000			03243nam a22004215i 4500
988			_aSpringer_Engineering_2020
999			_c116877 _d116877 _x1
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003			ES-MaUEC
005			20230104140223.0
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007			cr nn nnnaamaa
008			191010s2020 gw | s |||| 0|eng d
020			_a9783030269654
024	7		_a10.1007/978-3-030-26965-4 _2doi
040			_aES-MaUEC _bspa _cES-MaUEC _dES-MaUEC
050		4	_aTL782 _b2020 EB
100	1		_aKrishnan, Subramaniam _eautor _4aut _4http://id.loc.gov/vocabulary/relators/aut _9672036
245	1	0	_aChemical Rockets : _bPerformance Prediction and Internal Ballistics Design _cby Subramaniam Krishnan, Jeenu Raghavan.
250			_a1st ed. 2020.
264		1	_aCham _bSpringer International Publishing _c2020.
300			_a1 recurso en línea (XI, 538 páginas) _b23 ilustraciones, 2 ilustraciones a color
336			_2rdacontent _aTexto _btxt
337			_2rdamedia _aelectrónico _bc
338			_2rdacarrier _arecurso electrónico _bcr
347			_atext file _bPDF
490	0		_aSpringer Aerospace Technology _x1869-1730
490	0		_aEngineering (Springer-11647)
505	0		_aPartI: Performance Calculation of Chemical Propellants by Energy Minimization -- Chapter1: Introduction -- Chapter2: Chemical Potential -- Chapter3: Mass Balance -- Chapter4: Iteration Equations -- Chapter5: Thermodynamic Derivatives -- Chapter6: Thermodynamic Data -- Chapter7: Theoretical Rocket Performance -- PartII: Performance Prediction and Internal Ballistics Design of Solid Propellant Rocket Motors -- Chapter8: Introduction -- Chapter9: Equilibrium-Pressure Analysis -- Chapter10: Incremental Analysis -- Chapter11: Computer Program.
520			_aThe purpose of this book is to discuss, at the graduate level, the methods of performance prediction for chemical rocket propulsion. A pedagogical presentation of such methods has been unavailable thus far and this text, based upon lectures, fills this gap. The first part contains the energy-minimization to calculate the propellant-combustion composition and the subsequent computation of rocket performance. While incremental analysis is for high performance solid motors, equilibrium-pressure analysis is for low performance ones. Both are detailed in the book's second part for the prediction of ignition and tail-off transients, and equilibrium operation. Computer codes, adopting the incremental analysis along with erosive burning effect, are included. The material is encouraged to be used and presented at lectures. Senior undergraduate and graduate students in universities, as well as practicing engineers and scientists in rocket industries, form the readership.
650		7	_2embne _9669712 _aSistemas de propulsión
700	1		_aRaghavan, Jeenu _eautor _4aut _4http://id.loc.gov/vocabulary/relators/aut
776	0	8	_iPrinted edition: _z9783030269647
776	0	8	_iPrinted edition: _z9783030269661
776	0	8	_iPrinted edition: _z9783030269678
856	4	0	_uhttps://go.openathens.net/redirector/universidadeuropea.es?url=https://doi.org/10.1007/978-3-030-26965-4 _zAcceso a este recurso digital (usuarios Universidad Europea de Madrid)
942			_2lcc _cLE
998			_aSI _cm _dz _feng _ggw _h0 _b01/2020 _eIG _zSI