external influences such as PCB construction, circuit
layout etc. As such, external components in addition
to those listed herein may be required in specific
instances to gain full compliance to the standards
specified.
[b]
[c]
Compatible with SurfMate and InMate socketing system
Not intended for socket or Surfmate mounting
M-FIAM5B
Page 1 of 7
Rev 4.8
03/2019
M-FIAM5BM21
Specifications
(Typical at T
BP
= 25°C, nominal line and 75% load, unless otherwise specified)
INPUT SPECIFICATIONS
Parameter
Input voltage
Inrush limiting
Transient immunity
Min
14
Typ
28
Max
36
0.007
50
Unit
V
DC
A/µF
V
DC
12.5ms per MIL-STD-704E/F, continuous operation
Test conditions AA and FF normal overvoltage transients per
MIL-HDBK-704
Notes
Continuous
OUTPUT SPECIFICATIONS
Parameter
Output current
Output power
Efficiency
Internal voltage drop
External capacitance
330
1000
µF
96
98
0.5
Min
Typ
Max
20
560
0.7
Unit
A
W
%
V
DC
@ 20A, 100°C baseplate
See Figure 6 on page 5
50V
Notes
CONTROL PIN SPECIFICATIONS
Parameter
ON/OFF control
Enable (ON)
Disable (OFF)
Min
0.0
3.5
Typ
Max
1.0
5.0
Unit
V
DC
V
DC
Notes
Referenced to – V
OUT
100kΩ internal pull up resistor
SAFETY SPECIFICATIONS
Parameter
Min
1,500
2,121
Typ
Max
Unit
V
RMS
V
DC
Notes
Input / Output to Base
Input / Output to Base
D
ielectric withstand
EMI
Standard
MIL-STD-461E
Conducted emissions:
Conducted susceptibility:
Test Procedure
CE101, CE102
CS101, CS114, CS115, CS116
Notes
EMI performance is subject to a wide variety of external influences such as PCB construction, circuit layout etc. As such, external components in addition
to those listed herein may be required in specific instances to gain full compliance to the standards specified.
GENERAL SPECIFICATIONS
Parameter
Weight
Warranty
Min
Typ
Max
3.3 (94)
2
Unit
Ounces (grams)
Years
Notes
M-FIAM5B
Page 2 of 7
Rev 4.8
03/2019
M-FIAM5BM21
Specifications (Cont.)
ENVIRONMENTAL QUALIFICATION
Altitude
MIL-STD-810F, Method 500.4, Procedure I & II, 40,000ft. and 70,000ft. Operational.
Explosive Atmosphere
MIL-STD-810F, Method 511.4, Procedure I, Operational.
Vibration
MIL-STD-810F, Method 514.5, Procedure I, Category 14, Sine and Random vibration per Table 514.5C for Helicopter AH-6J Main Rotor with overall level
of 5.6Grms for 4 hours per axis. MIL-STD-810F, Method 514.5C, General Minimum Integrity Curve per Figure 514.5C-17 with overall level of 7.7Grms
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