000			03174nam a22004455i 4500
710	2		_aSpringerLink (Online service) _9106996
999			_c102516 _d102516 _x1
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003			ES-MaUEC
005			20230102113045.0
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007			cr nn 008mamaa
008			170831s2018 gw | s |||| 0|eng d
020			_a9783662547441
024	7		_a10.1007/978-3-662-54744-1 _2doi
040			_aES-MaUEC _bspa _cES-MaUEC _dES-MaUEC
050		4	_aTL782 _b2018 EB
100	1		_aCzysz, Paul A. _eautor _9672985
245	1	0	_aFuture Spacecraft Propulsion Systems and Integration. _bEnabling Technologies for Space Exploration _cby Paul A. Czysz, Claudio Bruno, Bernd Chudoba
250			_a3rd edition
264		1	_aBerlin, Heidelberg _bSpringer International Publishing _c2018
300			_a1 recurso en línea (LXI, 463 páginas 349) _bilustraciones
336			_2rdacontent _aTexto _btxt
337			_2rdamedia _aelectrónico _bc
338			_2rdacarrier _arecurso electrónico _bcr
490	0		_aAstronautical Engineering, _x2365-9599
490	0		_aEngineering (Springer-11647)
505	0		_aOverview -- Our progress appears to be impeded -- Commercial near-Earth space launcher: a perspective -- Commercial near-Earth launcher: propulsion -- Earth orbit on-orbit operations in near-Earth orbit, a necessary second step -- Earth-Moon system: establishing a Solar System presence -- Exploration of our Solar System -- Stellar and interstellar precursor missions -- View to the future and exploration of our Galaxy.
520	3		_aThe updated and expanded third edition of this book focuses on the multi-disciplinary coupling between flight-vehicle hardware alternatives and enabling propulsion systems. It discusses how to match near-term and far-term aerospace vehicles to missions and provides a comprehensive overview of the subject, directly contributing to the next-generation space infrastructure, from space tourism to space exploration. This holistic treatment defines a mission portfolio addressing near-term to long-term space transportation needs covering sub-orbital, orbital and escape flight profiles. In this context, a vehicle configuration classification is introduced covering alternatives starting from the dawn of space access. A best-practice parametric sizing approach is introduced to correctly design the flight vehicle for the mission. This technique balances required mission with the available vehicle solution space and is an essential capability sought after by technology forecasters and strategic planners alike.
988			_aEBSPRINGER_2018
650		7	_2embne _9139696 _aVehículos espaciales
650		7	_2embne _9669712 _aSistemas de propulsión
700	1		_aBruno, Claudio _eautor _9672986
700	1		_aChudoba, Bernd. _eautor _9671593
776	0	8	_iEdición impresa: _z9783662547427
776	0	8	_iEdición impresa: _z9783662547434
776	0	8	_iEdición impresa: _z9783662572085
856	4	0	_uhttps://go.openathens.net/redirector/universidadeuropea.es?url=https://doi.org/10.1007/978-3-662-54744-1 _zAcceso a este recurso digital (usuarios Universidad Europea de Madrid)
942			_2lcc _cLE
998			_b04/2020 _dz _ek _zSI