MOR285SZ/883 [CRANE]
1-OUTPUT 100W DC-DC REG PWR SUPPLY MODULE, MODULE-12;
| 型号： | MOR285SZ/883 |
| 厂家： | 
Crane Aerospace & Electronics. |
| 描述： | 1-OUTPUT 100W DC-DC REG PWR SUPPLY MODULE, MODULE-12 输出元件 |
| 文件： | 总24页 (文件大小：2126K) |
| 中文： | 中文翻译 | 下载： | 下载PDF数据表文档文件 |
Crane Aerospace & Electronics Power Solutions
Mor sꢆꢇglꢂ ꢀꢇꢋ dꢉꢀl dc/dc cꢃꢇvꢂꢁꢅꢂꢁꢊ
28 Voꢌt input – 120 Watt
Features
pꢀꢁꢀllꢂl ꢃꢄꢂꢁꢀꢅꢆꢃꢇ wꢆꢅh ꢈꢉꢁꢁꢂꢇꢅ ꢊhꢀꢁꢂ,
ꢉꢄ ꢅꢃ 5 ꢉꢇꢆꢅꢊ (540 wꢀꢅꢅꢊ)
oꢉꢅꢄꢉꢅ flꢂxꢆbꢆlꢆꢅy, ꢅꢁꢆm ꢃf 60% ꢅꢃ 110%
•ꢀ Operating temperature -55° to +125°C
•ꢀ Input voltage 16 to 40 VDC
•ꢀ Transient protection 50 V for 120 ms
•ꢀ Fully isolated, magnetic feedback
•ꢀ Fixed high frequency switching
•ꢀ Remote sense on single output models
•ꢀ Inhibit function
MODELS
VDC OUTPUT
•ꢀ Sync In and Sync Out
S i n g l e S
d u a l S
±3.3
±5
•ꢀ Indefinite short circuit protection
•ꢀ High power density with up to 87% efficiency
3.3
5
6.3
9.5
12
15
±6.3
±9.5
±12
±15
description
With up to 120 watts of output power, the MOR Series™ of DC/
DC converters operates from a standard 28 volt bus and offers
a wide input range of 16 to 40 VDC. Full operation over the
military temperature range, -55°C to +125°C, makes the MOR
Series an ideal choice for military, aerospace, space, and other
high reliability applications. In compliance with MIL-STD-704D,
the converters will withstand transients of up to 50 volts for up
to 120 milliseconds. Use Interpoint’s FMCE-1528 EMI filter to
meet the requirements of MIL-STD-461C CE03 and CS01 and/or
MIL-STD-461D, E and F CE102 and CS101 levels of conducted
emissions.
Sh o r t Ci r C u i t Pr o t e C t i o n
The converters also provide short circuit protection by restricting
the current to 125% of the full load output current, typical.
in h i b i t Fu n C t i o n
All models offer two inhibits, one referenced to input common
and one referenced sense return (single output models) or to
output common (dual output models). A remote sense function is
available on single output models.
tr i m Fu n C t i o n
Using the trim function, the MOR Series can provide any output
from 2 to 33 VDC. For example, trimming the two 15 volt outputs
of the 15 dual (MOR2815D) to 14 volts, and then stacking the
outputs will provide a 28 volt output.
The converters are offered with standard screening, “ES”
screening, or fully compliant to “883” MIL-PRF-38534 Class H
screening. Standard microcircuit drawings (SMD) are available.
The MOR Series converters incorporate a single-ended forward
topology which uses a constant frequency Pulse Width Modulator
(PWM) current mode control design and switches at 550 kHz,
nominal.
ou t P u t Vo l t a g e oP t i o n S
The MOR Series converters are capable of providing other
output voltage options in addition to those characterized on this
datasheet. Contact your sales representative to discuss other
output voltage options, www.interpoint.com/contacts.
uS Pa t e n t S
Interpoint converters may use one or more of the following US
patents 5,521,807, 5,694,303, and 5,631,822.
Crane Aerospace & Electronics
Page 1 of 24
MOR Rev K - 20100422
Electronics Group (Interpoint Brand)
POꢀBoxꢀ97005ꢀꢀ•ꢀꢀRedmondꢀWAꢀ98073-9705
425.882.3100ꢀꢀꢀ•ꢀꢀꢀpower@crane-eg.com
www.interpoint.com
Crane Aerospace & Electronics Power Solutions
Mor sꢆꢇglꢂ ꢀꢇꢋ dꢉꢀl dc/dc cꢃꢇvꢂꢁꢅꢂꢁꢊ
28 Voꢌt input – 120 Watt
HoW to use tHe Functions
tr i m
Both single and dual output models include a trim function.
Output voltage can be trimmed from 60% up to 110% of nominal
V out . When trimming up, do not exceed the maximum output
power. When trimming down, do not exceed the maximum
output current. See Figure 2.
in P u t Vo l t a g e
Steady state voltage range is 16 to 40 VDC. Transient range
is 40 to 50 V for a maximum of 120 msec. All models include
a soft-start function to prevent large current draw and minimize
overshoot.
Trim
3
RT
TRIM UP
emi in P u t Fi l t e r S
7
Positive Output
Positive Sense
Internal 500 volt capacitors are connected between the case and
10
MOR
Single
Output
input common and between the case and output common.
9
8
Sense Return
Use Interpoint’s FMCE-1528 EMI filter to meet the requirements
of MIL-STD-461C CE03 and CS01 and/or MIL-STD-461D, E and
F CE102 and CS101 levels of conducted emissions. When using
an external input filter it is important that the case of the filter
and the case of the converter be connected through as low as
an impedance as possible. Direct connection of the baseplates
to chassis ground is the best connection. If connected by a
single trace, the trace should be as wide as it is long. See Figure
1.
Output Common
TRIM
DOWN
Fi g u r e 2: tr i m – Si n g l e
On dual models the positive output is regulated and the negative
output is transformer coupled (cross-regulated) to the positive
output. When trimming the duals, both output voltages will be
adjusted equally. See Figure 3.
1, 2, 3
10, 11, 12
1
Positive Input
Positive Input
Positive Output
MOR
Single or Dual
Output
Trim
RT
10
FMCE-1528
EMI Filter
28V
TRIM UP
7
8
Positive Output
MOR
Dual
Output
4, 5, 6
Input Common
7, 8, 9
Case
2
Input Common
Output Common
Output Common
TRIM DOWN
9
Negative Output
Chassis Ground
Fi g u r e 3: tr i m – du a l
Fi g u r e 1: ex t e r n a l Fi l t e r Co n n e C t i o n
trim FormulaS
Trim Up:
Vo
a
=
, 1.0 ≤ a ≤ 1.1
Vo nominal
Vo
2.5
(
– 1 • 20
)
RT (kΩ) =
– 50
(a -1)
Example:
Vo nominal = 5.0, Vo = 5.25, a = 1.05, RT = 390 kΩ
Trim Down:
Vo
Vo nominal
a
=
, 0.6 ≤ a ≤ 1.0
50 • a – 30
RT (kΩ) =
1 – a
Example: Vo nominal = 5.0,Vo = 4.5, a = 0.9, RT = 150 kΩ
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Page 2 of 24
MOR Rev K - 20100422
Crane Aerospace & Electronics Power Solutions
Mor sꢆꢇglꢂ ꢀꢇꢋ dꢉꢀl dc/dc cꢃꢇvꢂꢁꢅꢂꢁꢊ
28 Voꢌt input – 120 Watt
in h i b i t 1 a n d 2
un d e r V o l t a g e lo C k o u t
Two inhibit terminals disable switching, resulting in no output
and very low quiescent input current. The two inhibit pins allow
access to an inhibit function on either side of the isolation barrier
to help maintain isolation.
