RDC5028C 5962-0423503

REVISIONS
LTR
DESCRIPTION
DATE (YR-MO-DA)
APPROVED
A
Add device type 02. 1.2.2, device type 01, change the generic
number to ACT5028-201.
09-03-30
Joseph D. Rodenbeck
B
Added device type 03. Replaced figure 6. Changed paragraph 6.8 to
include the device type 03 and make corrections. -sld
10-09-14
Charles F. Saffle
C
Table I; Added footnote 2 to the Input capacitance test (CIN) and
separated the device type 03 from device type 01 and 02 with a max
limit of 120 ns for CW/CCW, RIPPLE, B1-B16 rise and fall time test. sld
10-10-27
Charles F. Saffle
D
Added radiation hardness assurance requirements. Paragraph 1.3;
Added Power Dissipation (PD) rating. Corrected Maximum junction
temperature from "135°C" to "150°C". Table I; Added "Operating
Supply Current (ISC)" test. Corrected the subgroups from "1,2,3" to
"4,5,6" and added footnote 4 for the VCO frequency (fVCO) test. Table
II; Added subgroup 1 for Interim electrical parameters. -sld
12-12-17
Charles F. Saffle
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PMIC N/A
PREPARED BY
Steve Duncan
STANDARD
MICROCIRCUIT
DRAWING
CHECKED BY
Raymond Monnin
THIS DRAWING IS
AVAILABLE
FOR USE BY ALL
DEPARTMENTS
APPROVED BY
Raymond Monnin
AND AGENCIES OF THE
DEPARTMENT OF DEFENSE
AMSC N/A
DLA LAND AND MARITIME
COLUMBUS, OHIO 43218-3990
http://www.landandmaritime.dla.mil/
MICROCIRCUIT, LINEAR, RESOLVER-TODIGITAL CONVERTER, 16-BIT, TRACKING,
MONOLITHIC SILICON
DRAWING APPROVAL DATE
04-10-01
REVISION LEVEL
D
SIZE
CAGE CODE
A
67268
SHEET
DSCC FORM 2233
APR 97
1 OF
5962-04235
31
5962-E411-12
1. SCOPE
1.1 Scope. This drawing documents five product assurance classes as defined in paragraph 1.2.3 and MIL-PRF-38534. A
choice of case outlines and lead finishes which are available and are reflected in the Part or Identifying Number (PIN). When
available, a choice of radiation hardness assurance levels are reflected in the PIN.
1.2 PIN. The PIN shall be as shown in the following example:
5962



Federal
stock class
designator
\
H



RHA
designator
(see 1.2.1)
04235
03



Device
type
(see 1.2.2)
/
K



Device
class
designator
(see 1.2.3)
X



Case
outline
(see 1.2.4)
X



Lead
finish
(see 1.2.5)
\/
Drawing number
1.2.1 Radiation hardness assurance (RHA) designator. RHA marked devices shall meet the MIL-PRF-38534 specified RHA
levels and shall be marked with the appropriate RHA designator. A dash (-) indicates a non-RHA device.
1.2.2 Device type(s). The device type(s) identify the circuit function as follows:
Device type
Generic number
01
02
03
Circuit function
ACT5028-201
ACT5028-202
RDC5028-301
Resolver-to-digital converter, tracking, 16-bit
Resolver-to-digital converter, tracking, 16-bit
Resolver-to-digital converter, tracking, 16-bit
1.2.3 Device class designator. This device class designator shall be a single letter identifying the product assurance level.
All levels are defined by the requirements of MIL-PRF-38534 and require QML Certification as well as qualification (Class H, K,
and E) or QML Listing (Class G and D). The product assurance levels are as follows:
Device class
Device performance documentation
K
Highest reliability class available. This level is intended for use in space
applications.
H
Standard military quality class level. This level is intended for use in applications
where non-space high reliability devices are required.
G
Reduced testing version of the standard military quality class. This level uses the
Class H screening and In-Process Inspections with a possible limited temperature
range, manufacturer specified incoming flow, and the manufacturer guarantees (but
may not test) periodic and conformance inspections (Group A, B, C, and D).
E
Designates devices which are based upon one of the other classes (K, H, or G)
with exception(s) taken to the requirements of that class. These exception(s) must
be specified in the device acquisition document; therefore the acquisition document
should be reviewed to ensure that the exception(s) taken will not adversely affect
system performance.
D
Manufacturer specified quality class. Quality level is defined by the manufacturers
internal, QML certified flow. This product may have a limited temperature range.
STANDARD
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REVISION LEVEL
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SHEET
2
1.2.4 Case outline(s). The case outline(s) are as designated in MIL-STD-1835 and as follows:
Outline letter
X
Descriptive designator
See figure 1
Terminals
Package style
52
Ceramic, quad flat package
1.2.5 Lead finish. The lead finish shall be as specified in MIL-PRF-38534.
1.3 Absolute maximum ratings. 1/
Positive supply voltage range (VCC and VDD).............................. ..................
Analog output current (Output shorted to GND)......................... ..................
Digital output current (Output shorted to GND) .............................................
Analog input voltage range ...........................................................................
Digital input voltage range ............................................................................
Power dissipation (PD), TC = -55°C to +125°C ..............................................
Thermal resistance, junction-to-case (θJC) ....................................................
Junction temperature (TJ)......................................................... .....................
Storage temperature .....................................................................................
Lead temperature (soldering, 10 seconds) ...................................................
-0.5 V dc to +7.0 V dc
32 mA
18.6 mA
-0.3 V to (VCC + .3 V)
-0.3 V to (VDD + .3 V)
200 mW
1.25°C/W
+150°C
-65°C to +150°C
+300°C
1.4 Recommended operating conditions.
Operating voltage range (VCC and VDD) ..........................................................
Operating current (ICC + IDD) ...........................................................................
Ambient operating temperature range (TA).....................................................
+4.5 V dc to +5.5 V dc
23 mA
-55°C to +125°C
1.5 Radiation features. 2/
Total Ionizing Dose (TID) ...... (dose rate = 50 - 300 rad(Si)/s):
In accordance with MIL-STD-883, method 1019, condition A....................
Enhanced Low Dose Rate Sensitvity (ELDRS).............................................
Single event phenomenon (SEP) effective linear energy transfer (LET):
No SEL ......................................................................................................
