of MIL-PRF-19500.
Subgroup
C2
Method Condition
2036
2036
Axial devices − Tension: Condition A, 4 pounds, t = 15s - 1N5802, 1N5804,
1N5806. 12 pounds - 1N5807, 1N5809, 1N5811. Fatigue: Condition E, 2
pounds. (Lead fatigue is not applicable to US diodes).
*
C2
US devices – Tension: condition A; 4 pounds, t = 15s for 1N5802US,
1N5804US, 1N5806US. Condition A, 12 pounds, t = 15s for 1N5807US,
1N5809US, 1N5811US. Suitable fixtures may be used to pull the end-caps in a
manner which does not aid construction. Reference to axial lead may be
interpreted as end-cap with fixtures used for mounting (see figure 7 herein).
(Lead fatigue is not applicable to US diodes).
C5
C6
4081
1027
R
θJL(maximum) see col. 7 of 1.3.2 and 4.3.1 herein; L = .375 inch (9.53 mm).
For surface mount devices (US version), RθJEC see col. 8 of 1.3.2 and 4.3.1
herein.
IO = IO1 rated minimum (see col. 4 of 1.3.2); adjust IO to achieve
TJ = 150°C minimum, apply VR = rated VRWM (see col. 2 of 1.3.2), f = 50 - 60 Hz
(see 4.5.3.1). TA = 55°C max. For irradiated devices, include trr as an end-point
measurement.
4.4.4 Group E inspection. Group E inspection shall be conducted in accordance with the conditions specified for
subgroup testing in appendix E, table E-IX of MIL-PRF-19500 and as specified herein. Electrical measurements
(end-points) shall be in accordance with table I, subgroup 2 herein.
8
MIL-PRF-19500/742A
4.5 Methods of inspection. Methods of inspection shall be as specified in the appropriate tables as follows.
4.5.1 Pulse measurements. Conditions for pulse measurement shall be as specified in section 4 of MIL-STD-750.
4.5.2 Scope display evaluation. Scope display evaluation shall be stable in accordance with method 4023 of
MIL-STD-750, condition A. Scope display may be performed on ATE (automatic test equipment) for screening only
with the approval of the qualifying activity. Scope display in table I, subgroup 4 shall be performed on a curve tracer.
The reverse current (IBR) over the knee shall be 500 µA peak.
4.5.3 Burn-in and life tests. These tests shall be conducted with a half-sine waveform of the specified peak voltage
impressed across the diode in the reverse direction followed by a half-sine waveform of the specified average
rectified current. The forward conduction angle of the rectified current shall be neither greater than 180 degrees, nor
less than 150 degrees.
4.5.3.1 Free air burn-in and life tests. The use of a current limiting or ballast resistor is permitted provided that
each DUT still sees the minimum IO or IF and that the minimum applied voltage, where applicable, is maintained
through-out the burn-in period. Use method 3100 of MIL-STD-750 to measure TJ.
4.5.4 Thermal resistance. Thermal resistance measurement shall be performed in accordance with method 4081
of MIL-STD-750 using the guidelines in that method for determining IM, IH, and tH. Measurement delay time tMD = 70
µs max. See table E-IX of MIL-PRF-19500, subgroup 4, and figures 3, 4, 5, and 6 herein. Forced moving air or draft
shall not be permitted across the device during test.
9
MIL-PRF-19500/742A
TABLE I. Group A inspection.
