SMFLH2812SHO CRANE [Crane Aerospace & Electronics.], SMFLH2812SHO Datasheet - Page 12

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SMFLH2812SHO

Manufacturer Part Number
SMFLH2812SHO
Description
SMFLHP Single and Dual DC/DC Converters
Manufacturer
CRANE [Crane Aerospace & Electronics.]
Datasheet
www.craneae.com
END ITEM-LEVEL TEST
PERFORMED
Non-destruct bond pull
Pre-cap Inspection
Temperature Cycle (10 times)
Constant Acceleration
PIND Test
Pre burn-in test
Burn-in
Final Electrical Test MIL-PRF-38534
Radiography
Post Radiography Electrical Test
Hermeticity Test
Final visual inspection
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 required by DSCC but performed to assure product quality.
Method 2023
Method 2017, 2032
Method 1010, Cond. C, -65°C to 150°C, ambient
Method 2001, 3000 g
Method 2020, Cond. A
Method 1015, 125°C case, typical
Group A, Subgroups 1 through 6
Method 2012
Room temperature
Fine Leak, Method 1014, Cond. A
Gross Leak, Method 1014, Cond. C
Method 2009
96 hours
160 hours
2 x 160 hours (includes mid-BI test)
-55°C, +25°C, +125°C case
C
LASS
H
SMFLHP Single and Dual DC/DC Converters
AND
K, MIL-PRF-38534 E
28 VOLT INPUT – 100 WATT
SPACE PROTOTYPE (O)
Rev H - 20071221
Page 12 of 13
NON-QML
N/A
N/A
yes
yes
yes
yes
yes
yes
yes
yes
yes
no
no
no
no
NVIRONMENTAL
1
Crane Aerospace & Electronics Power Solutions
CLASS H
QML
yes
yes
yes
yes
yes
yes
yes
yes
N/A
N/A
yes
yes
yes
no
no
2
2
S
CREENING
CLASS K
QML
yes
N/A
yes
yes
yes
yes
yes
yes
yes
yes
yes
yes
yes
no
no
2

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