1 Mrad(Si)
CMOS Immune
2
< 100 MeV-cm /mg 3/ 4/
2. APPLICABLE DOCUMENTS
2.1 Government specification, standards, and handbooks. The following specification, standards, and handbooks form a part
of this drawing to the extent specified herein. Unless otherwise specified, the issues of these documents are those cited in the
solicitation or contract.
DEPARTMENT OF DEFENSE SPECIFICATION
MIL-PRF-38534 - Hybrid Microcircuits, General Specification for.
DEPARTMENT OF DEFENSE STANDARDS
MIL-STD-883 - Test Method Standard Microcircuits.
MIL-STD-1835 - Interface Standard for Electronic Component Case Outlines.
_________
1/ Stresses above the absolute maximum ratings may cause permanent damage to the device. Extended operation at the
maximum levels may degrade performance and affect reliability.
2/ See section 4.3.5 for the manufacturer's radiation hardness assurance analysis and testing.
2
3/ Single event testing was performed at 100 MeV-cm /mg with no latch-up exhibited.
4/ See table IB.
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REVISION LEVEL
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SHEET
3
DEPARTMENT OF DEFENSE HANDBOOKS
MIL-HDBK-103 - List of Standard Microcircuit Drawings.
MIL-HDBK-780 - Standard Microcircuit Drawings.
(Copies of these documents are available online at https://assist.dla.mil/quicksearch/ or from the Standardization Document
Order Desk, 700 Robbins Avenue, Building 4D, Philadelphia, PA 19111-5094.)
2.2 Non-Government publications. The following documents form a part of this document to the extent specified herein.
AMERICAN SOCIETY FOR TESTING AND MATERIALS (ASTM)
ASTM F 1192
- Standard Guide for the Measurement of Single Event Phenomena (SEP) Induced by
Heavy Ion Irradiation of Semiconductor Devices.
2.3 Order of precedence. In the event of a conflict between the text of this drawing and the references cited herein, the text
of this drawing takes precedence. Nothing in this document, however, supersedes applicable laws and regulations unless a
specific exemption has been obtained.
3. REQUIREMENTS
3.1 Item requirements. The individual item performance requirements for device classes D, E, G, H, and K shall be in
accordance with MIL-PRF-38534. Compliance with MIL-PRF-38534 shall include the performance of all tests herein or as
designated in the device manufacturer's Quality Management (QM) plan or as designated for the applicable device class. The
manufacturer may eliminate, modify or optimize the tests and inspections herein, however the performance requirements as
defined in MIL-PRF-38534 shall be met for the applicable device class. In addition, the modification in the QM plan shall not
affect the form, fit, or function of the device for the applicable device class.
3.2 Design, construction, and physical dimensions. The design, construction, and physical dimensions shall be as specified
in MIL-PRF-38534 and herein.
3.2.1 Case outline(s). The case outline(s) shall be in accordance with 1.2.4 herein and figure 1.
3.2.2 Terminal connections. The terminal connections shall be as specified on figure 2.
3.2.3 Block diagram. The block diagram shall be as specified on figure 3.
3.2.4 Functional Block diagram. The functional block diagram shall be as specified on figure 4.
3.2.5 Transfer function diagram. The transfer function diagram shall be as specified on figure 5.
3.2.6 Timing diagram(s). The timing diagram(s) shall be as specified on figure 6.
3.2.7 Radiation exposure circuits. The radiation exposure circuits shall be maintained by the manufacturer under document
revision level control and shall be made available to the preparing and acquiring activity upon request.
3.3 Electrical performance characteristics. Unless otherwise specified herein, the electrical performance characteristics are
as specified in table I and shall apply over the full specified operating temperature range.
3.4 Electrical test requirements. The electrical test requirements shall be the subgroups specified in table II. The electrical
tests for each subgroup are defined in table IA.
3.5 Marking of device(s). Marking of device(s) shall be in accordance with MIL-PRF-38534. The device shall be marked with
the PIN listed in 1.2 herein. In addition, the manufacturer's vendor similar PIN may also be marked.
STANDARD
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REVISION LEVEL
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4
3.6 Data. In addition to the general performance requirements of MIL-PRF-38534, the manufacturer of the device described
herein shall maintain the electrical test data (variables format) from the initial quality conformance inspection group A lot sample,
for each device type listed herein. Also, the data should include a summary of all parameters manually tested, and for those
which, if any, are guaranteed. This data shall be maintained under document revision level control by the manufacturer and be
made available to the preparing activity (DLA Land and Maritime -VA) upon request.
3.7 Certificate of compliance. A certificate of compliance shall be required from a manufacturer in order to supply to this
drawing. The certificate of compliance (original copy) submitted to DLA Land and Maritime - VA shall affirm that the
manufacturer's product meets the performance requirements of MIL-PRF-38534 and herein.
3.8 Certificate of conformance. A certificate of conformance as required in MIL-PRF-38534 shall be provided with each lot of
microcircuits delivered to this drawing.
STANDARD
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REVISION LEVEL
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TABLE IA. Electrical performance characteristics.
Test
Symbol
Conditions 1/
-55°C ≤ TA ≤ +125°C
VCC = VDD = +5 V dc
unless otherwise specified
Group A
subgroups
Device
types
Limits
Min
Unit
Max
DC PARAMETERS
Operating Supply Current
2/
ISC
VCC = VDD = +5.5 V dc
1,2,3
All
35
mA
Accuracy 2/ 3/
ACC
Add 1 LSB for total error
1,2,3
All
±5
Minutes
1,2,3
All
1
LSB
1,2,3
All
Repeatability
Resolution per LSB, 2/
(see paragraph 6.8)
RES
10 Bit Mode
12 Bit Mode
14 Bit Mode
16 Bit Mode
10 Bit Mode
12 Bit Mode
14 Bit Mode
16 Bit Mode
Maximum tracking rate 2/
10 Bit Mode
12 Bit Mode
14 Bit Mode
16 Bit Mode
SC1 SC2 Bits used
0
0 B1 - B10
0
1 B1 - B12
1
0 B1 - B14
1
1 B1 - B16
1,2,3
0.35
0.09
0.022
0.0055
Degrees
21.1
5.27
1.32
0.33
Minutes
All
1024
256
64
16
RPS
1.05
MHz
VCO frequency 4/
ANALOG INPUTS
fVCO
4,5,6
All
Voltage between ± analog
signal inputs,
±SIN, ±COS, ±REF 2/ 4/
VSIN,VCOS,
VREF
4,5,6
All
1.0
1.5
Vrms
Reference input
frequency, ±REF 4/
fREF
4,5,6
All
45
30K
Hz
Input impedance 4/
ZIN
TA = +25°C and +125°C
1,2
All
2.5
Input capacitance 4/
CIN
TA = +25°C
1
All
DC voltage bias on -SIN,
and -COS
VB
1,2,3
All
Input bias current 2/
IB
1
All
2
MΩ
15
pF
2.0
2.5
V dc
-100
+100
-1000
+1000
nA
See footnotes at end of table.