Undervoltage lockout prevents the units from operating below
approximately 15.5 VDC input voltage to keep system current
levels smooth, especially during initialization or re-start opera-
tions.
An open collector is required for interfacing with both of the
inhibit pins. Applying an active low to either inhibit pin will inhibit
the converter. Leaving the pins open will enable the converter.
Inhibit 1 is referenced to Input Common. Inhibit 2 is refer-
enced to Sense Return for single output models and to Output
Common for dual output models.
Sy n C in a n d Sy n C ou t
The MOR converters can be synchronized to the system clock
by applying an active high sync signal to the Sync In pin. Sync
Out can be used to synchronize other components to the MOR
converter’s switching frequency.
VCC
The open circuit voltage (unit enabled) for Inhibit 1 is 13 V
and for Inhibit 2 it is up to 8 V. Leave the Inhibit pins uncon-
nected if not used. The required active low voltage level is 0.8
V maximum for Inhibit 1 and 0.2 V maximum for Inhibit 2. See
Figures 4 and 5.
~
~
10 k
5V
~
~
330 pF
10 k
1 k
Sync In
1.8 k
Input
Common
Fi g u r e 6: Sy n C in
Positive
Input
200
The frequency range for external synchronization is 525 to 625
kHz. The requirements for an external signal are 15% to 50%
dutyꢀcycle,ꢀ0ꢀ≤ꢀLꢀ≤ꢀ0.8ꢀVꢀandꢀ4.5ꢀ≤ꢀHꢀ≤ꢀ9ꢀV.ꢀBothꢀSyncꢀInꢀandꢀ
Sync Out are referenced to input common. Sync In should be
connected to input common if not used. See Figures 6 and 7.
20 k
10 k
Inhibit 1
VCC
12V
VCC
~
~
Input
Common
MOR Input Side
200 Ω
Sync Out
Fi g u r e 4: in h i b i t 1
Input
Common
Fi g u r e 7: Sy n C ou t
VS
~
~
Voltage
E/A
Current
Limit
Po S i t iV e ou t P u t , ne g a t iV e ou t P u t a n d
ou t P u t Co m m o n
Output current is typically limited to 125% of maximum specified
10 k
200
current under short circuit or load fault conditions.
Feedback
Inhibit 2
Single output models operate from no load to full load. Dual
output models with balanced loads operate from no load to full
load. For dual models with unbalanced loads, at least 10% of
the total output power must be drawn from the positive output
at all times, however, the negative output does not require a
minimum load. See note 4, cross regulation, under the Electrical
Characteristics Tables.
Sense
Return
MOR Output Side - Single Output
Fi g u r e 5: in h i b i t 2
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Page 3 of 24
MOR Rev K - 20100422
Crane Aerospace & Electronics Power Solutions
Mor sꢆꢇglꢂ ꢀꢇꢋ dꢉꢀl dc/dc cꢃꢇvꢂꢁꢅꢂꢁꢊ
28 Voꢌt input – 120 Watt
Pa r a l l e l i n g (Sh a r e Pin)
Po S i t iV e Se n S e , Se n S e re t u r n
By using the Share pin, up to five single or dual converters
may be paralleled for a total output power of up to 540 watts,
depending on model. To calculate available power, multiply the
A special remote sensing feature maintains the desired output
voltage at the load. See Figure 9. When this feature is not used,
connect the sense lines to their respective output terminals. See
number of converters (up to five) by their maximum output power. Figure 10. Remote sensing is available on single output models
Multiply the result by 90% for total available power. See Figure
8 for the internal circuit. The converters will share within 10% of
each other at 25% to 90% rated power. MOR converters feature
true n+1 redundancy for reliability in critical applications. See
Figure 9 for the proper connections.
only. Do not exceed 110% of Vout and do not exceed maximum
output power.
7
1
6
Positive Output
Positive Sense
Positive Input
Sync In
+
10
MOR
Single
Output
28V
Load
12
9
4
2
Inhibit 2
Inhbit 1
All Positive Outputs and Positive Senses should be connected to
a common point. All Negative Outputs and Sense Returns should
be connected to a common point. The Share pin is referenced to
Sense Return. Leave the share pin floating (unconnected) if not
used. Also see Figure 9.
Sense Return
8
Input Common
–
+
Output Common
7
1
6
Positive Output
Inhibit 2
Positive Input
12
Load
Load
MOR
Dual
Sync In
Inhbit 1
28V
8
Output Common
0
4
2
Output
Input Common
9
–
Negative Output
Fi g u r e 10: ty P i C a l Co n n e C t i o n S
Share
in C r e a S e ou t P u t Vo l t a g e b y St a C k i n g ou t P u t S
Outputs may be stacked to increase the output voltage using a
dual model.
260 k
10 k
Sense
Return
Fi g u r e 8: Sh a r e
Dual outputs may be stacked to double the output voltage. See
Figure 11.
7
1
Positive Output
Inhibit 2
Positive Input
7
1
6
5
2
Positive Output
Positive Input
10
Positive Sense
+
–
MOR
Dual Output
Sync In
28V
Output Common
8
9
Load
11
9
Share
Sync Out
Sense Return
8
Output common
Input Common
Input Common
2
Negative Output
7
1
6
Positive Output
Positive Sense
Positive Input
Sync In
10
Fi g u r e 11: St a C k e d ou t P u t S – du a l mo d e l
+
11
9
5
2
Share
Sense Return
Output common
Sync Out
Load
–
8
Input Common
7
1
6
Positive Output
Positive Sense
Positive Input
Sync In
10
11
9
Share
5
2
Sync Out
Sense Return
8
Input Common Output common
Fi g u r e 9: Pa r a l l e l i n g
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Page 4 of 24
MOR Rev K - 20100422
Crane Aerospace & Electronics Power Solutions
Mor sꢆꢇglꢂ ꢀꢇꢋ dꢉꢀl dc/dc cꢃꢇvꢂꢁꢅꢂꢁꢊ
28 Voꢌt input – 120 Watt
Block Diagram
0.5 µH
1.7 µH
Positive
Output
Positive
Input
100 Ω
100 Ω
Positive
Sense
6 µF
6 µF
Sense
Return
0.1 Ω
Input
Output
Common
Common
0.015 µF
500 V
0.015 µF
500 V
Share
Function
Share
Trim
Bias
FET
Driver
Inhibit 1
V
Secondary V
S+
CC
Supply
+
_
+
_
UVLO
V
In
PWM
Controller
V
Ref
Secondary V
CC
Sync In
Sync
In / Out
Inhibit 2
Sync Out
Fi g u r e 12: mor Si n g l e ou t P u t bl o C k di a g r a m
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Page 5 of 24
MOR Rev K - 20100422
Crane Aerospace & Electronics Power Solutions
Mor sꢆꢇglꢂ ꢀꢇꢋ dꢉꢀl dc/dc cꢃꢇvꢂꢁꢅꢂꢁꢊ
28 Voꢌt input – 120 Watt
operating conDitions anD characteristics
sync anD inhiBit
iꢇꢄꢉꢅ Vꢃlꢅꢀgꢂ rꢀꢇgꢂ
syꢇꢈ
•ꢀ 16 to 40 VDC continuous
•ꢀ 50 V for 120 ms transient
•ꢀSync In
‣Input frequency 525 to 625 kHz
‣Active low 0.8 V max, duty cycle 15% to 50%
‣Active high 4.5 V min, 9 V max
‣Referenced to input common
•ꢀSync Out - Referenced to input common
oꢉꢅꢄꢉꢅ pꢃwꢂꢁ
•ꢀ 66 to 120 W, depending on model
ꢌꢂꢀꢋ sꢃlꢋꢂꢁꢆꢇg tꢂmꢄꢂꢁꢀꢅꢉꢁꢂ (10 ꢊꢂꢈ ꢄꢂꢁ lꢂꢀꢋ)
•ꢀ 300°C
iꢇhꢆbꢆꢅ (inH1, inH2)
•ꢀ Active low (output disabled)
‣Inhibit 1 (INH1)
sꢅꢃꢁꢀgꢂ tꢂmꢄꢂꢁꢀꢅꢉꢁꢂ rꢀꢇgꢂ (tc)
•ꢀ -65°C to +150°C
- Referenced to input common
- 0.8 V max.
