A Study on Flow Characteristics of Pressure-Controlled Propellant Crossfeed in Liquid Rocket Systems[J]. 2020, 54(4): 165-172.
DOI:
A Study on Flow Characteristics of Pressure-Controlled Propellant Crossfeed in Liquid Rocket Systems[J]. 2020, 54(4): 165-172.DOI: 10.7652/xjtuxb202004020.
A Study on Flow Characteristics of Pressure-Controlled Propellant Crossfeed in Liquid Rocket Systems
A numerical model is developed to study the dynamic characteristics of the propellant cross-feeding process. The model is based on the software AMEsim and adopts the modulari-ation idea to model the pressuri-ation
storage tank
pipeline feeding system and other functional modules. The crossfeed model is validated by experimental data
and consistency between the calculated and measured data is found. Then
the flow characteristics and the corresponding influencing factors during the pressure-controlled crossfeed process are analy-ed. The results show that there is a critical pressure to guarantee the full tank of core stage after booster separation
and the critical value is dependent on the initial propellant amount
the flight overload
and the volume flow rate. The initial refueling amount of the boost stage has no significant influence on the water hammer pressure under the critical pressure. However
an increase in the volume flow rate leads to an increase of water hammer pressur
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