STANDARD
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REVISION LEVEL
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TABLE IA. Electrical performance characteristics - Continued.
Test
Symbol
Conditions 1/
-55°C ≤ TA ≤ +125°C
VCC = VDD = +5 V dc
unless otherwise specified
Group A
subgroups
Device
types
Limits
Min
Unit
Max
DC PARAMETERS - CONTINUED, DIGITAL INPUTS
ENABLE, DATA LOAD, INH, SC1, and SC2
Input low voltage
4/
VIL
1,2,3
All
Input high voltage 4/
VIH
1,2,3
All
2.0
Input leakage current 2/
ILI
1
All
-200
+200
nA
-2000
+2000
nA
2
Input impedance 2/
ZIN
TA = +25°C and +125°C
Input capacitance 4/
CIN
0.8
V dc
V dc
1,2
All
2.5
TA = +25°C
1
All
15
pF
0.3
V dc
MΩ
DIGITAL OUTPUTS
BUSY, RIPPLE, and CW / CCW
Output low voltage 2/
VOL
IOL = 1.6 mA
1,2,3
All
Output high voltage 2/
VOH
IOH = -1.6 mA
1,2,3
All
VLI/O - .8
V dc
DIGITAL I/O, B1 - B16 5/
Input low voltage
4/
VIL
1,2,3
All
Input high voltage 4/
VIH
1,2,3
All
Output low voltage 2/
VOL
IOL = 1.6 mA
1,2,3
All
Output high voltage 2/
VOH
IOH = -1.6 mA
1,2,3
All
VLI/O - .8
Input leakage current 2/
ILI
1
All
-200
+200
nA
-2000
+2000
nA
-200
+200
nA
-2000
+2000
nA
2
High-Z leakage current 4/
IZ
1
2
All
0.8
V dc
2.0
V dc
0.3
V dc
V dc
See footnotes at end of table.
STANDARD
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TABLE IA. Electrical performance characteristics - Continued.
Test
Symbol
Conditions 1/
-55°C ≤ TA ≤ +125°C
VCC = VDD = +5 V dc
unless otherwise specified
Group A
subgroups
Device
types
Limits
Min
Unit
Max
AC TIMING, DIGITAL OUTPUT, CL = 50 pF
BUSY rise and fall time 2/
tLH, tHL
See figure 6
9,10,11
All
85
ns
CW / CCW, RIPPLE, B1 − B16
rise and fall time
tLH, tHL
See figure 6
9,10,11
01, 02
100
ns
03
120
2/
BUSY pulse width 2/
tBPW
See figure 6
9,10,11
All
BUSY to data stable 4/
tBDS
ENABLE = low,
See figure 6
9,10,11
All
RIPPLE pulse width
2/
tRPW
See figure 6
9,10,11
All
BUSY to RIPPLE
4/
tBR
See figure 6
9,10,11
300
600
ns
350
ns
300
ns
All
150
ns
140
READ DATA, ENABLE and INH are tied together , DATA LOAD = log ic Hi, CL = 50 pF
ENABLE low to data stable
4/
tELDS
See figure 6
9,10,11
All
70
ns
ENABLE high to data Hi − Z
4/
tEHZ
See figure 6
9,10,11
All
70
ns
INH low to data stable
4/
tILDS
See figure 6
9,10,11
All
400
ns
INH high to data change
4/
tIHZ
See figure 6
9,10,11
All
150
ns
WRITE DATA, ENABLE and INH = log ic Hi, CL = 50 pF
DATA LOAD pulse width
4/
tDLPW
See figure 6
9,10,11
All
200
ns
Data setup to DATA LOAD
4/
tWDS
See figure 6
9,10,11
All
60
ns
Data hold 4/
tWDH
See figure 6
9,10,11
All
10
ns
See foonotes at top of next page.
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REVISION LEVEL
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TABLE IA. Electrical performance characteristics - Continued.
1/
For radiation features see paragraph 1.5 herein.
2/
This device has been tested to (1.5 Mrad(Si)) to ensure RHA designator level "H" (1 Mrad(Si)) of Method 1019, condition
A of MIL-STD-883 at +25°C for these parameters. This device will be re-tested after design or process changes that can
affect RHA response of this device
3/
Accuracy applies over the full operating power supply voltage range, Full operating temperature range, reference
frequency range, 10 percent signal amplitude variation, and 10 percent reference harmonic distortion.
4/
Parameter shall be tested as part of device characterization and after design and process changes. Thereafter,
parameters shall be guaranteed to the limits specified in table IA.
5/
All unused inputs shall be tied to ground. Bit 1 is always the MSB.
TABLE IB. SEP test limits. 1/
Device type
SEP
Temperature (TC)
Effective linear energy
transfer (LET)
03
No SEL
(Destructive)
+125°C
≤ 100 MeV-cm /mg
2
1/ For SEP test conditions, see 4.3.5.1.2.2 herein.
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Symbol
A
A1
A2
b
b1
c
D/E
D1/E1
e
L
Millimeters
Min
Max
2.54
1.42
1.78
0.20 REF
0.58 TYP
0.43 TYP
0.13
0.20
24.28
15.11
15.37
1.27 TYP
6.30
6.40
Inches
Min
Max
.100
.056
.070
.008 REF
.023 TYP
.017 TYP
.005
.008
.956
.595
.605
.050 TYP
.248
.252
NOTES:
1. The U.S. government preferred system of measurement is the metric SI. This item was designed using inch-pound
units of measurement. In case of problems involving conflicts between the metric and inch-pound units, the
inch-pound units shall rule.
2. Pin 1 is indicated by the ESD triangle marked on top of the package.
FIGURE 1. Case outline.
