LEADER 01681nam  2200469I  450 
001 9910705900503321
005 20170712141923.0
035   $a(CKB)5470000002453407
035   $a(OCoLC)993603170
035   $a(EXLCZ)995470000002453407
100   $a20170712j201703    ua             0
101 0 $aeng
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aApplication of the Brinkley Dynamic Response Criterion to spacecraft transient dynamic events /$fJeffrey T. Somers, Dustin Gohmert, James W. Brinkley
210  1$aHouston, Texas :$cNational Aeronautics and Space Administration, Lyndon B. Johnson Space Center,$dMarch 2017.
215   $a1 online resource (76 pages) $ccolor illustrations
225 1 $aNASA-TM ;$v2013-217380
300   $a"March 2017."
320   $aIncludes bibliographical references (pages 58-66).
606   $aAdditive manufacturing$2nasat
606   $aGas atomization$2nasat
606   $aHeat resistant alloys$2nasat
606   $aPowder (particles)$2nasat
606   $aShape memory alloys$2nasat
615  7$aAdditive manufacturing.
615  7$aGas atomization.
615  7$aHeat resistant alloys.
615  7$aPowder (particles)
615  7$aShape memory alloys.
700   $aSomers$b Jeffrey T.$01419613
702   $aGohmert$b Dustin
702   $aBrinkley$b James W.
712 02$aLyndon B. Johnson Space Center,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910705900503321
996   $aApplication of the Brinkley Dynamic Response Criterion to spacecraft transient dynamic events$93534650
997   $aUNINA