| Record ID | harvard_bibliographic_metadata/ab.bib.13.20150123.full.mrc:625808971:1618 |
| Source | harvard_bibliographic_metadata |
| Download Link | /show-records/harvard_bibliographic_metadata/ab.bib.13.20150123.full.mrc:625808971:1618?format=raw |
LEADER: 01618nam a2200445 i 4500
001 013590454-4
005 20130504133621.0
006 m o d f
008 121226s2012 vaua obt f000 0 eng c
035 0 $aocn822966153
035 $a(FDLP)ocn822966153
040 $aGPO$beng$erda$cGPO
042 $apcc
074 $a0830-H-15 (online)
086 0 $aNAS 1.60:2012-217595
100 1 $aBlosser, Max L.
245 10 $aAnalysis and sizing for transient thermal heating of insulated aerospace vehicle structures /$cMax L. Blosser.
264 1 $aHampton, Va. :$bNational Aeronautics and Space Administration, Langley Research Center,$c2012.
300 $a1 online resource (50 pages) :$bcolor illustrations
336 $atext$btxt$2rdacontent
337 $acomputer$bc$2rdamedia
338 $aonline resource$bcr$2rdacarrier
490 1 $aNASA/TP ;$v2012-217595
500 $aTitle from title screen (viewed on Dec. 26, 2012).
500 $a"August 2012."
504 $aIncludes bibliographical references (pages 44-45).
536 $aSponsored by National Aeronautics and Space Administration$h736466.01.08.07.09.02
536 $dL-20165
650 7 $aSize (dimensions)$2nasat
650 7 $aAerospace vehicles.$2nasat
650 7 $aInsulation.$2nasat
650 7 $aTransient heating.$2nasat
650 7 $aAircraft structures.$2nasat
650 7 $aTransient response.$2nasat
650 7 $aMathematical models.$2nasat
650 7 $aHypersonic vehicles.$2nasat
710 2 $aLangley Research Center.
830 0 $aNASA technical paper ;$v2012-217595.
988 $a20130112
906 $0OCLC