Multiphase investigation of water hammer phenomenon using the full cavitation model

J Pinho, M Lema, P Rambaud, J Steelant - Journal of Propulsion and …, 2014 - arc.aiaa.org
The aim of this work is to clarify some issues raised recently on the characterization of the
water hammer, by presenting a numerical analysis on the multiphysics taking place. For this …

航天器推进系统水击及其抑制方法

晏政, 彭小辉, 程玉强, 吴建军 - 航空动力学报, 2012 - jasp.com.cn
针对航天器推进系统充填和关机过程水击这一动力学问题, 基于已建立的航天器推进系统仿真
模型, 开展了某型推进系统的仿真研究, 并重点分析了节流孔, 弯管对推进剂供应管路水击的抑制 …

[PDF][PDF] Experimental characterization of the priming phase using a propellant line mock-up

M Lema, J Steelant, FP Lopez… - Space Propulsion …, 2012 - researchgate.net
The propulsion systems used in satellites can face fluid hammer effects, threatening system
integrity. Fluid hammer can be particularly adverse during the priming phase, which involves …

System dynamic characteristic simulation of spacecraft propulsion system based on AMESim

Z Yan, XH Peng, YQ Cheng, JJ Wu - Advanced Materials Research, 2013 - Trans Tech Publ
In order to investigate the dynamic characteristic of the spacecraft propulsion system,
numerical simulation was carried out based on the modular and extensible simulation model …

Experimental database with real propellants to study multi-phase fluid hammer phenomena

J Anthoine, JY Lestrade, J Steelant - Space Propulsion 2014, 2014 - onera.hal.science
The objective of the present study is to generate a reliable experimental database on the
fluid hammer phenomenon with real propellants (MMH and NTO) to validate the physical …

Modeling and Simulation of System Dynamics for Spacecraft Propulsion System

Z Yan, XH Peng, YQ Cheng, JJ Wu - Applied Mechanics and …, 2012 - Trans Tech Publ
The spacecraft propulsion system is used for geosynchronous orbit transfer, three-axis
stabilization and station-keeping. In order to investigate the system dynamics of spacecraft …