000 | 01664nam a2200121Ia 4500 | ||
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008 | 220620s9999||||xx |||||||||||||| ||und|| | ||
245 | 0 | _aAdvances in Hybrid Rocket Technology and Related Analysis Methodologies | |
546 | _aEnglish[eng] | ||
650 | _ahybrid rocket||marine propulsion||rupture disc||idling operation||underwater environment||hybrid rocket engines||multidisciplinary design optimization||robust optimization||electric feed system||ballistic reconstruction technique||fuel regression||nozzle erosion||c∗ efficiency||hybrid||regression rate||self-disintegration||HTPB||paraffin||low-energy polymer||magnesium||fuel regression rate||internal ballistics||computational fluid dynamics||hybrid rocket propulsion||swirl oxidizer injection||feedback loop control||error propagation analysis||resistor-based sensors||rocket||regression||Marxman||diffusion-limited||blowing factor||3D printing||fuel grain||hybrid combustion||modeling and simulation||hybrid propulsion||paraffin-based fuel||oxygen||combustion||testing||nano-sized aluminum||micron-sized aluminum||fluoropolymer||mechanically activated aluminum||coated aluminum||fuel-rich composite powder||aluminum aggregation||aluminum agglomeration||mass burning rate||n/a||“green†propellants||nitrous oxide decomposition||energy of activation||3-D printing||hybrid rocket engine||sounding rocket||carbon fiber composite||engine test||total impulse||lightweight design||ignition system||gas torch||methane-oxygen combustion||vortex combustion chamber||hybrid rocket motor||ramjet motor | ||
700 | _aCarmicino, Carmine | ||
856 | _uhttps://mdpi.com/books/pdfview/book/3180 | ||
942 | _cEB | ||
999 |
_c30289 _d30289 |