Crane Aerospace & Electronics Power Solutions

Mtr (50) single and Dual DC-DC Converters

MTR(50)SingleandDual,MTR-02RevAE-2016.04.26.Thisrevisionsupersedesallpreviousreleases.Alltechnicalinformationisbelievedto

beaccurate,butnoresponsibilityisassumedforerrorsoromissions.CraneElectronics,Inc.reservestherighttomakechangesinproductsor

specificationswithoutnotice.InterpointisaregisteredtrademarkofCraneCo.MTRSeriesisatrademarkofCraneElectronics,Inc.

Copyright©1999-2016CraneElectronics,Inc.Allrightsreserved.www.craneae.com/interpoint

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28 (16-50) VOlt INPut – 30 Watt

Tableisforreferenceonly.SeeindividualSeries'datasheetsforspecificscreening.

nOn

/eS

/883

Pre-cap Inspection, Method 2017, 2032

n

n

n

temperature Cycle (10 times)

Method1010,Cond.C,-65°Cto+150°C,ambient

n

Method1010,Cond.B,-55°Cto+125°C,ambient

n

Constant acceleration

Method2001,3000g

n

Method2001,500g

n

PIND, test Method 2020, Cond. a

n

96hours

n

160hours

n

Final electrical test, MIl-PrF-38534, group a,

Subgroups1through6,-55°C,+25°C,+125°Ccase

n

Subgroups1and4,+25°Ccase

n

n

Hermeticity test

n

n

n

n

GrossLeak,Dip

n

Final visual inspection, Method 2009

n

n

n

TestmethodsarereferencedtoMIL-STD-883asdeterminedbyMIL-PRF-38534.

Notes

1.StandardandESarenon-QMLproductsandmaynotmeetalloftherequirementsofMIL-PRF-38534.

2.AllprocessesareQMLqualifiedandperformedbycertifiedoperators.

3.NotrequiredbyDLAbutperformedtoassureproductquality.

4.Burn-intemperaturedesignedtobringthecasetemperatureto+125°Cminimum.

Burn-inisapoweredtest.