Inspection
1/
MIL-STD-750
Conditions
Limit
Unit
Symbol
Method
2071
Min
Max
Subgroup 1
Visual and mechanical
examination
Subgroup 2
Thermal impedance 2/
Forward voltage
3101
4011
See 4.3.1
°C/W
Z
θJX
Duty cycle ≤ 2 percent (pulsed
see 4.5.1); tp = 8.3 ms (max)
1N5802CB, CBUS,
1N5804CB, CBUS,
1N5806CB, CBUS
0.875
0.975
V
V
IFM = 1.0 A
IFM = 2.5 A
VFM1
1N5802CB, CBUS,
1N5804CB, CBUS,
1N5806CB, CBUS
VFM2
Forward voltage
4011
Duty cycle ≤ 2 percent (pulsed
see 4.5.1); tp = 8.3 ms (max)
1N5807CB, CBUS,
1N5809CB, CBUS,
1N5811CB, CBUS
0.865
0.875
0.925
V
V
V
IFM = 3.0 A
IFM = 4.0 A
VFM3
VFM4
VFM5
IR1
1N5807CB, CBUS,
1N5809CB, CBUS,
1N5811CB, CBUS
1N5807CB, CBUS
1N5809CB, CBUS
1N5811CB, CBUS
IFM = 6.0 A
Reverse current
4016
DC or equivalent pulse method
1N5802CB, CBUS
1N5804CB, CBUS
1N5806CB, CBUS
1N5807CB, CBUS
1N5809CB, CBUS
1N5811CB, CBUS
1.0
1.0
1.0
5.0
5.0
5.0
µA
µA
µA
µA
µA
µA
VR = 50 V
VR = 100 V
VR = 150 V
VR = 50 V
VR = 100 V
VR = 150 V
See footnotes at end of table.
10
MIL-PRF-19500/742A
TABLE I. Group A inspection - Continued.
Inspection
1/
MIL-STD-750
Limit
Unit
Symbol
Method
4021
Conditions
Min
Max
Subgroup 2 - continued
Breakdown voltage
I(BR) = 100 µA
V(BR)1
1N5802CB, CBUS,
1N5807CB, CBUS
60
V
V
V
1N5804CB, CBUS,
1N5809CB, CBUS
110
160
1N5806CB, CBUS,
1N5811CB, CBUS
Subgroup 3
High temperature
operation:
TA = +125°C minimum.
Reverse current
4016
DC or equivalent pulse method
IR2
1N5802CB, CBUS
1N5804CB, CBUS
175
175
µA
µA
VR = 50 V
VR = 100 V
1N5806CB, CBUS
1N5807CB, CBUS
1N5809CB, CBUS
1N5811CB, CBUS
175
525
525
525
µA
µA
µA
µA
VR = 150 V
VR = 50 V
VR = 100 V
VR = 150 V
Forward voltage
4011
Duty cycle ≤ 2 percent (pulsed
see 4.5.1); tp = 8.3 ms (max)
1N5802CB, CBUS,
1N5804CB, CBUS,
1N5806CB, CBUS
0.800
0.800
V
V
IFM = 1.0 A
IFM = 4.0 A
VFM6
1N5807CB, CBUS,
1N5809CB, CBUS,
1N5811CB, CBUS
VFM7
See footnotes at end of table.
11
MIL-PRF-19500/742A
TABLE I. Group A inspection - Continued.
Inspection
1/
MIL-STD-750
Limit
Unit
Symbol
Method
4011
Conditions
Min
Max
Low-temperature
operation:
TA = -65°C minimum.
Forward voltage
Duty cycle ≤ 2 percent (pulsed
see 4.5.1); tp = 8.3 ms (max)
1N5802CB, CBUS,
1N5804CB, CBUS,
1N5806CB, CBUS
1.075
1.075
V
V
IFM = 1.0 A
IFM = 4.0 A
I(BR) = 100 µA
VFM8
VFM9
V(BR)2
1N5807CB, CBUS,
1N5809CB, CBUS,
1N5811CB, CBUS
Breakdown voltage
4021
1N5802CB, CBUS,
1N5807CB, CBUS
50
V
V
V
1N5804CB, CBUS,
1N5809CB, CBUS
100
150
1N5806CB, CBUS,
1N5811CB, CBUS
Subgroup 4
Reverse recovery time
4031
Condition B
trr
1N5802CB, CBUS,
1N5804CB, CBUS,
1N5806CB, CBUS
25
30
ns
ns
IF = IRM = 0.5 A
IR (REC) = 0.05 A(pk)
di/dt = 65 A/µs (min)
1N5807CB, CBUS,
1N5809CB, CBUS,
1N5811CB, CBUS
IF = IRM = 1.0 A
IR (REC) = 0.1 A(pk)
di/dt = 100 A/µs (min)
Capacitance
4001
VR = 10 V; f = 1 MHz;
Vsig = 50 mV (p-p)
CJ
1N5802CB, CBUS,
1N5804CB, CBUS,
1N5806CB, CBUS
25
60
pF
pF
1N5807CB, CBUS,
1N5809CB, CBUS,
1N5811CB, CBUS
See footnotes at end of table.
