Record ID | marc_loc_2016/BooksAll.2016.part30.utf8:65400706:3876 |
Source | Library of Congress |
Download Link | /show-records/marc_loc_2016/BooksAll.2016.part30.utf8:65400706:3876?format=raw |
LEADER: 03876cam a22003497a 4500
001 2002421707
003 DLC
005 20070724083441.0
008 020528s1998 at a b 001 0 eng d
010 $a 2002421707
035 $a(OCoLC)ocm40516417
040 $aNAG$cNAG$dDLC
042 $alccopycat
020 $a905699090X
050 00 $aTL1075$b.L23 1998
082 00 $a629.4/11$221
100 1 $aLabunsky, Alexei V.
245 10 $aMultiple gravity assist interplanetary trajectories /$cAlexei V. Labunsky, Oleg V. Papkov, and Konstantin G. Sukhanov.
260 $aAustralia :$bGordon and Breach Science Publishers,$cc1998.
300 $avi, 285 p. :$bill. ;$c26 cm.
490 1 $aEarth Space Institute book series,$x1026-2660 ;$vv. 3
504 $aIncludes bibliographical references (p. 267-277) and indexes.
505 8 $aMachine generated contents note: 1. Dynamic scheme, models, and methods of analysis of spacecraft -- trajectories using gravity assist maneuvers -- 1.1. Dynamic scheme -- 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. Application of the graphic-analytical method to multi-purpose -- mission analysis -- 2.3. A universal algorithm for the synthesis of spacecraft multi-purpose -- 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 -- 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 -- 4.1.7. Flights 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. Numerical 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 perturbation potential -- 5.2. Formation of spacecraft orbits in planetary satellite systems -- 5.3. The use of gravity assist maneuvers to orbit the spacecraft -- as an artificial planetary satellite -- 5.4. Multi-purpose flight schemes to natural planetary satellites -- 6. Flights to small bodies in the solar system -- 6.1. Examination of flight schemes to comets -- 6.2. Examination of flight schemes to asteroids -- 7. Solution of navigational problems for multi-purpose missions -- at near-planet segments of the flight trajectory -- 7.1. Formation of descent and flyby trajectories -- 7.2. Determining the trajectories of interplanetary probes -- 7.3. Examples of application of the methods of planetocentric -- orbit analysis -- References -- Author index -- Subject index.
650 0 $aSpace trajectories.
650 0 $aCelestial mechanics.
650 0 $aOrbital mechanics.
650 0 $aGravity assist (Astrodynamics)
700 1 $aPapkov, Oleg V.
700 1 $aSukhanov, Konstantin G.
830 0 $aEarth Space Institute book series on public and private sector interest in space ;$vv. 3.
856 41 $3Table of contents$uhttp://www.loc.gov/catdir/toc/fy022/2002421707.html
856 42 $3Publisher description$uhttp://www.loc.gov/catdir/enhancements/fy0731/2002421707-d.html