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Palabras clave – provistas por la editorial

hybrid 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