- Inhibit pin current 1 mA max
‣Inhibit 2 (INH2)
- Single output models are referenced to Sense Return
- Dual output models are referenced to Output Common
- 0.2 V max
cꢀꢊꢂ oꢄꢂꢁꢀꢅꢆꢇg tꢂmꢄꢂꢁꢀꢅꢉꢁꢂ (tc)
•ꢀ -55°C to +125°C full power
•ꢀ -55°C to +135°C absolute
dꢂꢁꢀꢅꢆꢇg oꢉꢅꢄꢉꢅ pꢃwꢂꢁ/cꢉꢁꢁꢂꢇꢅ
•ꢀ Linearly from 100% at 125°C to 0% at 135° C
oꢉꢅꢄꢉꢅ Vꢃlꢅꢀgꢂ tꢂmꢄꢂꢁꢀꢅꢉꢁꢂ cꢃꢂffꢆꢈꢆꢂꢇꢅ
•ꢀ 100 ppm/°C typ
- Inhibit pin current 1 mA max
•ꢀ Active high (output enabled) open collector
‣Open pin voltage:
iꢇꢄꢉꢅ ꢅꢃ oꢉꢅꢄꢉꢅ cꢀꢄꢀꢈꢆꢅꢀꢇꢈꢂ
•ꢀ 150 pF typical
- Inhibit 1 (INH1) = 13 V typ.
- Inhibit 2 (INH2) = up to 8 V
cꢉꢁꢁꢂꢇꢅ ꢌꢆmꢆꢅ
•ꢀ 125% of full load typ
iꢊꢃlꢀꢅꢆꢃꢇ
•ꢀ 100 megohm min at 500 V
aꢉꢋꢆꢃ rꢂjꢂꢈꢅꢆꢃꢇ
•ꢀ 40 dB typ
cꢃꢇvꢂꢁꢊꢆꢃꢇ Fꢁꢂqꢉꢂꢇꢈy
•ꢀ Free run mode, 25°C, 550 kHz typ
‣ 480 kHz. min, 580 kHz max
uꢇꢋꢂꢁvꢃlꢅꢀgꢂ ꢌꢃꢈkꢃꢉꢅ
•ꢀ 15.5 V input typ
mechanical anD environmental
sꢈꢁꢂꢂꢇꢆꢇg
sꢆzꢂ (mꢀxꢆmꢉm)
•ꢀ Standard, ES, or 883 (Class H, QML) available. See
Screening Tables 1 and 2 for more information.
•ꢀ 3.005 x 1.505 x 0.400 inches (76.33 x 38.23 x 10.16 mm)
•ꢀ Available in a variety of packages. See cases U2, V, W, Y,
and Z for dimensions.
Wꢂꢆghꢅ (mꢀxꢆmꢉm)
•ꢀ 110 grams
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Page 6 of 24
MOR Rev K - 20100422
Crane Aerospace & Electronics Power Solutions
Mor sꢆꢇglꢂ ꢀꢇꢋ dꢉꢀl dc/dc cꢃꢇvꢂꢁꢅꢂꢁꢊ
28 Voꢌt input – 120 Watt
pins not in use
pin out
Case
User’s discretion
pꢆꢇ
1
sꢆꢇglꢂ oꢉꢅꢄꢉꢅ
dꢉꢀl oꢉꢅꢄꢉꢅ
Inhibit (INH1, INH2)
Sense Line
Leave unconnected
Positive Input
Input Common
Trim
Positive Input
Input Common
Case
Must be connected to the
appropriate outputs
2
3
Sync In
Sync Out
Share
Connect to input common
Leave unconnected
Leave unconnected
Leave unconnected
4
Inhibit 1 (INH1)
Sync Out
Inhibit 1 (INH1)
Sync Out
5
6
Sync In
Sync In
Trim
7
Positive Output
Positive Output
8
Output Common Output Common
9
Sense Return
Positive Sense
Share
Negative Output
Trim
10
11
12
Share
Inhibit 2 (INH2)
Inhibit 2 (INH2)
Angled corner and cover marking indicate pin one for cases
U2 and V. Cover marking indicates pin one for cases W, Y, and Z.
TOP VIEW
MOR
(Pin side, marked side)
1
2
3
4
5
6
12
11
10
9
Outline shown is case U2 pin out is the same
for all cases. Available in a variety of packages
See cases U2, V, W, Y and Z for dimensions.
8
7
Fi g u r e 13: Pin ou t to P Vi e w
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Page 7 of 24
MOR Rev K - 20100422
Crane Aerospace & Electronics Power Solutions
Mor sꢆꢇglꢂ ꢀꢇꢋ dꢉꢀl dc/dc cꢃꢇvꢂꢁꢅꢂꢁꢊ
28 Voꢌt input – 120 Watt
Modeꢌ nuMꢍerinꢎ ꢏeꢐ
sMd nuMꢍers
St a n d a r d Mi c r o c i r c u i t
Mor SiMilar Pa r t
MOR 28 05
S
Y / 883
dr a w i n g (SMd)
5962-9954401HXC
5962-9954801HXC
5962-9954501HXC
5962-9954601HXC
5962-9954901HXC
5962-9955001HXC
5962-9956401HXC
5962-9956101HXC
5962-9956501HXC
5962-9956601HXC
5962-9956201HXC
5962-9956301HXC
Base Model
Input Voltage
Output Voltage
MOR283R3S/883
MOR2805S/883
MOR286R3S/883
MOR289R5S/883
MOR2812S/883
MOR2815S/883
MOR283R3D/883
MOR2805D/883
MOR286R3D/883
MOR289R5D/883
MOR2812D/883
MOR2815D/883
(R = decimal point, 3R3 = 3.3 Vout)
Number of Outputs
(S = single, D = dual)
Case/Lead Option
(Standard case – U2 – has no designator
in this position)
Screening
(Standard screening has no designator in this position.
cꢀꢊꢂꢊ: sMd ꢀꢇꢋ sꢆmꢆlꢀꢁ pꢀꢁꢅ nꢉmbꢂꢁ
St a n d a r d Mi c r o c i r c u i t
dr a w i n g (SMd)
Mor SiMilar Pa r t
The models listed have the standard U2 case option. In
the DSCC number “X” is the equivalent of the standard
U2 case.
X
U
T
Y
Z
STANDARD CASE (U2)
V
W
Y
For exact specifications for an SMD product, refer to
the SMD drawing. SMDs can be downloaded from:
http://www.dscc.dla.mil/programs/smcr
Z
Modeꢌ seꢌection
on t h e l i n e S b e l o w , e n t e r o n e S e l e c t i o n f r o M e a c h c a t e g o r y to d e t e r M i n e t h e M o d e l n u M b e r .
