Crane Aerospace & Electronics Power Solutions
sFcs28-461 eMi input Filters
28 Volt input – 5 aMp
c
laSS
H
and
k, Mil-prF-38534 e
nvirOnMental
S
creening
t
eSt
p
erFOrMed
(
end iteM level
)
Non-destruct bond pull
2
Method 2023
Pre-cap Inspection
Method 2017, 2032
Temperature Cycle (10 times)
Method 1010, Cond. C, -65°C to 150°C, ambient
Constant Acceleration
Method 2001, 3000 g
PIND Test
Method 2020, Cond. A
Pre burn-in test
Burn-in
Method 1015, 125°C case, typical
96 hours
160 hours
2 x 160 hour (includes mid BI test)
Final electrical test MIL-PRF-38534
Group A, Subgroups 1 through 6
-55°C, +25°C, +125°C case
Radiography
Method 2012
Post Radiography Electrical Test
Room temperature
Hermeticity test
Fine Leak, Method 1014, Cond. A
Gross Leak, Method 1014, Cond. C
Final visual inspection
Method 2009
p
rOtOtype
O
nOn
-QMl
1
no
yes
yes
yes
no
yes
yes
no
no
yes
N/A
N/A
yes
yes
yes
S
pace
c
laSS
H, QMl
yes
3
yes
yes
yes
yes
3
yes
no
yes
no
yes
N/A
N/A
yes
yes
yes
c
laSS
k, QMl
yes
yes
yes
yes
yes
yes
no
no
yes
yes
yes
yes
3
yes
yes
yes
Test methods are referenced to MIL-STD-883 as determined by MIL-PRF-38534.
Notes:
1. Space Prototype (O), non-QML products, do not meet all of the requirements of MIL-PRF-38534.
2. Not applicable to EMI filters that have no wirebonds.
3. Not required by DSCC but performed to assure product quality.
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