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Device types 01, 02, and 03
Terminal
number
1
Terminal symbol
Terminal
number
DATA LOAD
19
Terminal symbol
AGND
Terminal
number
37
Terminal symbol
BIT 9
2
VLI/O
20
N/C
38
BIT 10
3
AGND
21
-SIN
39
BIT 11
4
VCC or +5 VA
22
+SIN
40
BIT 12
5
VCOIN
23
AGND
41
BIT 13
6
INTIN2
24
-COS
42
BIT 14
7
N/C
25
+COS
43
BIT 15
8
INTIN1
26
DGND
44
BIT 16 (LSB)
9
INT1
27
VDD or +5 VD
45
ENABLE
10
INT2
28
BIT 1 (MSB)
46
N/C
11
+REF
29
BIT 2
47
INH
12
-REF
30
BIT 3
48
SC2
13
AC2
31
BIT 4
49
SC1
14
AC1
32
BIT 5
50
BUSY
15
BPF2
33
N/C
51
CW/CCW
16
BPF1
34
BIT 6
52
RIPPLE
17
DEMOD1
35
BIT 7
18
DEMOD2
36
BIT 8
FIGURE 2. Terminal connections.
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FIGURE 3. Block diagram.
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FIGURE 4. Functional block diagram.
FIGURE 5. Transfer function diagram.
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FIGURE 6. Timing diagram(s).
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TABLE II. Electrical test requirements.
MIL-PRF-38534 test requirements
Subgroups
(in accordance with
MIL-PRF-38534, group A
test table)
Interim electrical parameters
1
Final electrical parameters
1*, 2, 3, 9, 10, 11
Group A test requirements
1, 2, 3, 9, 10, 11
Group C end-point electrical
parameters
1, 2, 3, 9, 10, 11
End-point electrical parameters
for Radiation Hardness Assurance
(RHA) devices
1
* PDA applies to subgroup 1.
4. VERIFICATION
4.1 Sampling and inspection. Sampling and inspection procedures shall be in accordance with MIL-PRF-38534 or as
modified in the device manufacturer's Quality Management (QM) plan. The modification in the QM plan shall not affect the form,
fit, or function as described herein.
4.2 Screening. Screening shall be in accordance with MIL-PRF-38534. The following additional criteria shall apply:
a.
b.
Burn-in test, method 1015 of MIL-STD-883.
(1)
Test condition A, B, C, or D. The test circuit shall be maintained by the manufacturer under document revision level
control and shall be made available to either DLA Land and Maritime -VA or the acquiring activity upon request.
Also, the test circuit shall specify the inputs, outputs, biases, and power dissipation, as applicable, in accordance
with the intent specified in method 1015 of MIL-STD-883.
(2)
TA as specified in accordance with table I of method 1015 of MIL-STD-883.
Interim and final electrical test parameters shall be as specified in table II herein, except interim electrical parameter
tests prior to burn-in are optional at the discretion of the manufacturer.
4.3 Conformance and periodic inspections. Conformance inspection (CI) and periodic inspection (PI) shall be in accordance
with MIL-PRF-38534 and as specified herein.
4.3.1 Group A inspection (CI). Group A inspection shall be in accordance with MIL-PRF-38534 and as follows:
a.
Tests shall be as specified in table II herein.
b.
Subgroups 4, 5, 6, 7, 8A, and 8B shall be omitted.
4.3.2 Group B inspection (PI). Group B inspection shall be in accordance with MIL-PRF-38534.
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4.3.3 Group C inspection (PI). Group C inspection shall be in accordance with MIL-PRF-38534 and as follows:
a.
End-point electrical parameters shall be as specified in table II herein.
b.
Steady-state life test, method 1005 of MIL-STD-883.
(1)
Test condition A, B, C, or D. The test circuit shall be maintained by the manufacturer under document revision level
control and shall be made available to either DLA Land and Maritime -VA or the acquiring activity upon request.
Also, the test circuit shall specify the inputs, outputs, biases, and power dissipation, as applicable, in accordance
with the intent specified in method 1005 of MIL-STD-883.
(2)
TA as specified in accordance with table I of method 1005 of MIL-STD-883.
(3)
Test duration: 1,000 hours, except as permitted by method 1005 of MIL-STD-883.
4.3.4 Group D inspection (PI). Group D inspection shall be in accordance with MIL-PRF-38534.
4.3.5. Radiation hardness assurance (RHA). RHA qualification is required only for those devices with the RHA designator as
specified herein. See table IIIA and table IIIB.
Table IIIA. Radiation Hardness Assurance Method Table.
RHA
method
employed
Testing at 1.5X
rated total dose
Element
Level
Hybrid
Device
Level
Yes
Yes
(See
4.3.5.1.1)
Worst Case Analysis Performed
No
Includes
Combines
temperature temperature and
effects
radiation effects
N/A
N/A
Combines End-of-life
total dose
and
displacement
effects
N/A
N/A
End points after dose is
achieved includes minimum
maximum, and room
temperatures
Element
Hybrid device level
Level
No
No
Table IIIB. Hybrid level and element level test table.
Low Dose
Rate
CMOS IC
NOTES:
X =
G =
(N) =
N/A =
G
Total Dose
High Dose Rate
(HDR)
X
(1.5 Mrad)
(See
4.3.5.1.1)
ELDRS
G
Radiation Test
Heavy Ion
SEU
SEL
(upset)
(latch-up)
+125°C
(N)
X
(100 MeV2
cm /mg)
Proton
Low
High
Energy Energy
(N)
(N)
SEE
(upset)
Neutron
Displacement
Damage (DD)
(N)
(N)
Radiation testing done (Level)
Guaranteed by design or process
Not yet tested
Not applicable for this SMD
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4.3.5.1 Radiation Hardness Assurance (RHA) inspection. RHA qualification is required for those devices with the RHA
designator as specified herein. End-point electrical parameters for radiation hardness assurance (RHA) devices shall be
specified in table II. Radiation testing will be in accordance with the qualifying activity (DLA Land and Maritime -VQ) approved
plan and with MIL-PRF-38534, Appendix G.
a.
The hybrid device manufacturer shall establish procedures controlling component radiation testing, and shall establish
radiation test plans used to implement component lot qualification during procurement. Test plans and test reports
shall be filed and controlled in accordance with the manufacturer's configuration management system.
b.
The hybrid device manufacturer shall designate a RHA program manager to oversee component lot qualification, and
to monitor design changes for continued compliance to RHA requirements.
4.3.5.1.1 Hybrid level RHA qualification. Hybrid level and element level testing are the same for the device on this (SMD)
since the active element is accessible to the device leads for test.
4.3.5.1.2 Element level qualifcation.
4.3.5.1.2.1 Total ionizing dose irradiation testing. Every wafer lot of the active element used will be tested at HDR in
accordance with condition A of method 1019 of MIL-STD-883 to 1.5 Mrad(Si). A minimum of 5 biased samples which were
determined to be worst case will be tested. 0.9000/90% statistics are applied to the device parameters as specified in table IA
herein.
