000 | 01734mc a2200421a 44500 | ||
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001 | NM000382 | ||
003 | AR-HaUTN | ||
007 | ta | ||
008 | 68020sc. 2 ||||||||||||||000 | spa|| | ||
005 | 20240917164003.0 | ||
020 | _a1563473224 | ||
040 | _aAR-HaUTN | ||
245 |
_aScramjet propulsion _c , Curran. E. T. |
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260 |
_aReston _bAmerican Institute of Aeronautics and Astronautics |
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300 |
_axxvii, 1293 p. _bgráficos |
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490 |
_aProgress in astronautics and aeronautics _v189 |
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500 | _aResúmenes, referencias bibliográficas, lecturas recomendadas y apéndices, al final de cada capítulo | ||
505 | _tScramjet testing in the T3 and T4 hypersonic impulse facilities | ||
505 | _tCramjet developments in France | ||
505 | _tScramjet investigations within the german Hypersonics Technology Program (19931996) | ||
505 | _tScramjet engine research at the National Space Laboratory in Japan | ||
505 | _tScramjet research and development in Russia | ||
505 | _tScramjet performance | ||
505 | _tCramjet inlets | ||
505 | _tSupersonic flow combustors | ||
505 | _tAerothermodynamics of the dualmode combustion system | ||
505 | _tBasic performance assessment of scram combustors | ||
505 | _tStrutjet rocketbased combinedcycle engine | ||
505 | _tLiquid hydrocarbon fuels for hypersonic propulsion | ||
505 | _tDetonationwawe ramjets | ||
505 | _tProblem of hypersonic flow deceleration by magnetic field | ||
505 | _tRudiments an methodology for design and analysis of hypersonic airbreathing vehicles | ||
505 | _tTransatmospheric launcher sizing | ||
505 | _tScramjet flowpath integration | ||
700 |
_aCurran. E. T. _95729 |
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800 |
_aZarchan, Paul _95730 |
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942 | _cBK | ||
999 |
_c382 _d382 |