LEADER 01753nam  2200505I  450 
001 9910705481003321
005 20140604091556.0
035   $a(CKB)5470000002450574
035   $a(OCoLC)880929089
035   $a(EXLCZ)995470000002450574
100   $a20140604j201308    ua             0
101 0 $aeng
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aTesting of an annular linear induction pump for the fission surface power technology demonstration unit /$fK.A. Polin [and four others]
210  1$aHuntsville, Alabama :$cNational Aeronautics and Space Administration, Marshall Space Flight Center,$dAugust 2013.
215   $a1 online resource (ix, 21 pages) $cillustrations (some color)
225 1 $aNASA/TP ;$v2013-217487
300   $aTitle from title screen (viewed June 4, 2014).
300   $a"August 2013."
320   $aIncludes bibliographical references (page 21).
606   $aElectric potential$2nasat
606   $aFission$2nasat
606   $aFlow velocity$2nasat
606   $aFrequency ranges$2nasat
606   $aLiquid metals$2nasat
606   $aPressure heads$2nasat
606   $aPumps$2nasat
615  7$aElectric potential.
615  7$aFission.
615  7$aFlow velocity.
615  7$aFrequency ranges.
615  7$aLiquid metals.
615  7$aPressure heads.
615  7$aPumps.
700   $aPolzin$b K. A.$01396047
712 02$aGeorge C. Marshall Space Flight Center,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910705481003321
996   $aTesting of an annular linear induction pump for the fission surface power technology demonstration unit$93502891
997   $aUNINA