01349cam2-2200409---450-99000300507020331620110421110336.0978-88-217-2448-0000300507USA01000300507(ALEPH)000300507USA0100030050720071105d2007----|||y0itay0103----baitaITy|||n|||001||2007guida alla compilazione quadro per quadro, casistica ed esempi praticiFrancesco Scopacasaaggiornato on-line[Milanofiori, Assago]IPSOA2007362 p.24 cmDichiarazioni fiscali 200712001Dichiarazioni fiscali 200710010003523842001Dichiarazione IvaImposta sul valore aggiuntoGuide pratiche343.45055SCOPACASA,Francesco298440ITsalbcISBD990003005070203316XXIV.5.C. 813 (IG VII 983)15964 E.C.XXIV.5.C.00064383BKGIUiuCHIARA9020071105USA011210IANNONE9020090408USA011231RSIAV49020090904USA011110RSIAV29020101214USA011031CHIARA9020110421USA01110320071515444UNISA02033nam 2200613I 450 991070462990332120130708092902.0(CKB)5470000002443418(OCoLC)852140947(EXLCZ)99547000000244341820130708d2013 ua 0engurmn|||||||||txtrdacontentcrdamediacrrdacarrierMars Sample Return Mars ascent vehicle mission & technology requirements /Jerrey V. Bowles, Loc C. Huynh, Veronica M. HawkeMoffett Field, CA :National Aeronautics and Space Administration, Ames Research Center,2013.1 online resource (50 pages) illustrations (some color)NASA/TM ;2013-216511Title from title screen (viewed on July 8, 2013)."March 2013."Includes bibliographical references (page 50).Mars Sample Return Mars sample return missionsnasatCost effectivenessnasatLaunch vehiclesnasatAscentnasatMission planningnasatHypergolic rocket propellantsnasatEngine designnasatAscent propulsion systemsnasatSpacecraft designnasatAeroshellsnasatMars sample return missions.Cost effectiveness.Launch vehicles.Ascent.Mission planning.Hypergolic rocket propellants.Engine design.Ascent propulsion systems.Spacecraft design.Aeroshells.Bowles Jerrey V.1398674Huynh Loc C.Hawke VeronicaAmes Research Center,GPOGPOBOOK9910704629903321Mars Sample Return3462400UNINA