12
MIL-PRF-19500/742A
TABLE I. Group A inspection - Continued.
Inspection
1/
MIL-STD-750
Limit
Unit
Symbol
Method
4026
Conditions
Min
Max
Subgroup 4 - continued
Forward recovery voltage
tr = 8 ns
V(peak)
1N5802CB, CBUS,
1N5804CB, CBUS,
1N5806CB, CBUS
2.2
2.2
V (pk)
V (pk)
IF = 250 mA
1N5807CB, CBUS,
1N5809CB, CBUS,
1N5811CB, CBUS
IF = 500 mA
Forward recovery time
4026
tp ≥ 20 ns, tr = 8 ns, the test is
tfr
measured at VFR = 1.1 x VF
1N5802CB, CBUS,
1N5804CB, CBUS,
1N5806CB, CBUS
15
15
ns
ns
IFM = 250 mA
IFM = 500 mA
1N5807CB, CBUS,
1N5809CB, CBUS,
1N5811CB, CBUS
Scope display evaluation
Subgroup 5
4023
4066
See 4.5.2, n = 116, c = 0
Not applicable
Subgroup 6
Forward surge
IFSM = rated (see 1.3.2); ten
surges of 8.3 ms each at 1
minute intervals superimposed
on IO = IO1 rated (see 1.3.2);
VRWM = rated (see 1.3.2); TA =
+ 25°C.
Electrical measurements
See table I, subgroup 2 except
ZθJX
.
Subgroup 7
Not applicable
1/ For sampling plan, see MIL-PRF-19500.
2/ Not applicable to JANHC and JANKC devices.
13
MIL-PRF-19500/742A
* TABLE II. Group E inspection (all quality levels) for qualification and requalification only.
Inspection
MIL-STD-750
Conditions
Sampling
plan
Method
Subgroup 1A
45 devices
c = 0
Temperature cycling (air
to air)
1051
1071
20 cycles, except high temperature shall be 150°C and
low temperature shall be -195°C.
Hermetic seal
Electrical measurement
Subgroup 1B
See table I, subgroup 2.
45 devices
c = 0
Temperature cycling (air
to air)
1051
1071
-65°C to +175°C, 500 cycles.
Hermetic seal
Electrical measurement
Subgroup 2
See table I, subgroup 2.
22 devices
c = 0
Steady-state dc blocking
life
1048
t = 1,000 hours; TA = +150°C; VR dc = 80 - 85 percent
rated VRWM (see 1.3.2).
Electrical measurement
See table I, subgroup 2, except ZθJX need not to be
performed. For irradiated devices, include trr, VF, and IR
as end-point measurements.
Sample size
N/A
Subgroup 4
Thermal impedance
curves
See MIL-PRF-19500.
Subgroups 5 and 6
Not applicable
14
MIL-PRF-19500/742A
* TABLE II. Group E inspection (all quality levels) for qualification and requalification only - Continued.
Inspection
MIL-STD-750
Conditions
Sampling
plan
Method
4065
Subgroup 8
n = 45
Peak reverse power
Peak reverse power, (PRM) = shall be characterized by
the supplier and this data shall be available to the
Government. Test shall be performed on each sublot.
Electrical measurement
During the PRM test, the voltage (VBR) shall be monitored
to verify it has not collapsed. Any collapse in VBR during
or after the PRM test or rise in leakage current (IR) after
the test that exceeds IR1 in table I shall be considered a
failure to that level of applied PRM. Progressively higher
levels of PRM shall be applied until failure occurs on all
devices within the chosen sample size.