4.3.5.1.2.2 Single Event Phenomena (SEP). A minimum of four samples of device type 03 is characterized for SEP response
at initial qualification and after any design or process changes which may affect the RHA response of the device. Testing shall
be performed in accordance with ASTM F 1192. Test conditions for SEP are as follows:
a.
The ion beam angle of incidence shall be normal to the die surface at 46 degrees. No shadowing of the ion beam due
to fixturing is allowed.
b.
The fluence shall be ≥ 1x10 particles/cm .
c.
The flux shall be between 10 and 10 ions/cm /s.
d.
The particle range shall be ≥ 35 micron in silicon.
e.
The characterization is performed at maximum recommended voltages, input 5KHz constantly rotating angles, 16-bit
configuration and the test temperature shall be +125°C ± 10°C in air.
7
2
2
5
2
4.3.5.2 RHA Lot Acceptance. Each wafer lot of the active element shall be evaluated for acceptance in accordance with MILPRF-38534 and herein.
4.3.5.2.1 Total ionizing dose. See paragraph 4.3.5.1.2.1 herein.
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4.3.5.2.2 Enhanced Element Evaluation. Enhanced Element Evaluation per Table IV herein including 45 devices subjected to
Group C2, 1000 hours life testing, is required only for those devices with the RHA designator as specified herein.
Table IV. Enhanced Element Evaluation For Microcircuit Die.
Subgroup
Class
K
2
X
1
3
4
Test
MIL-STD-883
Method
Condition
2010
X
X
X
Element visual
Assembled into package
as specified in 1.2.4
herein.
Element electrical
Internal visual
Temperature cycling
X
Constant acceleration
2001
X
Burn-in
1015
X
X
Interim electrical
Burn-in
1015
X
X
Post burn-in Final
Electrical, Group A
Steady-state life
1005
5
X
X
Final electrical
Wire bond evaluation 3/
2011
6
X
SEM
2018
Quantity
(accept number)
100 percent
100 percent
100 percent
100 percent
2017
1010
C
Reference
Paragraph
1/
C.3.3.2
C.3.3.1
C.5.5
C.3.3.3
100 percent
3000g’s, Y1
direction
160 hours
minimum at
+125°C
C.5.6
C.3.3.4.3
160 hours
minimum at
+125°C
C.5.10
1000 hours
minimum at
+125°C
45(0)
2/
10(0) wires or
20(1) wires
See method 2018
of MIL-STD-883
C.3.3.4.3
C.3.3.3
C.3.3.5
C.3.3.6
1/ See MIL-PRF-38534.
2/ Die shall be traceable to the wafer and wafer lot. The sample size shall consist of a minimum of 3 die from each wafer
and a minimum of 45 die from each wafer lot.
3/ This device herein is manufactured with aluminum wires and aluminum bond sites on the IC. No bimetallic bonds.
4.3.5.3 Technologies not tested. The active element in this device is RHA tested.
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5. PACKAGING
5.1 Packaging requirements. The requirements for packaging shall be in accordance with MIL-PRF-38534.
6. NOTES
6.1 Intended use. Microcircuits conforming to this drawing are intended for use for Government microcircuit applications
(original equipment), design applications, and logistics purposes.
6.2 Replaceability. Microcircuits covered by this drawing will replace the same generic device covered by a contractorprepared specification or drawing.
6.3 Configuration control of SMD's. All proposed changes to existing SMD's will be coordinated as specified in MIL-PRF38534.
6.4 Record of users. Military and industrial users shall inform DLA Land and Maritime when a system application requires
configuration control and the applicable SMD. DLA Land and Maritime will maintain a record of users and this list will be used
for coordination and distribution of changes to the drawings. Users of drawings covering microelectronic devices (FSC 5962)
should contact DLA Land and Maritime -VA, telephone (614) 692-0544.
6.5 Comments. Comments on this drawing should be directed to DLA Land and Maritime -VA, Columbus, Ohio 43218-3990,
or telephone (614) 692-1081.
6.6 Sources of supply. Sources of supply are listed in MIL-HDBK-103 and QML-38534. The vendors listed in MIL-HDBK-103
and QML-38534 have submitted a certificate of compliance (see 3.7 herein) to DLA Land and Maritime -VA and have agreed to
this drawing.
6.7 Pin functions. Microcircuits conforming to this drawing shall have the pin functions as specified in table V herein.
6.8 Additional information. When applicable, a copy of the following additional data shall be maintained and available from
the device manufacturer:
a. RHA upset levels.
b. Test conditions (SEP).
c. Occurrence of latchup (SEP).
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Table V. Pin functions.
SIGNAL
DIRECTION PIN
SIGNAL DESCRIPTION
+SIN
-SIN
INPUT
22
21
Analog Sine input from Synchro or Resolver. 1.3 V rms nominal
+COS
-COS
INPUT
25
24
Analog Cosine input from Synchro or Resolver. 1.3 V rms nominal
+REF
-REF
INPUT
11
12
Analog Reference input
BIT 1 (MSB)
BIT 2
BIT 3
BIT 4
BIT 5
BIT 6
BIT 7
BIT 8
BIT 9
BIT 10
BIT 11
BIT 12
BIT 13
BIT 14
BIT 15
BIT 16 (LSB)
BIDIR
28
29
30
31
32
34
35
36
37
38
39
40
41
42
43
44
Digital angle data. Parallel format. Natural binary positive logic.
Bit 1, most significant bit = 180°, Bit 2 = 90°, Bit 3 = 45° and so on.
SC1
SC2
INPUT
49
48
Digital input. Sets the resolution.
SC1 SC2 Resolution
0
0
10 bit
0
1
12 bit
1
0
14 bit
1
1
16 bit
ENABLE
INPUT
45
Logic 0 enables digital angle output. Otherwise it is high impedance.
INH
INPUT
47
Logic 0 freezes the digital angle output so that it can be safely read.
DATA LOAD
INPUT
1
Logic 0 enables the digital angle lines to be inputs to preset the angle. Logic 1 is for
normal digital angle output.
BUSY
OUTPUT
50
A logic 1 pulse when the digital angle changes by 1 LSB.
CW/CCW
OUTPUT
51
For turns counting. Logic 1 = counting up (CW), logic 0 = counting down (CCW).
RIPPLE
OUTPUT
52
Ripple clock for turns counting. A logic 0 pulse = a 0° transition in either direction.
