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O
UTPUT
C
HARACTERISTICS
Voltage & Current Ratings
2
Output Voltage Accuracy
Single/Dual Output Models
Triple Output Models
Voltage Adjustment
3
Voltage Balance
4
Dual Outputs
Triple Outputs (Aux. Outputs)
Ripple & Noise, 20 MHz BW
Line Regulation
Single Output Models
Dual Output Models
Triple Output Models: Primary
Aux.
Load Regulation
Single Output Models
Dual Output Models
Triple Output Models:Primary
Aux.
Min. Load
Temperature Coefficient @ FL
Temperature Coefficient Balance
Transient Recovery Time
5
Short Circuit Protection
Over Voltage Protection
Unit/Comments
See Model Selection Guide
±1%, Max.
±4%, Max.
±5%
±2%, Max.
±4%, Max.
1% Pk-Pk of Vout
±0.5%, Max.
±0.5%, Max.
±0.5%, Max.
±1.0%, Max.
±0.5%, Max.
±1.0%, Max.
±0.5%, Max.
±1.0%, Max.
10% of Full Load
±0.02%/
o
C, Max.
±1%
100
μSec
Max. to 1%of Final
value
All outputs, by input current
limiting
See Model Selection Guide
E-mail:info@make-ps.com
I
NPUT
C
HARACTERISTICS
Input Voltage, Nominal
Input Voltage range
1
Input Surge
Input Filter
Unit/ Comments
28 VDC
18 VDC to 36 VDC
Per Mil-STD-704D and MIL- STD-1275A
Dual input(π )Pi Network.
Differential and common mode
type. Meets the requirements of
FCC 20780 Class B for computing
dervices. Meets requirements of
MIL-STD-461C, CE01.
12A, Max.
150% of Current Input
> 50 VDC
8 VDC
600W @ 1 mSec
5.5 VDC or Open Circuit
0 VDC to 0.8 VDC
Negative (-) Input
TTL Open Collector or CMOS Open
Drain
32 mA
Reverse Polarity Input Current
Short Circuit Current Limit
Overvoltage Shutdown
Undervotlage Shutdown
Transient Protection
Remote On/Off control
Supply On
Supply Off
Logic Input Reference
Logic Compability
Standby Current
G
ENERAL
C
HARACTERISTICS
Efficiency
6
Isolation Voltage Isolation
Isolation Resistance
Acceleration
Unit / Comment
See Model Selection Guide
1000 VDC, Min; Primary to sec. for
1 min. per MIL-STD-202F, Method 301.
100 MOhms per MIL-STD-202F,
Method 302, Test condition B
Per MIL-STD-810E, Method 513.4,
Prodedure II. Operation test
(centrifuge) 12g’s (Manned Aerospace
Vehicles).
Per MIL-STD-810E, Method 516.4,
Procedure I. Functional shock 40g’s.
Per MIL-STD-810E, Method 514.4,
Prodedure I, Cat 6 (equipment
installed in Helicopters)
Per MIL-STD-810E, Method 500.3,
Prodedure III. Rapid decompression,
40K ft.
Per MIL-STD-810E, Method 507.3,
Procedure I. Natural non-hazardous
items, cycle 1,240 Hrs.
100 kHz, Min.
S
PECIFIATION
N
OTES
1
2
Shock
Vibration
Altitude
Humidity
Switching Frequency
3
4
5
6
7
= The max. input range of 16 to 50 VDC is specified for 250 mS (Per
MIL-STD-704D).
= Total output power should not exceed 16W. The load on
any auxiliary output should not exceed 500 mA.
= Outputs are adjustable on single and dual output units only.
= Voltage balance is measured with balanced loads applied.
= Transient response is measured on the primary output for a 50%
load change (50% load to full load).
= Efficiency is specified at nominal input line and full load.
= These converters have a thermal resistance of 2.1
o
C/W (Internally
dissipated). The internal thermal protection circuits are trigged if
the case temperature exceeds 95
o
C. Maintaining the module case
temp. below 95
o
C can be accomplished by mounting a low
thermal resistance heat sink (with vertically orientated fins) to the
case with a thermally conductive compond. This will significantly
increase heat transfer from the module to the ambient. Forced
convection cooling can also be used. The amount of cooling will
depend upon the flow of air in linear feer per minute (LFM) over
the module.
>> 2
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