2021
DOI: 10.1016/j.actaastro.2021.08.046
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Analysis of dynamic characteristics and sensitivity of hydrogen-oxygen expansion cycle rocket engine system

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Cited by 16 publications
(5 citation statements)
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“…Gravity in pipes is not accounted for and the model is 1D with homogenous flow (no slip between the phases, homogenous temperature in the volume). The two-phase fluid obeys the Helmholtz energy law (as in [38]) for water mixtures. The Maxwell criterion is used to calculate the fluid saturation curve (as in [39]).…”
Section: A Numerical Simulation Modelmentioning
confidence: 99%
“…Gravity in pipes is not accounted for and the model is 1D with homogenous flow (no slip between the phases, homogenous temperature in the volume). The two-phase fluid obeys the Helmholtz energy law (as in [38]) for water mixtures. The Maxwell criterion is used to calculate the fluid saturation curve (as in [39]).…”
Section: A Numerical Simulation Modelmentioning
confidence: 99%
“…where, Q is the volume flow, and N is the pump speed. According to the definition of θ and specific speed (N S ) in Equation ( 2), the head function (W H) and torque function (WT) are defined in Equation ( 3) [8].…”
Section: Electric Pumpmentioning
confidence: 99%
“…The turbine pump feed system uses the pump to pressurize the propellant, which greatly reduces the mass of the tank and improves the thrust chamber pressure. These engines have high specific impulse [7][8][9]. However, the structure of these engines is complex, generally including components such as gas generators, turbines, and centrifugal pumps.…”
Section: Introductionmentioning
confidence: 99%
“…To ensure the atomization effect, the injector pressure drop is taken as 0.2 times of the combustion chamber pressure [2]. The pressure drop is mainly considering the valve, venturi and filter, etc.…”
Section: Engine Balance Parametersmentioning
confidence: 99%
“…Meanwhile, the turbopump feeding system is unqualified for repeated startups due to intricate structure and small range of thrust adjustment. The rocket engine with hydrogen peroxide and electric pumps is an important step toward a non-toxic, non-polluting and storable propellant system [1][2][3].…”
Section: Introductionmentioning
confidence: 99%