Subgroup 9
n = 45
Resistance to glass
cracking
1057
4066
Step stress to destruction by increasing cycles or up to a
maximum of 25 cycles.
Subgroup 10
22 devices
c = 0
Forward surge
Condition A, IFSM = rated (see 1.3.2); ten surges of 8.3
ms each at 1 minute intervals superimposed on IO = IO1
rated (see 1.3.2); VRWM = rated (see 1.3.2); TA = + 25°C.
Electrical measurement
See table I, subgroup 2.
15
MIL-PRF-19500/742A
Maximum Thermal Impedance
50
Design Curve
10
5
1
0.5
0.001
0.01
0.1
1
10
50
Heating Time (sec)
Z
θJX = 4°C/W at 10 ms.
FIGURE 3. Thermal impedance curve, R
θJL
= 36°C/W for 1N5802CB, 1N5804CB, 1N5806CB.
16
MIL-PRF-19500/742A
Maximum Thermal Impedance
20
10
5
Design Limit
1
0.005 0.01
0.1
1
10
50
Heating Time (sec)
Z
θJX = 4°C/W at 10 ms.
FIGURE 4. Thermal impedance curve R
θJEC
= 13°C/W for 1N5802CBUS, 1N5804CBUS, 1N5806CBUS.
17
MIL-PRF-19500/742A
Maximum Thermal Impedance
50
Design Limit
10
5
1
0.5
0.2
0.001
0.01
0.1
1
10
50
Heating Time (sec)
Z
θJX = 1.5°C/W at 10 ms.
FIGURE 5. Thermal impedance curve R
θJL
= 22°C/W for 1N5807CB, 1N5809CB, 1N5811CB.
18
MIL-PRF-19500/742A
Maximum Thermal Impedance
10
5
Design Limit
1
0.5
0.2
0.001
0.01
0.1
1
10 20
Heating Time (sec)
Z
θJX = 1.5°C/W at 10 ms.
FIGURE 6. Thermal impedance curve R
θJEC
= 6.5°C/W for 1N5807CBUS, 1N5809CBUS, 1N5811CBUS.
19
MIL-PRF-19500/742A
FIGURE 7. US terminal strength mounting.
20
MIL-PRF-19500/742A
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 3.4.2).
d. Product assurance level and type designator.
* 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
Defense Supply Center, Columbus, ATTN: DSCC/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 http://assist.daps.dla.mil.
6.4 Applications data.
6.4.1 Half-sine-wave application with 1N5807CB(US) to 1N5811CB(US). For a PCB mounting example with FR4
material where the full 3 amp IO rating (half-sine-wave) is used at a TJ of 175ºC and ambient temperature of 55ºC,
the following steps guide the user in what the PCB pad size will need to be with 1 oz, 2 oz, and 3 oz copper for a
1N5807CB to 1N5811CB or 1N5807CBUS to 1N5811CBUS. For axial-leaded, the lead length for mounting will be
.187 inch (4.76 mm) or less from body to entry point on PCB surface. See 6.4.3 for the smaller example devices
1N5802CB to 1N5806CB or 1N5802CB(US) to 1N5806CB(US).
a. Use the IO versus Po curve on figure 8 to look up 3 amps (X-axis) and follow up to the TJ =175ºC curve (lower)
for 2.30 watts.
b. Calculate maximum thermal resistance needed (175ºC - 55ºC) / 2.30 W = 52ºC/W.
c. Look up thermal resistance of 52ºC/W on Y-axis using a thermal resistance versus pad area plot on one of the
three curves on figure 9 for different weights of copper cladding and then intersect curve horizontally to get
answer. These curves assume still air, horizontal position.
d. In this example, the answer is: 1 oz PCB = .5 in2 (1.27 mm2), 2 oz PCB = .3 in2 (0.76 mm2), 3 oz PCB =
.2 in2 (0.51 mm2) for each pad.
e. Add a conservative guard-band to the pad size (larger) to keep TJ below 175ºC.
