LEADER 01591nam  2200445Ia 450 
001 9910698070703321
005 20090210082532.0
035   $a(CKB)5470000002394294
035   $a(OCoLC)302340476
035   $a(EXLCZ)995470000002394294
100   $a20090210d1989      ua             0
101 0 $aeng
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 00$aTwo-stage reusable launch system utilizing a winged core vehicle and glideback boosters$b[electronic resource] /$fIan O. MacConochie ... [and others]
210  1$aHampton, Va. :$cNational Aeronautics and Space Administration, Langley Research Center,$d[1989]
215   $a19 pages $cdigital, PDF file
225 1 $aNASA technical memorandum ;$v101513
300   $aTitle from title screen (viewed Feb. 9, 2009)
300   $a"July 1989."
320   $aIncludes bibliographical references (page 6).
606   $aLaunch complexes (Astronautics)
606   $aCommonality$2nasat
606   $aLaunch vehicles$2nasat
606   $aReusable spacecraft$2nasat
606   $aStructural design$2nasat
615  0$aLaunch complexes (Astronautics)
615  7$aCommonality.
615  7$aLaunch vehicles.
615  7$aReusable spacecraft.
615  7$aStructural design.
701   $aMacConochie$b Ian O$01400955
712 02$aLangley Research Center.
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910698070703321
996   $aTwo-stage reusable launch system utilizing a winged core vehicle and glideback boosters$93500115
997   $aUNINA