LEADER 01544oam  2200457Ia 450 
001 9910699342503321
005 20230902161819.0
035   $a(CKB)5470000002402492
035   $a(OCoLC)227912280
035   $a(EXLCZ)995470000002402492
100   $a20080513d2006      ua             0
101 0 $aeng
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aEffect of the FlashJet paint removal system on rotor blade skin materials$b[electronic resource] /$fScott Grendahl
210  1$aAberdeen Proving Ground, MD :$cArmy Research Laboratory,$d[2006]
215   $a1 online resource (vi, 28 pages) $ccolor illustrations
225 1 $aARL-TR ;$v4003
300   $aTitle from title screen (viewed on Sept. 27, 2011).
300   $a"December 2006."
320   $aIncludes bibliographical references (page 26).
410  0$aARL-TR (Aberdeen Proving Ground, Md.) ;$v4003.
606   $aBlades$xMechanical properties
606   $aPaint removers
606   $aCoatings
615  0$aBlades$xMechanical properties.
615  0$aPaint removers.
615  0$aCoatings.
700   $aGrendahl$b Scott$01391695
712 02$aU.S. Army Aviation and Missile Command.
712 02$aU.S. Army Research Laboratory.
801  0$bDTICE
801  1$bDTICE
801  2$bOCLCQ
801  2$bGPO
906   $aBOOK
912   $a9910699342503321
996   $aEffect of the FlashJet paint removal system on rotor blade skin materials$93511887
997   $aUNINA