In the 10 bit mode, Bit 10 is the LSB. Bits 11-16 are 0s.
In the 12 bit mode, Bit 12 is the LSB. Bits 13-16 are 0s.
In the 14 bit mode, Bit 14 is the LSB. Bits 15-16 are 0s.
In the 16 bit mode, Bit 16 is the LSB.
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Table V. Pin functions - Continued.
SIGNAL
DIRECTION
PIN
SIGNAL DESCRIPTION
AC1
AC2
OUTPUT
14
13
Differential AC error output
BPF1
BPF2
INPUT
16
15
Differential AC error input to demodulator
OUTPUT
17
18
Differential DC error output
INPUT
8
6
Differential DC input to differential velocity integrator
OUTPUT
9
10
Differential velocity output
INPUT
5
Input to Voltage Controlled Oscillator
POWER
4
27
Analog Power In
Digital Power In
A GND
D GND
POWER
3,19,23
26
VLi/o
POWER
2
DEMOD1
DEMOD2
INTIN1
INTIN2
INT1
INT 2
VCOIN
VCC or +5 VA
VDD or +5 VD
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Digital Power ground
Digital input/output DC power supply. Sets logic 1 level. +3V to
+5V
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6.9 Die anomalies. The first anomoly exists only for device types 01 and 02. The first anomaly is the instability at 360°
and 180° input angles. This problem only occurs in the 16-bit mode when rotating in the clockwise direction and has been
observed on 100 percent of the parts at 25°C. It occurs 100 percent of the time at 360° and approximately 76 percent at 180°.
At 360° the problem occurs when the counter passes from FFFF to 0000 then reverse rotation counter clockwise back to FFFF.
At 180° the problem occurs when the counter passes from 7FFF to 8000 then reverse rotation counter clockwise back to 7FFF.
Two different failure modes have been observed for this anomaly and are as follows:
1). The output latch locks to a value with the most significant bit (MSB) inverted giving indication that the part is 180° out
phase, the part exhibits zero error. This condition remains indefinitely until the resolver rotates in either direction
by one count. At which time, the part responds to the 180° error which takes less than 150 milliseconds to correct.
2). The part sees an immediate error of 180° and begins to correct this error which takes less than 150 milliseconds.
In some cases it has been observed that the MSB is fine but the next bit gets inverted which provides a 90° error. In this
case the time required for the part to correct itself is less than 75 milliseconds.
The recommended actions to avoid this problem are as follows:
1). Use the 10, 12, or 14-bit mode. For device type 02 only, the ambient operating temperature range for 10 and 12-bit
mode is -55°C to +125°C, for 14-bit mode is -40°C to +125°C.
2). Insure hysteresis of at least one bit to prevent this anomaly when rotating very slowly.
3). Avoid reversing direction at 360° and 180° when rotating in the clockwise direction.
4). If the resolver stops within two counts of 360° or 180° wait 150 milliseconds after motion resumes before reading
the parts output.
The second anomaly for device types 01, 02, and 03 is correcting the Integral Nonlinearity Error . The following information is
provided to address the constant Integral Nonlinearity (INL) that exists at each angle of the part. The error is repeatable from
part to part and table VI of offsets is included herein that must be added to the output of the part to get the correct angle. Figure
7 shows the error in minutes that exist at 2° increments for the full 360°. The INL error from 0° to 180° is basically the same
error between 180° to 360°. Table VI has the angle correction factor (in minutes) that must be added to zero out the INL error.
A simple calculation can be performed to derive a correction factor for angles that fall between the angles listed in table VI
herein.
AL
AS
CL
CS
NA
NCF
=
=
=
=
=
=
Larger Angle
Smaller Angle
Correction factor associated with Larger Angle
Correction factor associated with Smaller Angle
New Angle
New Correction Factor
Formula:
NCF = CS + ((( NA - AS) / (AL - AS)) * (CL - CS))
Example:
Require the correction factor at 15°
NCF = 23.4009 + (((15 -14) / (16 - 14)) * (24.0326 - 23.4009))
NCF = 23.4009 + (((1) / (2)) * .6137
NCF = 23.4009 + (.5 * .6137)
NCF = 23.4009 + .31585
NCF = 23.71675 minutes
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Device type 01.
FIGURE 7. Anomaly 2, Angle Error Chart.
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Device type 02.
FIGURE 7. Anomaly 2, Angle Error Chart - Continued.
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Device type 03.
FIGURE 7. Anomaly 2, Angle Error Chart - Continued.
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Table VI. Anomaly 2, Correction Factor (minutes) for device type 01.
Angle
0
Correction
Factor
Angle
Correction
Factor
Angle
Correction
Factor
Angle
Correction
Factor
0.125244141
90
0.415283203
180
0.145019531
270
0.474609375
2
1.911621094
92
1.153564453
182
1.997314453
272
1.206298828
4
4.073730469
94
1.977539062
184
3.981445312
274
1.970947266
6
5.715087891
96
2.537841797
186
5.754638672
276
2.577392578
8
6.868652344
98
2.814697266
188
6.822509766
278
2.649902344
10
8.411132812
100
3.071777344
190
8.411132813
280
3.150878906
12
9.241699219
102
2.735595703
192
9.221923828
282
2.794921875
14
10.17114258
104
2.656494141
194
10.19750977
284
2.682861328
16
11.11376953
106
2.478515625
196
11.09399414
286
2.564208984
18
11.54882812
108
1.885253906
198
11.44995117
288
1.858886719
20
11.94433594
110
1.285400391
200
11.97729492
290
1.562255859
22
11.99707031
112
0.837158203
202
12.01025391
292
0.626220703
24
11.91137695
114
-0.243896484
204
11.88500977
294
-0.171386719
26
12.26733398
116
-0.626220703
206
12.19482422
296
-0.652587891
28
11.85205078
118
-1.621582031
208
12.10913086
298
-1.496337891
30
11.77954102
120
-2.168701172
210
11.82568359
300
-2.083007812
32
11.97070312
122
-2.814697266
212
11.92456055
302
-2.649902344
34
11.64770508
124
-3.460693359
214
11.64111328
304
-3.618896484
36
11.26538086
126
-4.548339844
216
11.22583008
306
-4.403320313
38
10.90942383
128
-4.871337891
218
10.89624023
308
-4.95703125
40
10.16455078
130
-5.945800781
220
10.13818359
310
-5.879882812
42
9.683349609
132
-6.842285156
222
9.650390625
312
-6.723632813
44
9.030761719
134
-7.48828125
224
8.984619141
314
-7.461914063
46
8.002441406
136
-8.582519531
226
7.969482422
316
-8.450683594
48
7.237792969
138
-9.043945313
228
7.218017578
318
-8.918701172
50
6.545654297
140
-9.887695313
230
6.492919922
320
-9.755859375
52
5.6953125
142
-10.31616211
232
5.682128906
322
-10.29638672
54
5.174560547
144
-10.73144531
234
5.174560547
324
-10.81054687
56
4.198974609
146
-11.15332031
236
4.185791016
326
-11.29174805
58
3.487060547
148
-11.43017578
238
3.520019531
328
-11.3972168
60
2.939941406
150
-11.32470703
240
2.887207031
330
-11.44995117
62
2.241210938
152
-11.64770508
242
2.181884766
332
-11.57519531
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Table VI. Anomaly 2, Correction Factor (minutes) for device type 01 - Continued.