___________
Mor28
/
cateꢎorꢐ
seꢌection
1
2
4
Base Model and
Input Voltage
Output Voltage
Number of Outputs
Case/Lead
Screening
3
Options
3r3
05
s
d
(U2 leave blank)
(STANDARD leave blank)
V
W
ꢐ
es
MOR28 is the only
available option
6r3
9r5
12
883
ꢑ
15
Notes:
1. Output Voltage: An R indicates a decimal point. 3R3 is 3.3 volts out.
2. Number of Outputs: S is a single output and D is a dual output
3. Case Options: For the standard case (case U2) leave the case option blank. For other case options, insert the letter that corresponds to the desired case.
4. Screening: For standard screening leave the screening option blank. For other screening options, insert the desired screening level. For more information see Screening
Tables 1 and 2.
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Page 8 of 24
MOR Rev K - 20100422
Crane Aerospace & Electronics Power Solutions
Mor sꢆꢇglꢂ ꢀꢇꢋ dꢉꢀl dc/dc cꢃꢇvꢂꢁꢅꢂꢁꢊ
28 Voꢌt input – 120 Watt
Electrical Characteristics: -55 to +125°C T , 28 VDC Vin, 100% load, free run, unless otherwise specified.
C
SINGLE OUTPUT MODELS
Parameter
MOR283R3S
MOR2805S
MOR286R3S
ConditionS
MIN
TYP
3.30
—
MAX
MIN
4.87
0
TYP
5.00
—
MAX
5.25
20
MIN
TYP
6.30
—
MAX
unitS
VDC
A
outPut Voltage
outPut Current
outPut Power
3.22
0
3.38
20
66
80
50
20
30
40
50
150
10
70
90
—
6.17
0
6.43
16
Vin = 16 to 40 VdC
Vin = 16 to 40 VdC
10 khz - 20 mhz
10 khz - 2 mhz
0
—
0
—
100
80
0
—
100
100
60
W
outPut riPPle
—
—
—
—
16
—
—
—
—
—
74
30
20
0
—
—
—
—
16
—
—
—
—
—
77
30
20
0
—
—
—
—
16
—
—
—
—
—
80
75
50
0
mV p-p
50
line regulation
load regulation
inPut Voltage
V
= 16 to 40 VdC
20
20
mV
mV
VDC
V
in
no load to Full
ContinuouS
0
0
30
0
30
28
—
28
—
40
28
—
40
1
TRANSIENT 120 msec.
50
50
inPut Current
no load
70
—
70
—
150
10
70
—
150
10
inhibited–inh1
inhibited–inh2
10 khz - 20 mhz
mA
—
—
70
—
70
inPut riPPle Current
eFFiCienCy
40
78
50
81
130
—
50
83
130
—
mA p-p
%
load Fault
Power diSSiPation
1
oVerload
—
—
—
27
—
—
—
22
10
—
—
—
30
—
—
—
27
10
—
—
—
30
—
—
—
24
10
W
2
Short CirCuit
1
reCoVery
ms
SteP load reSPonSe
SteP line reSPonSe
50% - 100% - 50%
tranSient
—
—
—
—
250
200
—
—
—
—
250
200
—
—
—
—
500
300
mV pk
µs
3
reCoVery
16 - 40 - 16 VdC
1, 4
tranSient
—
—
—
—
—
—
—
0
400
300
10
—
—
—
—
—
—
—
0
400
300
10
—
—
—
—
—
—
—
0
500
300
10
mV pk
µs
1, 3
reCoVery
5
Start-uP
delay
ms
1
oVerShoot
25
50
50
mV pk
1
CaPaCitiVe load
no eFFeCt on dC
PerFormanCe
—
—
1000
—
—
1000
—
—
1000
µF
Notes:
1. ꢎꢉꢀꢁꢀꢇꢅꢂꢂꢋ by ꢋꢂꢊꢆgꢇ, ꢇꢃꢅ ꢅꢂꢊꢅꢂꢋ.
2. Short circuit is measured with a 10 m ohm (±10%) resistive load.
3. Time to settle to within 1% of Vout.
4. Transition time > 10 µs
5. Tested on release from inhibit.
www.interpoint.com
Page 9 of 24
MOR Rev K - 20100422
Crane Aerospace & Electronics Power Solutions
Mor sꢆꢇglꢂ ꢀꢇꢋ dꢉꢀl dc/dc cꢃꢇvꢂꢁꢅꢂꢁꢊ
28 Voꢌt input – 120 Watt
Electrical Characteristics: -55 to +125°C T , 28 VDC Vin, 100% load, free run, unless otherwise specified.
C
SINGLE OUTPUT MODELS
Parameter
MOR289R5S
MOR2812S
TYP
MOR2815S
TYP
ConditionS
MIN
TYP
9.50
—
MAX
MIN
MAX
12.24
9.2
110
120
100
20
MIN
MAX
15.30
8
unitS
VDC
A
outPut Voltage
outPut Current
outPut Power
9.31
0
9.69
11
11.76
0
12.00
—
—
75
50
0
14.70
0
15.00
—
—
75
50
0
Vin = 16 to 40 VdC
Vin = 16 to 40 VdC
10 khz - 20 mhz
10 khz - 2 mhz
0
—
105
120
80
—
—
—
—
—
16
—
—
—
—
—
83
—
—
—
—
—
16
—
—
—
—
—
83
120
150
120
40
W
outPut riPPle
—
—
—
—
16
—
—
—
—
—
80
75
50
0
mV p-p
line regulation
load regulation
inPut Voltage
V
= 16 to 40 VdC
40
mV
mV
VDC
V
in
no load to Full
ContinuouS
0
95
0
100
40
0
100
40
28
—
40
28
—
70
—
—
50
86
28
—
70
—
—
50
87
1
TRANSIENT 120 ms
50
50
50
inPut Current
no load
70
—
150
10
150
10
150
10
inhibited–inh1
inhibited–inh2
10 khz - 20 mhz
mA
—
70
70
70
inPut riPPle Current
eFFiCienCy
50
84
130
—
130
—
130
—
mA p-p
%
load Fault
Power diSSiPation
1
oVerload
—
—
—
—
—
—
30
24
10
—
—
—
—
—
—
30
22
10
—
—
—
—
—
—
30
20
10
W
2
Short CirCuit
1
reCoVery
ms
SteP load reSPonSe
SteP line reSPonSe
50% - 100% - 50%
tranSient
—
—
—
—
500
300
—
—
—
—
600
300
—
—
—
—
600
300
mV pk
µs
3
reCoVery
16 - 40 - 16 VdC
1, 4
tranSient
—
—
—
—
—
—
—
—
500
300
10
—
—
—
—
—
—
—
—
600
300
10
—
—
—
—
—
—
—
—
600
300
10
mV pk
µs
1, 3
reCoVery
5
Start-uP
delay
ms
1
oVerShoot
50
50
50
mV pk
1
CaPaCitiVe load
no eFFeCt on dC
PerFormanCe
—
—
1000
—
—
1000
—
—
1000
µF
Notes:
1. ꢎꢉꢀꢁꢀꢇꢅꢂꢂꢋ by ꢋꢂꢊꢆgꢇ, ꢇꢃꢅ ꢅꢂꢊꢅꢂꢋ.
