| Record ID | marc_miami_univ_ohio/allbibs0087.out:2256470:1251 |
| Source | Miami University of Ohio |
| Download Link | /show-records/marc_miami_univ_ohio/allbibs0087.out:2256470:1251?format=raw |
LEADER: 01251nam 2200277 i 4500
001 ocm04015749
008 780629s1977 dcua b f00010 eng d
020 $bpbk
040 $cGPO
049 $aMIB*
074 $a0830-D
086 $aNAS 1.15:74056
086 $aNAS 1.15:74056
100 10 $aFreeman, Delma C
245 10 $aStatic aerodynamic characeristics of a single-stage-to-orbit vehicle with low planform loading at Mach numbers from 0.3 to 4.63 /$cDelma C. Freemand, Jr. and Roger H. Fournier
260 0 $a[Washington] :$bNational Aeronautics and Space Administration, Scientific and Technical Information Office ;$aSpringfield, Va. :$bfor sale by the National Information Service,$c1977
300 $a66 p. :$bill. ;$c27 cm
490 0 $aNASA technical memorandum ; 74056
500 $aIssued Nov. 1977
504 $aIncludes bibliographical references
650 $aStability of space vehicles
700 10 $aFournier, Roger H.,$ejoint author
710 10 $aUnited States.$bNational Aeronautics and Space Administration.$bScientific and Technical Information Office
907 $a.b21507326$b05-20-98$c11-13-94
998 $adoc$b11-13-94$cm$da$e-$feng$gdcu$h0$i1
945 $g1$j0$ldocsf$nrecd$o-$p$0.00$sf$t21$u0$v0$w0$x0$y.i25473360$z11-13-94