| Record ID | harvard_bibliographic_metadata/ab.bib.13.20150123.full.mrc:262789179:1444 |
| Source | harvard_bibliographic_metadata |
| Download Link | /show-records/harvard_bibliographic_metadata/ab.bib.13.20150123.full.mrc:262789179:1444?format=raw |
LEADER: 01444nam a2200397Ia 4500
001 013228864-8
005 20120706194821.0
006 m d f
008 110310s2010 alua obt f000 0 eng d
035 0 $aocn706732471
035 $a(FDLP)ocn706732471
040 $aGPO$cGPO
074 $a0830-H-15 (online)
086 0 $aNAS 1.60:2010-216434
100 1 $aNettles, A. T.$q(Alan T.)
245 00 $aSimplification of fatigue test requirements for damage tolerance of composite interstage launch vehicle hardware$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[2010]
300 $a1 online resource (27 p.) :$bill.
490 1 $aNASA/TP ;$v2010-216434
500 $aTitle from title screen (viewed on March 10, 2011).
500 $a"June 2010."
504 $aIncludes bibliographical references (p. 24-27).
536 $dM-1283
650 7 $aTolerances (mechanics)$2nasat
650 7 $aFatigue (materials)$2nasat
650 7 $aComposite materials.$2nasat
650 7 $aCompression loads.$2nasat
650 7 $aDegradation.$2nasat
650 7 $aDamage.$2nasat
650 7 $aFailure.$2nasat
700 1 $aHodge, A.J.
700 1 $aJackson, J.R.
710 2 $aGeorge C. Marshall Space Flight Center.
830 0 $aNASA technical paper ;$v216434.
988 $a20120608
906 $0OCLC