2. Short circuit is measured with a 10 m ohm (±10%) resistive load.
3. Time to settle to within 1% of Vout.
4. Transition time > 10 µs
5. Tested on release from inhibit.
www.interpoint.com
Page 10 of 24
MOR Rev K - 20100422
Crane Aerospace & Electronics Power Solutions
Mor sꢆꢇglꢂ ꢀꢇꢋ dꢉꢀl dc/dc cꢃꢇvꢂꢁꢅꢂꢁꢊ
28 Voꢌt input – 120 Watt
Electrical Characteristics: -55°C to +125°C T , 28 VDC Vin, 100% load, free run, unless otherwise specified.
C
MOR283R3D
MOR2805D
TYP
5.00
5.00
±10
—
MOR286R3D
DUAL OUTPUT MODELS
unitS
Parameter
ConditionS
MIN
3.20
3.16
—
TYP
3.30
3.30
±10
—
MAX
3.40
3.44
MIN
4.85
4.82
—
MAX
5.15
5.18
MIN
6.17
6.12
—
TYP
MAX
6.43
6.48
2
outPut Voltage
+V
6.30
out
VDC
-V
6.30
out
3
1
1
1
outPut Current
eaCh outPut
total
14
14
±8
—
±50
—
50
30
25
50
25
50
5
11.2
16
A
W
Vin = 16 to 40 VdC
—
20
—
20
—
3
1
1
1
outPut Power
eaCh outPut
total
—
±33
—
46
—
±50
—
70
—
70
Vin = 16 to 40 VdC
—
66
80
—
100
80
—
100
100
60
outPut riPPle
10 khz - 20 mhz
10 khz - 2 mhz
—
50
—
50
—
mV p-p
mV
±V
out
—
35
50
—
35
50
—
line regulation
+V
—
25
50
—
25
50
—
50
out
V
= 16 to 40 VdC
in
-V
—
50
100
50
—
50
100
50
—
100
50
out
load regulation
+V
—
25
—
25
—
out
mV
-V
—
50
100
10
—
50
150
8
—
200
8
out
1, 4
CroSS regulation
inPut Voltage
-V
—
6
—
5
—
%
VDC
V
out
ContinuouS
TRANSIENT 120 ms
no load
16
—
28
40
16
—
28
40
16
—
28
—
70
—
—
—
83
40
1
—
50
—
50
50
inPut Current
—
70
160
10
—
70
160
10
—
160
10
inhibited–inh1
inhibited–inh2
10 mhz - 20 mhz
—
—
—
—
—
mA
—
—
70
—
—
70
—
70
inPut riPPle Current
eFFiCienCy
—
60
90
—
60
130
—
—
130
—
mA p-p
%
75
77
—
77
81
80
load Fault
Power diSSiPation
1
oVerload
—
—
—
—
—
—
27
22
10
—
—
—
—
—
—
30
27
10
—
—
—
—
—
—
30
24
10
W
5
Short CirCuit
1
reCoVery
ms
SteP load reSPonSe
50% - 100% - 50%
tranSient
±V
out
—
—
—
—
250
300
—
—
—
—
250
200
—
—
—
—
500
300
mV pk
µs
6
reCoVery
SteP line reSPonSe
16 - 40 - 16 VdC
±V
1, 7
out
tranSient
—
—
—
—
—
—
—
—
400
300
10
—
—
—
—
—
—
—
—
400
300
10
—
—
—
—
—
—
—
—
500
300
10
mV pk
µs
1, 6
reCoVery
8
Start-uP
delay
ms
1
oVerShoot
25
50
50
mV pk
1
CaPaCitiVe load
no eFFeCt on dC
PerFormanCe
—
—
1000
—
—
1000
—
—
1000
µF
Notes:
1. ꢎꢉꢀꢁꢀꢇꢅꢂꢂꢋ by ꢋꢂꢊꢆgꢇ, ꢇꢃꢅ ꢅꢂꢊꢅꢂꢋ.
2. Output voltage for dual output models is measured at half load.
3. The “Total” specification is the maximum combined current/power of both outputs.
Up to 70% of that total is available from either output provided the other output
maintains a minimum of 15% of the total power used. The 15% minimum
maintains regulation.
4. Effect on negative Vout from 50%/50% loads to 70%/30&% or 30%/70% loads.
5. Short circuit is measured with a 10 milliohm (±10%) resistive load.
6. Time to settle to within 1% of Vout.
7. Transition time > 10 µs
8. Tested on release from inhibit.
www.interpoint.com
Page 11 of 24
MOR Rev K - 20100422
Crane Aerospace & Electronics Power Solutions
Mor sꢆꢇglꢂ ꢀꢇꢋ dꢉꢀl dc/dc cꢃꢇvꢂꢁꢅꢂꢁꢊ
28 Voꢌt input – 120 Watt
Electrical Characteristics: -55°C to +125°C T , 28 VDC Vin, 100% load, free run, unless otherwise specified.
C
MOR289R5D
MOR2812D
MOR2815D
DUAL OUTPUT MODELS
unitS
Parameter
ConditionS
MIN
9.31
9.26
—
TYP
MAX
9.69
9.74
MIN
11.76
11.70
—
TYP
12.00
12.00
±4.58
—
MAX
12.24
12.30
MIN
14.70
14.62
—
TYP
15.00
15.00
±4.00
—
MAX
15.30
15.38
2
outPut Voltage
+V
9.50
out
VDC
-V
9.50
out
3
1
1
1
outPut Current
eaCh outPut
total
±5.53
—
7.75
6.4
5.6
A
W
Vin = 16 to 40 VdC
—
11.05
—
9.16
—
8
3
1
1
1
outPut Power
eaCh outPut
total
—
±52.5
—
73.5
—
±55
—
77
—
±60
—
84
Vin = 16 to 40 VdC
—
105
120
80
—
110
120
100
50
—
120
150
120
50
outPut riPPle
10 khz - 20 mhz
10 khz - 2 mhz
—
75
50
25
50
25
50
4
—
75
—
75
mV p-p
mV
±V
out
—
—
50
—
50
line regulation
+V
—
50
—
25
—
25
out
V
= 16 to 40 VdC
in
-V
—
100
50
—
50
100
50
—
50
100
50
out
load regulation
+V
—
—
25
—
25
out
mV
-V
—
200
7
—
50
200
5
—
50
200
4
out
1, 4
CroSS regulation
inPut Voltage
-V
—
—
3
—
2
%
VDC
V
out
ContinuouS
TRANSIENT 120 ms
no load
16
—
28
—
40
16
—
28
40
16
—
28
40
1
50
—
50
—
50
inPut Current
—
70
—
160
10
—
70
160
10
—
70
160
10
inhibited–inh1
inhibited–inh2
10 mhz - 20 mhz
—
—
—
—
—
mA
—
—
70
—
—
70
—
—
70
inPut riPPle Current
eFFiCienCy
—
—
130
—
—
—
130
—
—
—
130
—
mA p-p
%
80
84
82
86
83
87
load Fault
Power diSSiPation
1
oVerload
—
—
—
—
—
—
30
24
10
—
—
—
—
—
—
30
22
10
—
—
—
—
—
—
30
20
10
W
5
Short CirCuit
1
reCoVery
ms
SteP load reSPonSe
50% - 100% - 50%
tranSient
±V
out
—
—
—
—
500
300
—
—
—
—
600
300
—
—
—
—
600
300
mV pk
µs
6
reCoVery
SteP line reSPonSe
16 - 40 - 16 VdC
±V
1, 7
out
tranSient
—
—
—
—
—
—
—
—
600
300
10
—
—
—
—
—
—
—
—
600
300
10
—
—
—
—
—
—
—
—
750
300
10
mV pk
µs
1, 6
reCoVery
8
Start-uP
delay
ms
1
oVerShoot
50
25
50
mV pk
1
CaPaCitiVe load
no eFFeCt on dC
PerFormanCe
—
—
1000
—
—
1000
—
—
1000
µF
Notes:
1. ꢎꢉꢀꢁꢀꢇꢅꢂꢂꢋ by ꢋꢂꢊꢆgꢇ, ꢇꢃꢅ ꢅꢂꢊꢅꢂꢋ.
