#13282. Изучение характеристик твердотопливных магниевых и алюминиевых соединений и их сравнения с распространенными твердотопливными материалами

September 2026publication date
Proposal available till 13-05-2025
4 total number of authors per manuscript5500 $

The title of the journal is available only for the authors who have already paid for
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Journal’s subject area:
Aerospace Engineering or
Mechanical Engineering or
Space And Planetary Science or
Fuel Technology
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Abstract:
a series of static fire tests of solid-fuel hybrid rocket engines was carried out
Experimental materials included polylactic acid with magnesium particles, polylactic acid with aluminum particles and, for comparison, acrylonitrile butadiene styrene, acrylonitrile styrene-acrylate, polypropylene, polyethylene terephthalate glycol
To test the performance of fuel grains, an experimental setup with a set of sensors was designed and manufactured.
Keywords:
magnesium, aluminum, polylactic acid, rocket fuel, solid propellant charges, solid propellant rocket engines, fuel combustion, regression rate

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