Angle
64
Correction
Factor
Angle
Correction
Factor
Angle
Correction
Factor
Angle
Correction
Factor
1.614990234
154
-11.70043945
244
1.588623047
334
-11.65429688
66
1.087646484
156
-11.71362305
246
1.114013672
336
-11.62792969
68
0.131835938
158
-11.5949707
248
0.171386719
338
-11.62792969
70
-0.547119141
160
-11.58837891
250
-0.573486328
340
-11.56201172
72
-1.0546875
162
-11.1862793
252
-1.074462891
342
-11.12036133
74
-1.549072266
164
-10.79077148
254
-1.502929687
344
-10.81713867
76
-1.641357422
166
-9.861328125
256
-1.628173828
346
-9.834960938
78
-1.977539063
168
-8.971435547
258
-1.984130859
348
-8.978027344
80
-1.944580078
170
-7.929931641
260
-1.957763672
350
-7.883789063
82
-1.766601563
172
-6.512695313
262
-1.713867188
352
-6.473144531
84
-1.753417969
174
-5.510742187
264
-1.694091797
354
-5.444824219
86
-1.0546875
176
-3.697998047
266
-1.034912109
356
-3.684814453
88
-0.250488281
178
-1.680908203
268
-0.283447266
358
-1.654541016
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Table VI. Anomaly 2, Correction Factor (minutes) for device type 02 - Continued.
Angle
0
Correction
Factor
Angle
Correction
Factor
Angle
Correction
Factor
Angle
Correction
Factor
0.2037804
90
0.388944
180
0.1926492
270
0.1494676
2
1.2011235
92
0.4250145
182
1.3023937
272
0.4663943
4
2.7046554
94
1.0290481
184
2.6543247
274
1.0246463
6
3.7896351
96
1.0549836
186
3.5417379
276
1.1382954
8
4.4210134
98
0.985566
188
4.4124454
278
1.1587672
10
5.2155666
100
1.3049934
190
5.203492
280
1.0999234
12
5.8344789
102
0.9052019
192
5.8037239
282
0.6942761
14
6.3655715
104
0.6187665
194
6.3895613
284
0.6348358
16
6.9555728
106
0.3392372
196
6.9176556
286
0.4454498
18
7.2150137
108
-0.175559
198
7.1084421
288
-0.177215
20
7.668033
110
-0.406551
200
7.7189463
290
-0.454718
22
8.0207217
112
-0.999534
202
8.0275228
292
-0.889493
24
7.9337942
114
-1.499164
204
7.8880027
294
-1.403421
26
8.2323065
116
-1.844624
206
8.1449399
296
-1.843685
28
8.1783179
118
-2.397679
208
8.1387855
298
-2.293495
30
8.0459945
120
-2.881544
210
8.08097
300
-3.028745
32
8.3625996
122
-3.236345
212
8.2928404
302
-3.32441
34
8.1656155
124
-3.826773
214
8.137597
304
-3.956229
36
7.8536486
126
-4.4022
216
7.8531124
306
-4.509103
38
7.8015315
128
-4.68487
218
7.7737084
308
-4.688704
40
7.3359658
130
-5.328598
220
7.2755348
310
-5.187046
42
7.2219005
132
-5.670543
222
7.2015871
312
-5.509263
44
7.0820345
134
-5.974115
224
7.0049554
314
-5.88838
46
6.4602993
136
-6.658819
226
6.3980315
316
-6.480666
48
6.093604
138
-6.661897
228
6.0267529
318
-6.814285
50
5.6270972
140
-7.094022
230
5.5584493
320
-6.980524
52
5.2254441
142
-7.603145
232
5.1655597
322
-7.525344
54
4.7990496
144
-7.436118
234
4.7743379
324
-7.475306
56
4.3314519
146
-7.735451
236
4.3005015
326
-7.830463
58
3.6928435
148
-7.941762
238
3.677129
328
-7.845085
60
3.4616901
150
-7.955999
240
3.3761744
330
-7.737209
62
2.9175922
152
-8.046982
242
2.842719
332
-7.950106
STANDARD
MICROCIRCUIT DRAWING
DLA LAND AND MARITIME
COLUMBUS, OHIO 43218-3990
DSCC FORM 2234
APR 97
SIZE
5962-04235
A
REVISION LEVEL
D
SHEET
28
Table VI. Anomaly 2, Correction Factor (minutes) for device type 02 - Continued.
Angle
Correction
Factor
64
Angle
Correction
Factor
Angle
Correction
Factor
Angle
Correction
Factor
2.3965424
154
-7.808906
244
2.3611981
334
-8.023122
66
2.2065613
156
-7.518633
246
2.219188
336
-7.690546
68
1.5534788
158
-7.694355
248
1.3174688
338
-7.719087
70
1.0493304
160
-7.452276
250
1.0260607
340
-7.438014
72
0.5976757
162
-6.973083
252
0.5846875
342
-6.895998
74
0.206093
164
-6.728264
254
0.2573653
344
-6.759761
76
0.0199815
166
-6.19136
256
0.0243755
346
-6.141721
78
-0.21906
168
-5.698378
258
-0.199283
348
-5.697088
80
-0.54652
170
-5.196078
260
-0.576188
350
-5.132956
82
-0.576408
172
-4.228528
262
-0.53484
352
-4.203093
84
-0.61473
174
-3.402853
264
-0.531974
354
-3.33512
86
-0.399631
176
-2.508138
266
-0.387925
356
-2.453571
88
0.1805842
178
-1.065913
268
0.1435904
358
-1.041203
STANDARD
MICROCIRCUIT DRAWING
DLA LAND AND MARITIME
COLUMBUS, OHIO 43218-3990
DSCC FORM 2234
APR 97
SIZE
5962-04235
A
REVISION LEVEL
D
SHEET
29
Table VI. Anomaly 2, Correction Factor (minutes) for device type 03 - Continued.