2. Output voltage for dual output models is measured at half load.
3. The “Total” specification is the maximum combined current/power of both outputs.
Up to 70% of that total is available from either output provided the other output
maintains a minimum of 15% of the total power used. The 15% minimum
maintains regulation.
4. Effect on negative Vout from 50%/50% loads to 70%/30&% or 30%/70% loads.
5. Short circuit is measured with a 10 milliohm (±10%) resistive load.
6. Time to settle to within 1% of Vout.
7. Transition time > 10 µs
8. Tested on release from inhibit.
www.interpoint.com
Page 12 of 24
MOR Rev K - 20100422
Crane Aerospace & Electronics Power Solutions
Mor sꢆꢇglꢂ ꢀꢇꢋ dꢉꢀl dc/dc cꢃꢇvꢂꢁꢅꢂꢁꢊ
28 Voꢌt input – 120 Watt
Typical Performance Curves: 25°C T , 28 VDC Vin, 100% load, free run, unless otherwise specified.
C
90
80
90
80
90
80
16V
16V
40V
40V
16V
40V
28V
28V
28V
70
70
70
60
50
60
50
60
50
6.6
66
10
100
33
Output Power (Watts)
50
10
100
50
Output Power (Watts)
Output Power (Watts)
MOR283R3S Efficiency
MOR2805S Efficiency
MOR286R3S Efficiency
Fi g u r e 14
Fi g u r e 15
Fi g u r e 16
90
80
90
90
16V
16V
16V
40V
40V
28V
40V
80
70
80
70
28V
28V
70
60
50
60
50
60
50
10.5
105
11
110
12
120
52.5
55
60
Output Power (Watts)
Output Power (Watts)
MOR2812S Efficiency
Output Power (Watts)
MOR2815S Efficiency
MOR289R5S Efficiency
Fi g u r e 17
Fi g u r e 18
Fi g u r e 19
90
80
90
90
80
16V
16V
16V
80
70
40V
28V
40V
28V
40V
28V
70
70
60
50
60
50
60
50
6.6
66
10
100
10
100
33
50
50
Output Power (Watts)
Output Power (Watts)
Output Power (Watts)
MOR283R3D Efficiency
MOR286R3D Efficiency
MOR2805D Efficiency
Fi g u r e 20
Fi g u r e 21
Fi g u r e 22
www.interpoint.com
Page 13 of 24
MOR Rev K - 20100422
Crane Aerospace & Electronics Power Solutions
Mor sꢆꢇglꢂ ꢀꢇꢋ dꢉꢀl dc/dc cꢃꢇvꢂꢁꢅꢂꢁꢊ
28 Voꢌt input – 120 Watt
Typical Performance Curves: 25°C T , 28 VDC Vin, 100% load, free run, unless otherwise specified.
C
90
80
90
80
90
80
16V
16V
16V
40V
40V
40V
28V
28V
28V
70
70
70
60
50
60
50
60
50
10.5
105
11
110
12
120
52.5
55
60
Output Power (Watts)
Output Power (Watts)
Output Power (Watts)
MOR2815D Efficiency
MOR289R5D Efficiency
MOR2812D Efficiency
Fi g u r e 23
Fi g u r e 24
Fi g u r e 25
0
20
0
0
20
20
Negative Output
Positive Output
40
40
60
40
60
60
80
80
80
100
0.1
100
0.1
100
0.1
10
10
1
Frequency (kHz)
10
1
100
100
1
100
Frequency (kHz)
Frequency (kHz)
MOR2815D Audio Rejection
MOR2805S Audio Rejection
MOR2815S Audio Rejection
Fi g u r e 26
Fi g u r e 27
Fi g u r e 28
1 µs/div
25 µs/div
0 V
–
500 ns/div
1 µs/div
Representative of all models
MOR2812D Sync Out
80% Load
MOR2805S Output Ripple (Vout)
MOR2805S Input Ripple Current (Iin)
Fi g u r e 29
Fi g u r e 30
Fi g u r e 31
www.interpoint.com
Page 14 of 24
MOR Rev K - 20100422
Crane Aerospace & Electronics Power Solutions
Mor sꢆꢇglꢂ ꢀꢇꢋ dꢉꢀl dc/dc cꢃꢇvꢂꢁꢅꢂꢁꢊ
28 Voꢌt input – 120 Watt
Typical Performance Curves: 25°C T , 28 VDC Vin, 100% load, free run, unless otherwise specified.
C
100 -50%
Step Load
Vin
Vin
Vout
Vout
Vout
50 - 100%
Step Load
1 ms/div
18 to 40 V, 40 to 18 V
Vin
100 µs/div
All combinations of line and load
MOR2805S Turn On Response
MOR2805S Step Load Response
MOR2805S Step Line Response
Fi g u r e 32
Fi g u r e 33
Fi g u r e 34
Iin
Vout
5 ms/div
1 µs/div
With and without 470 µF cap. load
MOR2805S Inhibit Release Inrush Current
10 µs/div
MOR2815S Output Ripple (Vout)
MOR2815S Input Ripple (Iin)
Fi g u r e 35
Fi g u r e 36
Fi g u r e 37
Vin
Vout
Vin
100 -50%
Step Load
Vout
50 - 100%
Step Load
Vout
Vin
50 µs/div
100 µs/div
2.5 ms/div
18 to 40 V, 40 to 18 V, 50% load
All combinations of line and load
MOR2815S Step Line Response
MOR2815S Step Load Response
MOR2815S Turn On Response
Fi g u r e 38
Fi g u r e 40
Fi g u r e 39
www.interpoint.com
Page 15 of 24
MOR Rev K - 20100422
Crane Aerospace & Electronics Power Solutions
Mor sꢆꢇglꢂ ꢀꢇꢋ dꢉꢀl dc/dc cꢃꢇvꢂꢁꢅꢂꢁꢊ
28 Voꢌt input – 120 Watt
Typical Performance Curves: 25°C T , 28 VDC Vin, 100% load, free run, unless otherwise specified.
C
1 µs/div
Vin
+Vout
+Vout
25 µs/div
–Vout
–Vout
1 µs/div
25 µs/div
80% load each output
80% load each output
18 to 40 V, 80% load each output
MOR2805D Input Ripple (Iin)
MOR2805D Output Ripple (±Vout)
MOR2805D Step Line Response
Fi g u r e 41
Fi g u r e 42
Fi g u r e 43
Vin
100 - 50%
Step Load
+Vout
50 - 100%
Load
+Vout
+Vout
–Vout
50% Load
–Vout
–Vout
50% Load
50 µs/div
25 µs/div
50 µs/div
40 to 18 V, 80% load each output
MOR2805D Step Line Response
MOR2805D Step Load Response
MOR2805D Step Load Response
Fi g u r e 44
Fi g u r e 45
Fi g u r e 46
1 µs/div
+Vout
–Vout
Vin
+Vout
–Vout
25 µs/div
2.5 ms/div
1 µs/div
80% load each output
MOR2805D Turn On Response
MOR2812D Input Ripple (Iin)
MOR2812D Output Ripple (±Vout)
Fi g u r e 47
Fi g u r e 48
Fi g u r e 49
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Page 16 of 24
MOR Rev K - 20100422
Crane Aerospace & Electronics Power Solutions
Mor sꢆꢇglꢂ ꢀꢇꢋ dꢉꢀl dc/dc cꢃꢇvꢂꢁꢅꢂꢁꢊ
28 Voꢌt input – 120 Watt
Typical Performance Curves: 25°C T , 28 VDC Vin, 100% load, free run, unless otherwise specified.
