LEADER 01661oam  2200481   450 
001 9910716087103321
005 20210430122050.0
035   $a(CKB)5470000002517230
035   $a(OCoLC)761210058
035   $a(EXLCZ)995470000002517230
100   $a20111115j196902    ua             0
101 0 $aeng
135   $aur|||||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aPerformance of a towed, 48-inch-diameter (121.92-cm) ballute decelerator tested in free flight at Mach numbers from 4.2 to 0.4 /$fby J.W. Usry
210  1$aWashington, D.C. :$cNational Aeronautics and Space Administration,$dFebruary 1969.
215   $a1 online resource (31 pages) $cillustrations
225 1 $aNASA/TN ;$vD-4943
300   $a"February 1969."
320   $aIncludes bibliographical references (page 12).
517   $aPerformance of a towed, 48-inch-diameter 
606   $aMach number$2nasat
606   $aBallutes$2nasat
606   $aAcceleration (Mechanics)$2fast
606   $aParachutes$xTesting$2fast
615  7$aMach number.
615  7$aBallutes.
615  7$aAcceleration (Mechanics)
615  7$aParachutes$xTesting.
700   $aUsry$b J. W.$01401643
712 02$aUnited States.$bNational Aeronautics and Space Administration,
801  0$bOCLCE
801  1$bOCLCE
801  2$bOCLCQ
801  2$bOCLCF
801  2$bOCLCQ
801  2$bGPO
906   $aBOOK
912   $a9910716087103321
996   $aPerformance of a towed, 48-inch-diameter (121.92-cm) ballute decelerator tested in free flight at Mach numbers from 4.2 to 0.4$93470601
997   $aUNINA