Angle
Correction
Factor
Angle
Correction
Factor
Angle
Correction
Factor
Angle
Correction
Factor
0
0.02039
90
0.55724
180
0.01869
270
0.53516
2
2.01363
92
2.25318
182
2.04761
272
2.24299
4
3.86417
94
3.86757
184
3.92363
274
3.86417
6
5.64675
96
5.34264
186
5.67903
276
5.35623
8
5.95127
98
5.37024
188
5.96316
278
5.41101
10
6.09779
100
5.31119
190
6.14026
280
5.36046
12
6.32756
102
4.96163
192
6.05064
282
4.98202
14
5.61783
104
4.28418
194
5.64161
284
4.33175
16
5.10687
106
3.54386
196
5.11196
286
3.57275
18
4.91700
108
3.06688
198
4.92380
288
3.09577
20
5.08052
110
3.00444
200
5.09411
290
3.02653
22
5.37484
112
2.93690
202
5.36805
292
2.98107
24
5.85605
114
2.82179
204
5.53326
294
2.86426
26
5.76133
116
2.78992
206
5.75114
296
2.84089
28
6.31389
118
2.75806
208
5.98940
298
2.83621
30
5.40878
120
2.01095
210
5.40029
300
2.07551
32
4.77720
122
1.09225
212
4.76871
302
1.18060
34
4.06068
124
0.22282
214
4.06237
304
0.31796
36
3.46307
126
-0.47841
216
3.47157
306
-0.38497
38
2.81110
128
-1.18305
218
2.82130
308
-1.06413
40
2.33922
130
-1.69741
220
2.34602
310
-1.58528
42
2.45856
132
-1.73267
222
2.48064
312
-1.58996
44
2.46747
134
-1.81210
224
2.47936
314
-1.67959
46
2.35406
136
-1.95779
226
2.38124
316
-1.83547
48
2.30011
138
-1.98626
228
2.30520
318
-1.86054
50
2.33280
140
-1.87711
230
2.32601
320
-1.75479
52
1.84903
142
-2.40166
232
1.83713
322
-2.29293
54
1.18856
144
-3.07912
234
1.17157
324
-2.97718
56
0.52300
146
-4.01311
236
0.49752
326
-3.61556
58
-0.33114
148
-4.43062
238
-0.34473
328
-4.32699
60
-1.21076
150
-5.13696
240
-1.22435
330
-5.04352
-1.92219
152
-5.72437
242
-1.94088
332
-5.62413
62
STANDARD
MICROCIRCUIT DRAWING
DLA LAND AND MARITIME
COLUMBUS, OHIO 43218-3990
DSCC FORM 2234
APR 97
SIZE
5962-04235
A
REVISION LEVEL
D
SHEET
30
Table VI. Anomaly 2, Correction Factor (minutes) for device type 03 - Continued.
Angle
Correction
Factor
Angle
Correction
Factor
Angle
Correction
Factor
Angle
Correction
Factor
64
-1.89799
154
-5.51329
244
-1.92687
334
-5.40795
66
-1.87039
156
-5.30390
246
-1.89418
336
-5.20707
68
-1.94813
158
-5.13530
248
-1.97361
338
-5.06734
70
-2.01057
160
-4.91062
250
-2.02926
340
-4.86136
72
-2.05603
162
-4.76070
252
-2.07132
342
-4.70974
74
-2.50413
164
-4.99474
254
-2.52961
344
-4.92339
76
-3.23255
166
-5.51759
256
-3.26992
346
-5.45983
78
-3.90830
168
-5.92152
258
-3.94058
348
-5.90113
80
-4.26466
170
-6.03663
260
-4.29014
350
-6.02644
82
-4.31011
172
-5.87312
262
-4.32540
352
-5.86972
84
-4.22645
174
-5.57369
264
-4.25703
354
-5.57199
86
-2.72929
176
-3.78432
266
-2.75308
356
-3.78602
-1.10131
178
-1.88282
268
-1.11321
358
-1.89811
88
STANDARD
MICROCIRCUIT DRAWING
DLA LAND AND MARITIME
COLUMBUS, OHIO 43218-3990
DSCC FORM 2234
APR 97
SIZE
5962-04235
A
REVISION LEVEL
D
SHEET
31
STANDARD MICROCIRCUIT DRAWING BULLETIN
DATE: 12-12-17
Approved sources of supply for SMD 5962-04235 are listed below for immediate acquisition information only and
shall be added to MIL-HDBK-103 and QML-38534 during the next revisions. MIL-HDBK-103 and QML-38534 will be
revised to include the addition or deletion of sources. The vendors listed below have agreed to this drawing and a
certificate of compliance has been submitted to and accepted by DLA Land and Maritime -VA. This information
bulletin is superseded by the next dated revisions of MIL-HDBK-103 and QML-38534. DLA Land and Maritime
maintains an online database of all current sources of supply at http://www.landandmaritime.dla.mil/Programs/Smcr/.
Standard
microcircuit drawing
PIN 1/
Vendor
CAGE
number
Vendor
similar
PIN 2/
5962-0423501KXA
5962-0423501KXC
3/
3/
ACT5028-201-2S
ACT5028-201-1S
5962-0423502KXA
5962-0423502KXC
3/
3/
ACT5028-202-2S
ACT5028-202-1S
5962-0423503KXA
5962H0423503KXA
5962-0423503KXC
5962H0423503KXC
88379
88379
88379
88379
RDC5028-301-2S
RDC5028-931-2S
RDC5028-301-1S
RDC5028-931-1S
1/ The lead finish shown for each PIN representing a hermetic
package is the most readily available from the manufacturer
listed for that part. If the desired lead finish is not listed
contact the Vendor to determine its availability.
2/ Caution. Do not use this number for item acquisition. Items
acquired to this number may not satisfy the performance
requirements of this drawing.
3/ Not available from an approved source.
Vendor CAGE
number
88379
Vendor name
and address
Aeroflex Plainview Incorporated,
(Aeroflex Microelectronic Solutions)
35 South Service Road
Plainview, NY 11803-4193
The information contained herein is disseminated for convenience only and the
Government assumes no liability whatsoever for any inaccuracies in the
information bulletin.