C
100 - 50%
+Vout
–Vout
Step Load
+Vout
+Vout
–Vout
50 - 100%
Step Load
Vin
Vin
50% Load
50% Load
+Vout
100 µs/div
100 µs/div
100 µs/div
18 to 40 V, 40 to 18 V
MOR2812D Step Line Response
MOR2812D Step Load Response
MOR2812D Step Load Response
Fi g u r e 52
Fi g u r e 50
Fi g u r e 51
Vin
Iin
+Vout
Vout
–Vout
2.5 ms/div
5 ms/div
MOR2812D Turn On Response
MOR2812D Inhibit Release Inrush Current
Fi g u r e 53
Fi g u r e 54
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Page 17 of 24
MOR Rev K - 20100422
Crane Aerospace & Electronics Power Solutions
Mor sꢆꢇglꢂ ꢀꢇꢋ dꢉꢀl dc/dc cꢃꢇvꢂꢁꢅꢂꢁ cꢀꢊꢂꢊ
28 Voꢌt input – 120 Watt
TOP VIEW CASE U2
Flanged case, short leads
Case U2 does not require designator in Case Option position of model number for the MOR family
Seam Seal
Angled corner
0.300 ±0.050 (7.60 ±1.27) Pin length
0.128 dia
(3.25).
indicates pin one.
1.505 max. (38.23)
1.380 (35.05)
0.040 dia
(1.02)
1
2
3
4
5
6
12
11
10
9
1.250 (31.75)
1.050 (26.67)
0.850 (21.59)
0.650 (16.51)
0.450 (11.43)
8
0.250 (6.35)
0.120 (3.05)
0.000
7
Case dimensions in inches (mm)
Tolerance ±0.005 (0.13) for three decimal places
±0.01 (0.3) for two decimal places
unless otherwise specified
CAUTION
Heat from reflow or wave soldering may damage the device. Solder pins
individually with heat application not exceeding 300°C for 10 seconds per pin.
Materials
Header
Cover
Pins
Cold Rolled Steel/Nickel/Gold
Kovar/Nickel
#52 alloy/Gold, compresion glass seal
Seal Hole: 0.100 ±0.002 (2.54 ±0.05)
Case U2, Rev E, 20100401
Please refer to the numerical dimensions for accuracy. All information is believed to
be accurate, but no responsibility is assumed for errors or omissions. Interpoint
reserves the right to make changes in products or specifications without notice.
Copyright © 1999-2010 Interpoint Corp. All rights reserved.
Fi g u r e 55: Ca S e u2
www.interpoint.com
Page 18 of 24
MOR Rev K - 20100422
Crane Aerospace & Electronics Power Solutions
Mor sꢆꢇglꢂ ꢀꢇꢋ dꢉꢀl dc/dc cꢃꢇvꢂꢁꢅꢂꢁ cꢀꢊꢂꢊ
28 Voꢌt input – 120 Watt
TOP VIEW CASE V*
Flanged case, down leaded
*Designator "V" required in Case Option position of model number.
Maximum dimensions: 3.005 x 1.505 (76.33 x 38.23 mm)
Angled corner
Seam Seal
indicates pin one.
3.45 (87.6) Reference
(lead center to lead center)
0.128 dia
(3.25)
0.040 dia
(1.02)
1.380 (35.05)
1.250 (31.75)
12
11
10
9
8
7
1
2
3
4
5
6
1.050 (26.67)
0.850 (21.59)
0.650 (16.51)
0.450 (11.43)
0.250 (6.35)
0.120 (3.05)
0.000
Case dimensions in inches (mm)
Tolerance ±0.005 (0.13) for three decimal places
±0.01 (0.3) for two decimal places
unless otherwise specified
CAUTION
Heat from reflow or wave soldering may damage the device. Solder pins
individually with heat application not exceeding 300°C for 10 seconds per pin.
Materials
Header
Cover
Pins
Cold Rolled Steel/Nickel/Gold
Kovar/Nickel
#52 alloy/Gold, compresssion glas seal
Seal Hole: 0.120 ±0.002 (3.05 ±0.05)
Case V, Rev E, 20100106
Please refer to the numerical dimensions for accuracy. All information is believed to
be accurate, but no responsibility is assumed for errors or omissions. Interpoint
reserves the right to make changes in products or specifications without notice.
Copyright © 1999-2009 Interpoint Corp. All rights reserved.
Fi g u r e 56: Ca S e V
www.interpoint.com
Page 19 of 24
MOR Rev K - 20100422
Crane Aerospace & Electronics Power Solutions
Mor sꢆꢇglꢂ ꢀꢇꢋ dꢉꢀl dc/dc cꢃꢇvꢂꢁꢅꢂꢁ cꢀꢊꢂꢊ
28 Voꢌt input – 120 Watt
TOP VIEW CASE W*
Tabbed case, up-leaded
*
Designator "W" required in Case Option position of model number.
0.140 dia
0.250 (6.35) Typ.
(3.56)
Seam Seal
0.250 (6.35)
Typ.
1.750 (44.45)
1.625
(41.28)
0.040 dia
(1.02)
1.375
(34.93)
1
2
3
4
5
6
12
11
10
9
1.175
(29.85
0.975
(24.77)
2.000
(50.80)
0.775
(19.69)
0.575
(14.61)
8
0.375
(9.53)
7
0.125
(3.18)
0.000
Case dimensions in inches (mm)
Tolerance ±0.005 (0.13) for three decimal places
±0.01 (0.3) for two decimal places
unless otherwise specified
Lead Detail
0.84 ±0.05
(21.3 ±1.3)
0.400 (10.16) max.
0.220 (5.59)
0.000
CAUTION
Heat from reflow or wave soldering may damage
the device. Solder pins individually with heat
application not exceeding 300°C for 10 seconds per pin.
0.150 (3.81)
Materials
2.80 (71.1) Reference
(lead center to lead center)
Header
Cover
Pins
Cold Rolled Steel/Nickel/Gold
Kovar/Nickel
#52 alloy/Gold, compresssion glass seal
Seal Hole: 0.120 ±0.002 (3.05 ±0.05)
Case W, Rev E, 20100401
Please refer to the numerical dimensions for accuracy. All information is believed to
be accurate, but no responsibility is assumed for errors or omissions. Interpoint
reserves the right to make changes in products or specifications without notice.
Fi g u r e 57: Ca S e w
www.interpoint.com
Page 20 of 24
MOR Rev K - 20100422
Crane Aerospace & Electronics Power Solutions
Mor sꢆꢇglꢂ ꢀꢇꢋ dꢉꢀl dc/dc cꢃꢇvꢂꢁꢅꢂꢁ cꢀꢊꢂꢊ
28 Voꢌt input – 120 Watt
TOP VIEW CASE Y*
Tabbed case, straight-leaded
*Designator “Y” required in Case Option position of model number.