21
MIL-PRF-19500/742A
6.4.2 Square-wave application with 1N5807CB(US) to 1N5811CB(US). For a PCB mounting example with FR4
material to support a 1 amp IO square wave switching at a 0.50 duty factor (50 percent duty cycle) at TJ = 125ºC and
ambient temperature of 55ºC, the following steps guide the user in what the PCB pad size will need to be with 1 oz, 2
oz, and 3 oz copper.
a. Find size of copper pads on standard FR4 PCB to support operation at 1 amp IO square wave switching at a
0.50 duty factor (50 percent duty cycle) at TJ = 125ºC with TA = 55ºC.
b. Calculate peak IF = 1 A / 0.50 duty factor = 2 amps.
c. Use the VF versus IF curve on figure 10 to look up IF = 2 A (Y-axis) and follow across to the TJ = 125ºC curve
(middle) for VF = 0.65 V.
d. Calculate power = IF * VF * duty factor = 2 * 0.65 * 0.50 = 0.65 W.
e. Calculate maximum thermal resistance needed (125ºC – 55ºC) / 0.65 W = 107ºC/W.
f. Look up thermal resistance of 107ºC/W on the Y-axis using a thermal resistance versus pad area plot on one
of the three curves on figure 9 for different weights of copper cladding and then intersect curve horizontally to
get answer. Curves assume still air, horizontal position.
g. In this example, the answer is: 1 oz PCB = .058 in2 (1.4732 mm2), 2 oz PCB = .038 in2 (0.9652 mm2),
3 oz PCB = .024 in2 (0.6096 mm2) for each pad.
h. A conservative pad guard-band is optional since TJ is only 125ºC. NOTE: Multilayer PCBs, forced air cooling
will improve performance. Closed confinement of the PCB will do the opposite. Use sound thermal
management.
6.4.3 Half-sine-wave application with 1N5802CB(US) to 1N5806CB(US). For a PCB mounting example with FR4
material where the full 1 amp IO rating (half-sine-wave) is used at a TJ of 175ºC and ambient temperature of 55ºC,
the following steps guide the user in what the PCB pad size will need to be with 1 oz, 2 oz, and 3 oz copper for a
1N5802CB to 1N5806CB or 1N5802CB(US) to 1N5806CB(US). For axial-leaded, the lead length for mounting will
be .187 inch (4.76 mm) or less from body to entry point on PCB surface.
a. Use the IO versus Po curve on figure 11 to look up 1 amp (X-axis) and follow up to the TJ = 175ºC curve
(lower) for 0.78 watts.
b. Calculate maximum thermal resistance needed (175ºC – 55ºC) / 0.78 W = 154ºC/W.
c. Look up thermal resistance of 154ºC/W on Y-axis using a thermal resistance versus pad area plot on one of
the three curves on figure 12 for different weights of copper cladding and then intersect curve horizontally to
get answer. These curves assume still air, horizontal position.
d. In this example, the answer is: 1 oz PCB = .013 in2 (0.3302 mm2), 2 oz PCB = .008 in2 (0.2032 mm2), 3 oz
PCB = .0053 in2 (0.13462 mm2) for each pad.
e. Add a conservative guard-band to the pad size (larger) to keep TJ below 175ºC.
22
MIL-PRF-19500/742A
6.4.4 Square-wave application with 1N5802CB(US) to 1N5806CB(US). For a PCB mounting example with FR4
material to support a 0.5 amp IO square wave switching at a 0.50 duty factor (50 percent duty cycle) at TJ = 125ºC
and ambient temperature of 55ºC, the following steps guide the user in what the PCB pad size will need to be with 1
oz, 2 oz, and 3 oz copper.
a. Find size of copper pads on standard FR4 PCB to support operation at 0.5 amp IO square wave switching at a
0.50 duty factor (50 percent duty cycle) at TJ = 125ºC with TA = 55ºC.
b. Calculate peak IF = 0.5A / 0.50 duty factor = 1 amp.
