| Record ID | bcl_marc/bcl_open.03.mrc:196166646:1373 |
| Source | bcl_marc |
| Download Link | /show-records/bcl_marc/bcl_open.03.mrc:196166646:1373?format=raw |
LEADER: 01373nam 22003737a 4500
004 GPP0465
005 20000524102200.0
008 980910s1997 txu b f000 0 eng d
035 $a(OCoLC)ocm39850867
035 9 $aGPP0465
037 $a19970021239$bNASA
040 $aGPO$cGPO$dDLC$dMvI
049 $aBXMX
074 $a0830-H-15 (MF)
086 0 $aNAS 1.60:3683
100 1 $aSmith, James P.
245 10 $aX-38 vehicle 131 flutter assessment$h[microform] /$cJames P. Smith.
260 $a[Houston, Tex.] :$bNational Aeronautics and Space Administration, Lyndon B. Johnson Space Center ;$a[Springfield, Va. :$bNational Technical Information Service, distributor,$c1997]
300 $a1 v.
490 1 $aTechnical paper ;$v3683
500 $aShipping list no.: 98-0733-M.
533 $aMicrofiche.$b[Washington, D.C. :$cNational Aeronautics and Space Administration,$d1997]$e1 microfiche.
650 7 $aFlutter analysis.$2nasat
650 7 $aAerodynamic characteristics.$2nasat
650 7 $aAerodynamic forces.$2nasat
650 7 $aX-38 crew return vehicle.$2nasat
650 7 $aAerodynamic balance.$2nasat
650 7 $aDamping.$2nasat
650 7 $aRudders.$2nasat
650 7 $aFins.$2nasat
710 2 $aLyndon B. Johnson Space Center.
830 0 $aNASA technical paper$v3683.
852 30 $aMChB$bGOV$cFICHE$hNAS 1.60:3683$91
948 $aLTI 08/08/2000