0.140 dia
0.250 (6.35) Typ.
(3.56)
Seam Seal
0.250 (6.35)
Typ.
1.750 (44.45)
1.625
(41.28)
0.040 dia
(1.02)
1.375
(34.93)
1
2
3
4
5
6
12
11
10
9
1.175
(29.85
0.975
(24.77)
2.000
(50.80)
0.775
(19.69)
0.575
(14.61)
8
0.375
(9.53)
7
0.125
(3.18)
0.000
Case dimensions in inches (mm)
Tolerance ±0.005 (0.13) for three decimal places
±0.01 (0.3) for two decimal places
unless otherwise specified
Lead Detail
0.400 (10.16) max.
0.220 (5.59)
CAUTION
Heat from reflow or wave soldering may damage
the device. Solder pins individually with heat
application not exceeding 300°C for 10 seconds per pin.
0.000
0.30 ±0.05
(7.6 ±1.3)
Materials
3.10 (78.7) Reference
Header
Cover
Pins
Cold Rolled Steel/Nickel/Gold
Kovar/Nickel
#52 alloy/Gold, compresssion glass seal
Seal Hole: 0.120 ±0.002 (3.05 ±0.05)
Case Y, Rev E, 20100420
Please refer to the numerical dimensions for accuracy. All information is believed to
be accurate, but no responsibility is assumed for errors or omissions. Interpoint
reserves the right to make changes in products or specifications without notice.
Copyright © 1999-2010 Interpoint Corp. All rights reserved.
Fi g u r e 58: Ca S e y
www.interpoint.com
Page 21 of 24
MOR Rev K - 20100422
Crane Aerospace & Electronics Power Solutions
Mor sꢆꢇglꢂ ꢀꢇꢋ dꢉꢀl dc/dc cꢃꢇvꢂꢁꢅꢂꢁ cꢀꢊꢂꢊ
28 Voꢌt input – 120 Watt
TOP VIEW CASE Z*
Tabbed case, down-leaded
*Designator “Z” required in Case Option position of model number.
0.140 dia
Seam Seal
0.250 (6.35) Typ.
(3.56)
0.250 (6.35)
Typ.
1.750 (44.45)
1.625
(41.28)
0.040 dia
(1.02)
1.375
(34.93)
1
2
3
4
5
6
12
11
10
9
1.175
(29.85
0.975
(24.77)
2.000
(50.80)
0.775
(19.69)
0.575
(14.61)
8
0.375
(9.53)
7
0.125
(3.18)
0.000
Case dimensions in inches (mm)
Tolerance ±0.005 (0.13) for three decimal places
±0.01 (0.3) for two decimal places
unless otherwise specified
Lead Detail
0.150 (3.81)
0.400 (10.16) max.
CAUTION
0.220 (5.59)
0.000
Heat from reflow or wave soldering may damage
the device. Solder pins individually with heat
application not exceeding 300°C for 10 seconds per pin.
Materials
0.36 ±0.05
(9.1±0.13)
Header
Cover
Pins
Cold Rolled Steel/Nickel/Gold
Kovar/Nickel
#52 alloy/Gold, compresssion glass seal
Seal Hole: 0.120 ±0.002 (3.05 ±0.05)
2.80 (71.1) Reference
(lead center to lead center)
Case Z, Rev E, 20100401
Please refer to the numerical dimensions for accuracy. All information is believed to
be accurate, but no responsibility is assumed for errors or omissions. Interpoint
reserves the right to make changes in products or specifications without notice.
Copyright © 1999-2010 Interpoint Corp. All rights reserved.
Fi g u r e 59: Ca S e z
www.interpoint.com
Page 22 of 24
MOR Rev K - 20100422
Crane Aerospace & Electronics Power Solutions
Mor sꢆꢇglꢂ ꢀꢇꢋ dꢉꢀl dc/dc cꢃꢇvꢂꢁꢅꢂꢁꢊ
28 Voꢌt input – 120 Watt
ST A N D A R D A N D /ES (N O N -QML) A N D /883 (CL A S S H, QML)
PR O D U C T EL E M E N T EV A L U A T I O N
component-level test
perFormeD
stanDarD anD /es
non-Qml 1
/883
class h Qml
M/S 2
P 3
M/S 2
P 3
Element Electrical (probe)
Element Visual
yes
no
no
no
no
no
no
yes
yes
yes
yes
yes
yes
yes
N/A
yes
yes
Internal Visual
N/A
no
Final Electrical
4
Wire Bond Evaluation
no
SLAM™/C-SAM:
Input capacitors only
(Add’l test, not req. by H)
no
no
no
yes
Notes:
1. Standard and /ES, non-QML products, do no meet all of the requirements of
MIL-PRF-38534.
2. M/S = Active components (Microcircuit and Semiconductor Die)
3. P = Passive components
4. Not applicable to EMI filters that have no wire bonds.
Definitions:
Element Evaluation: Component testing/screening per MIL-STD-883 as determined by MIL-PRF-38534
SLAM™: Scanning Laser Acoustic Microscopy
C-SAM: C - Mode Scanning Acoustic Microscopy
SC r e e n i n g ta b l e 1: el e m e n t eV a l u a t i o n
www.interpoint.com
Page 23 of 24
MOR Rev K - 20100422
Crane Aerospace & Electronics Power Solutions
Mor sꢆꢇglꢂ ꢀꢇꢋ dꢉꢀl dc/dc cꢃꢇvꢂꢁꢅꢂꢁꢊ
28 Voꢌt input – 120 Watt
ST A N D A R D A N D /ES (N O N -QML) A N D /883 (CL A S S H, QML)
PR O D U C T EN V I R O N M E N T A L SC R E E N I N G
test perFormeD
125°c stanDarD
non-Qml1
125°c /es
non-Qml1
/883
class h Qml
Pre-cap Inspection
Method 2017, 2032
yes
yes
yes
Temperature Cycle (10 times)
Method 1010, Cond. C, -65°C to 150°C, ambient
Method 1010, Cond. B, -55°C to 125°C, ambient
no
no
no
yes
yes
no
Constant Acceleration
Method 2001, 3000 g
Method 2001, 500 g
no
no
no
yes
yes
no
2
Burn-in
Method 1015, 125°C case, typical
96 hours
160 hours
no
no
yes
no
no
yes
Final Electrical Test MIL-PRF-38534, Group A
Subgroups 1 through 6: -55°C, +25°C, +125°C case
Subgroups 1 and 4: +25°C case
no
yes
no
yes
yes
no
Hermeticity Test
Fine Leak, Method 1014, Cond. A
Gross Leak, Method 1014, Cond. C
Gross Leak, Dip (1 x 10 )
no
no
yes
yes
yes
no
yes
yes
no
-3
Final visual inspection
Method 2009
yes
yes
yes
Test methods are referenced to MIL-STD-883 as determined by MIL-PRF-38534.
Notes:
1. Standard and /ES, non-QML products, do not meet all of the requirements of MIL-PRF-38534.
2. Burn-in temperature designed to bring the case temperature to +125°C
SC r e e n i n g ta b l e 2: en V i r o n m e n t a l SC r e e n i n g
MOR Single and Dual, MOR Rev K - 20100422. This revision supersedes all previous releases. All technical information is believed to be accurate,
but no responsibility is assumed for errors or omissions. Interpoint reserves the right to make changes in products or specifications without notice.
MOR Series is a trademark of Interpoint. Copyright © 1999 - 2010 Interpoint Corporation. All rights reserved. www.interpoint.com
Page 24 of 24
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