| 000 | 01734mc a2200421a 44500 | ||
|---|---|---|---|
| 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. |
||
| 260 |
_aReston _bAmerican Institute of Aeronautics and Astronautics |
||
| 300 |
_axxvii, 1293 p. _bgráficos |
||
| 490 |
_aProgress in astronautics and aeronautics _v189 |
||
| 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 |
||
| 800 |
_aZarchan, Paul _95730 |
||
| 942 | _cBK | ||
| 999 |
_c382 _d382 |
||