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MARC Record from marc_columbia

Record ID marc_columbia/Columbia-extract-20221130-031.mrc:424774912:5593
Source marc_columbia
Download Link /show-records/marc_columbia/Columbia-extract-20221130-031.mrc:424774912:5593?format=raw

LEADER: 05593cam a2200805Mi 4500
001 15408567
005 20220528233313.0
006 m o d
007 cr |||||||||||
008 171103r20171998enk ob 001 0 eng d
035 $a(OCoLC)on1012165537
035 $a(NNC)15408567
040 $aNLE$beng$erda$cNLE$dOCLCO$dOCLCF$dOCLCQ$dUKMGB$dNLW$dTYFRS$dK6U$dOCLCO
015 $aGBB7L7735$2bnb
016 7 $a018593843$2Uk
020 $a9781351429702$q(ePub ebook)
020 $a1351429701$q(ePub ebook)
020 $a9780203746288$q(electronic bk.)
020 $a0203746287$q(electronic bk.)
020 $a9781351429696$q(electronic bk. : Mobipocket)
020 $a1351429698$q(electronic bk. : Mobipocket)
020 $a9781351429719$q(electronic bk. : PDF)
020 $a135142971X$q(electronic bk. : PDF)
020 $z9789056990909$q(hardback)
020 $z905699090X$q(hardback)
035 $a(OCoLC)1012165537
037 $a9781351429702$bIngram Content Group
037 $a9780203746288$bTaylor & Francis
050 4 $aTL1075
072 7 $aTEC$x009000$2bisacsh
072 7 $aSCI$x055000$2bisacsh
072 7 $aPH$2bicssc
082 04 $a629.4/11$223
049 $aZCUA
100 1 $aLabunsky, Alexei V.,$eauthor.
245 10 $aMultiple gravity assist interplanetary trajectories /$cAlexei V. Labunsky, Oleg V. Papkov and Konstantin G. Sukhanov.
264 1 $a[Abingdon] :$b[Routledge],$c[2017?]
264 4 $c©1998
300 $a1 online resource
336 $atext$btxt$2rdacontent
337 $acomputer$bc$2rdamedia
338 $aonline resource$bcr$2rdacarrier
500 $aOriginally published: Boca Raton : CRC Press, 1998.
504 $aIncludes bibliographical references and indexes.
505 0 $a""Cover""; ""Half Title""; ""Title Page""; ""Copyright Page""; ""Table of Contents""; ""Introduction""; ""1: Dynamic scheme, models, and methods of analysis of spacecraft trajectories using gravity assist maneuvers ""; ""1.1. Dynamic scheme""
505 0 $a""1.2. Effect of perturbation maneuvers on the spacecraft orbital characteristics""""1.3. Flight paths; methods of study""; ""2: Methods and algorithms for the development of optimal multi-purpose missions ""; ""2.1. Graphic-analytical method""; ""2.2. AppUcation of the graphic-analytical method to multi-purpose mission analysis""
505 0 $a""2.3. A universal algorithm for the synthesis of spacecraft multi-piupose missions""""2.4. Formation of multi-purpose spacecraft missions in the solar system""; ""3: Ballistic methods in multi-purpose interplanetary spacecraft design""; ""3.1. Isoline method""; ""3.2. Optimization of design and ballistic characteristics of multi-purpose spacecraft""; ""3.3. Optimization of design solutions based on the generalized criterion method""
505 0 $a""4: Analysis of multi-purpose schemes of interplanetary flight """"4.1. Nomographic analysis of spacecraft multi-purpose paths in the solar system""; ""4.1.1. Paths to Mars and Venus""; ""4.1.2. Recurrent and periodically-recurrent trajectories""; ""4.1.3. Flights to Mercury""; ""4.1.4. Flights to Jupiter""; ""4.1.5. Flights to Saturn""; ""4.1.6. Flights to Uranus""
505 0 $a""4.1.7. FUghts to Neptune and Pluto""""4.1.8. Nomographic analysis of the perturbation potential of the Earth in interplanetary flight schemes""; ""4.1.9. Flights to the sun""; ""4.2. Nmnerical studies of some promising schemes of planetary flights""; ""4.3. Examination of periodical recurrent trajectories with multiple flybys of Mars and Earth""; ""5: Multi-purpose flights in planetary-satellite systems""; ""5.1. Natural planetary satellites and their pertiubation fx>tential""; ""5.2. Formation of spacecraft orbits in planetary satellite systems""
520 $aReflecting the results of twenty years; experience in the field of multipurpose flights, this monograph includes the complex routes of the trajectories of a number of bodies (e.g., space vehicles, comets) in the solar system. A general methodological approach to the research of flight schemes and the choice of optimal performances is developed. Additionally, a number of interconnected methods and algorithms used at sequential stages of such development are introduced, which allow the selection of a rational multipurpose route for a space vehicle, the design of multipurpose orbits, the determination of optimal space vehicle design, and ballistic performances for carrying out the routes chosen. Other topics include the practical results obtained from using these methods, navigation problems, near-to-planet orbits, and an overview of proven and new flight schemes.
650 0 $aSpace trajectories.
650 0 $aInterplanetary voyages.
650 0 $aCelestial mechanics.
650 0 $aSpace flight.
650 6 $aTrajectoires spatiales.
650 6 $aVoyages interplanétaires.
650 6 $aMécanique céleste.
650 6 $aVol spatial.
650 7 $aTECHNOLOGY & ENGINEERING$xEngineering (General)$2bisacsh
650 7 $aSCIENCE / Physics$2bisacsh
650 7 $aCelestial mechanics.$2fast$0(OCoLC)fst00850133
650 7 $aInterplanetary voyages.$2fast$0(OCoLC)fst00977455
650 7 $aSpace flight.$2fast$0(OCoLC)fst01127676
650 7 $aSpace trajectories.$2fast$0(OCoLC)fst01127942
655 0 $aElectronic books.
655 4 $aElectronic books.
700 1 $aPapkov, Oleg V.,$eauthor.
700 1 $aSukhanov, Konstantin G.,$eauthor.
856 40 $uhttp://www.columbia.edu/cgi-bin/cul/resolve?clio15408567$zTaylor & Francis eBooks
852 8 $blweb$hEBOOKS