LEADER 02309nam  2200589I  450 
001 9910704624103321
005 20131121115833.0
035   $a(CKB)5470000002443477
035   $a(OCoLC)863637849
035   $a(EXLCZ)995470000002443477
100   $a20131121d2012      ua             0
101 0 $aeng
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aDesign and manufacturing considerations for shockproof and corrosion-immune superelastic nickel-titanium bearings for a space station application /$fChristopher DellaCorte and Walter A. Wozniak
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Glenn Research Center,$d[2012]
215   $a1 online resource (11 pages) $cillustrations
225 1 $aNASA/TM ;$v2012-216015
300   $aTitle from title screen (viewed Nov. 21, 2013).
300   $a"May 2012."
300   $a"Prepared for the 41st Aerospace Mechanisms Symposium cosponsored by the NASA Jet Propulsion Laboratory and Lockheed Martin Space Systems Company, Pasadena, California, May 16-18, 2012."
320   $aIncludes bibliographical references (pages 11).
606   $aTitanium alloys$2nasat
606   $aNickel alloys$2nasat
606   $aBall bearings$2nasat
606   $aCorrosion resistance$2nasat
606   $aHeat treatment$2nasat
606   $aIntermetallics$2nasat
606   $aResidual stress$2nasat
606   $aModulus of elasticity$2nasat
606   $aFracture mechanics$2nasat
615  7$aTitanium alloys.
615  7$aNickel alloys.
615  7$aBall bearings.
615  7$aCorrosion resistance.
615  7$aHeat treatment.
615  7$aIntermetallics.
615  7$aResidual stress.
615  7$aModulus of elasticity.
615  7$aFracture mechanics.
700   $aDellaCorte$b Christopher$01386701
702   $aWozniak$b Walter A.
712 02$aFundamental Aeronautics Program (U.S.),
712 02$aNASA Glenn Research Center,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910704624103321
996   $aDesign and manufacturing considerations for shockproof and corrosion-immune superelastic nickel-titanium bearings for a space station application$93533520
997   $aUNINA