000			04083cam a22003857a 4500
999			_c81050 _d81050
001			12789436
003			OSt
005			20220629164646.0
008			020528s1998 at a b 001 0 eng d
010			_a 2002421707
020			_a9780367900014 (Set)
020			_a9780367850180 (hbk)
035			_a(OCoLC)ocm40516417
040			_aNAG _cRGU _dDLC _bENGLISH
042			_alccopycat
082	0	0	_a629.411 _bLAB-M
100	1		_aLabunsky, Alexei V. _eaut _929912
245	1	0	_aMultiple gravity assist interplanetary trajectories / _cAlexei V. Labunsky, Oleg V. Papkov, and Konstantin G. Sukhanov.
250			_aLibrary Edition: Particle & high energy physics
260			_aAustralia : _bGordon and Breach Science Publishers, _cc1998.
300			_avi, 285 p. : _bill. ; _c26 cm.
650		0	_aSpace trajectories. _929913
650		0	_aCelestial mechanics. _929914
650		0	_aOrbital mechanics. _929915
650		0	_aGravity assist (Astrodynamics) _929916
700	1		_aPapkov, Oleg V. _eaut _929917
700	1		_aSukhanov, Konstantin G. _eaut _929918
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.
830		0	_aEarth Space Institute book series on public and private sector interest in space ; _vv. 3. _929919
856	4	1	_3Table of contents _uhttp://www.loc.gov/catdir/toc/fy022/2002421707.html
856	4	2	_3Publisher description _uhttp://www.loc.gov/catdir/enhancements/fy0731/2002421707-d.html
942			_2ddc _cREF