| Record ID | harvard_bibliographic_metadata/ab.bib.13.20150123.full.mrc:268118023:1565 |
| Source | harvard_bibliographic_metadata |
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LEADER: 01565nam a2200409Ia 4500
001 013231950-0
005 20120608023231.0
006 m d f
008 110802s2011 alua obt f000 0 eng d
035 0 $aocn744420941
035 $a(FDLP)ocn744420941
040 $aGPO$cGPO
074 $a0830-H-15 (online)
086 0 $aNAS 1.60:2011-216457
100 1 $aNettles, A. T.$q(Alan T.)
245 14 $aThe effects of foam thermal protection system on the damage tolerance characteristics of composite sandwich structures for launch vehicles$h[electronic resource] /$cA.T. Nettles, A.J. Hodge, and J.R. Jackson.
260 $a[Huntsville], Ala. :$bNational Aeronautics and Space Administration, Marshall Space Flight Center,$c[2011]
300 $a1 online resource (vii, 23 p.) :$bill.
490 1 $aNASA/TP ;$v2011-216457
500 $aTitle from title screen (viewed on Aug. 2, 2011).
500 $a"February 2011."
504 $aIncludes bibliographical references (p. 22-23).
650 7 $aDamage assessment.$2nasat
650 7 $aLaunch vehicles.$2nasat
650 7 $aThermal protection.$2nasat
650 7 $aSandwich structures.$2nasat
650 7 $aResidual strength.$2nasat
650 7 $aAres 1 launch vehicle.$2nasat
650 7 $aComposite structures.$2nasat
650 7 $aComposite materials.$2nasat
650 7 $aImpact damage.$2nasat
700 1 $aHodge, A. J.
700 1 $aJackson, J. R.
710 2 $aGeorge C. Marshall Space Flight Center.
830 0 $aNASA technical paper ;$v216457.
988 $a20120608
906 $0OCLC