000 | 03240nam a22005535i 4500 | ||
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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 |
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024 | 7 |
_a10.1007/3-540-37645-3 _2doi |
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050 | 4 | _aTL787-4050.22 | |
072 | 7 |
_aTRP _2bicssc |
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072 | 7 |
_aTTDS _2bicssc |
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072 | 7 |
_aTEC002000 _2bisacsh |
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082 | 0 | 4 |
_a629.1 _223 |
100 | 1 |
_aKemble, Stephen. _eauthor. |
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245 | 1 | 0 |
_aInterplanetary Mission Analysis and Design _h[electronic resource] / _cby Stephen Kemble. |
264 | 1 |
_aBerlin, Heidelberg : _bSpringer Berlin Heidelberg, _c2006. |
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300 |
_aXXXVI, 484 p. _bonline resource. |
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336 |
_atext _btxt _2rdacontent |
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337 |
_acomputer _bc _2rdamedia |
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338 |
_aonline resource _bcr _2rdacarrier |
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347 |
_atext file _bPDF _2rda |
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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 |