000 03240nam a22005535i 4500
001 978-3-540-37645-3
003 DE-He213
005 20161121231121.0
007 cr nn 008mamaa
008 100301s2006 gw | s |||| 0|eng d
020 _a9783540376453
_9978-3-540-37645-3
024 7 _a10.1007/3-540-37645-3
_2doi
050 4 _aTL787-4050.22
072 7 _aTRP
_2bicssc
072 7 _aTTDS
_2bicssc
072 7 _aTEC002000
_2bisacsh
082 0 4 _a629.1
_223
100 1 _aKemble, Stephen.
_eauthor.
245 1 0 _aInterplanetary Mission Analysis and Design
_h[electronic resource] /
_cby Stephen Kemble.
264 1 _aBerlin, Heidelberg :
_bSpringer Berlin Heidelberg,
_c2006.
300 _aXXXVI, 484 p.
_bonline resource.
336 _atext
_btxt
_2rdacontent
337 _acomputer
_bc
_2rdamedia
338 _aonline resource
_bcr
_2rdacarrier
347 _atext file
_bPDF
_2rda
490 1 _aSpringer Praxis Books
505 0 _aInterplanetary missions -- Spacecraft propulsion -- Optimisation -- Special techniques -- Missions to the planets.
520 _aThe book describes current mission analysis and design techniques that may be applied to a very wide range of interplanetary missions from those targeting the inner planets to those destined for the outer planets and Solar System escape trajectories. The early chapters comprise an introduction and a description of the fundamentals of interplanetary missions, aspects of leaving Earth and planet orbit selection and insertion. A discussion of various propulsion systems for interplanetary transfer is followed by a detailed overview of transfer techniques, including the principles of gravity assist and a range of applications of this technique, low-thrust transfers in combination with gravity assist and for planetary escape and capture and the utilisation of multi-body gravity perturbations. The final chapter deals with various optimisation methods for interplanetary missions. The dynamics of the problems are analysed and algorithms that may be used to solve the problems are presented. Practical difficulties that may be encountered are also discussed. The mission design options are considered in the context of spacecraft types, ranging from high thrust, nuclear thermal rockets to low thrust ion propulsion systems. A series of specific examples are described in detail in the appendices, covering ‘end-to-end’ mission design for some topical space mission scenarios.
650 0 _aEngineering.
650 0 _aSpace sciences.
650 0 _aVibration.
650 0 _aDynamical systems.
650 0 _aDynamics.
650 0 _aAutomotive engineering.
650 0 _aAerospace engineering.
650 0 _aAstronautics.
650 1 4 _aEngineering.
650 2 4 _aAerospace Technology and Astronautics.
650 2 4 _aExtraterrestrial Physics, Space Sciences.
650 2 4 _aVibration, Dynamical Systems, Control.
650 2 4 _aAutomotive Engineering.
710 2 _aSpringerLink (Online service)
773 0 _tSpringer eBooks
776 0 8 _iPrinted edition:
_z9783540299134
830 0 _aSpringer Praxis Books
856 4 0 _uhttp://dx.doi.org/10.1007/3-540-37645-3
912 _aZDB-2-ENG
950 _aEngineering (Springer-11647)
999 _c508833
_d508833