c. Use the VF versus IF curve on figure 13 to look up IF = 1 A (Y-axis) and follow across to the TJ = 125ºC curve
(middle) for VF = 0.70 V.
d. Calculate power = IF * VF * duty factor = 2 * 0.70 * 0.50 = 0.70 W.
e. Calculate maximum thermal resistance needed (125ºC – 55ºC) / 0.70 W = 100ºC/W.
f. Look up thermal resistance of 100ºC/W on the Y-axis using a thermal resistance versus pad area plot on one of
the three curves on figure 12 for different weights of copper cladding and then intersect curve horizontally to get
answer. Curves assume still air, horizontal position.
g. In this example, the answer is: 1 oz PCB = .084 in2 (2.1336 mm2), 2 oz PCB = .051 in2 (1.2954 mm2), 3 oz PCB
= .034 in2 (0.8636 mm2) for each pad.
h. A conservative pad guard-band is optional since TJ is only 125ºC. NOTE: Multilayer PCBs, forced air cooling,
will improve performance. Closed confinement of the PCB will do the opposite. Use sound thermal
management.
23
MIL-PRF-19500/742A
5
4.5
4
3.5
3
2.5
2
1.5
1
Po (W) for: Model @ Tj=25C
Po (W) for: Model @ Tj=90C
Po (W) for: Model @ Tj=125C
Po (W) for: Model @ Tj=175C
0.5
0
0.00
1.00
2.00
3.00
4.00
5.00
6.00
Io (A)
FIGURE 8. Rectifier power versus IO (average forward current) for 1N5807CB(US) to 1N5811CB(US).
24
MIL-PRF-19500/742A
1000
100
10
1oz Foil
2oz Foil
3oz Foil
0.001
0.01
0.1
1
10
100
Pad Area per Pad (in2)
FIGURE 9. Thermal resistance versus pad area still air, PCB horizonal (for each pad) with 1, 2, and 3 oz copper for
1N5807CB(US) to 1N5811CB(US).
25
MIL-PRF-19500/742A
s
0.30
10
0.40
0.50
0.60
0.70
0.80
0.90
1.00
1
Model @ Tj=25C
Model @ Tj=90C
Model @ Tj=125C
Model @ Tj=175C
0.1
Vf (V)
FIGURE 10. Forward voltage versus forward current for 1N5807CB(US) to 1N5811CB(US).
26
MIL-PRF-19500/742A
3.5
3
2.5
2
1.5
1
Po (W) for: Model @ Tj=25C
Po (W) for: Model @ Tj=90C
Po (W) for: Model @ Tj=125C
Po (W) for: Model @ Tj=175C
0.5
0
0.00
0.50
1.00
1.50
2.00
2.50
3.00
Io (A)
FIGURE 11. Rectifier power versus IO (average forward current) for 1N5802CB(US) to 1N5806CB(US).
27
MIL-PRF-19500/742A
1000
100
10
1oz Foil
2oz Foil
3oz Foil
0.001
0.01
0.1
1
10
100
Pad Area (in2)
FIGURE 12. Thermal resistance versus pad area still air, PCB horizontal (for each pad) with 1, 2, and 3 oz copper
for 1N5802CB(US) to 1N5806CB(US).
28
MIL-PRF-19500/742A
0.20
10
0.30
0.40
0.50
0.60
0.70
0.80
0.90
1.00
1.10
1.20
1
0.1
Model @ Tj=25C
Model @ Tj=90C
Model @ Tj=125C
Model @ Tj=175C
0.01
0.001
Vf (V)
FIGURE 13. Forward voltage versus forward current for 1N5802CB(US) to 1N5806CB(US).
29
MIL-PRF-19500/742A
6.5 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
Navy - EC
Air Force - 85
NASA - NA
DLA - CC
Preparing activity:
DLA - CC
(Project 5961-2008-091)
Review activities:
Army - AR, AV, MI, SM
Navy - AS, MC
Air Force - 19, 71, 99
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 http://assist.daps.dla.mil.
30
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