Measurements and modeling of the density of rocket propellant RP-2 at temperatures to 573 K and pressures to 100 MPa
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DOI: 10.1016/j.fuel.2019.05.089
Abstract: Abstract Liquid rocket propellants are subject to wide ranges of temperature and pressure when flowing through high performance liquid rocket engines. For example, as rocket propellant (RP) is used for regenerative cooling, near-wall fluid temperatures… read more here.
Keywords: rocket propellant; 573 pressures; density; temperatures 573 ... See more keywords