Feasibility Study on the Orbit Transfer utilizing the Tether System Dynamics in the Debris-Crowded Circular Orbit

Author(s):  
Shoichi Yoshimura
2019 ◽  
Vol 18 (2) ◽  
pp. 281-296 ◽  
Author(s):  
Fadilla Indrayuni Prastyasari ◽  
Dhimas Widhi Handani ◽  
A.A.B. Dinariyana ◽  
Miranto A. Prakoso

2012 ◽  
Vol 229-231 ◽  
pp. 2112-2116
Author(s):  
Zheng Yan ◽  
Xiao Hui Peng ◽  
Yu Qiang Cheng ◽  
Jian Jun Wu

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 propulsion system with complex pressurization pipelines and propellant supply pipelines, a modular and extensible simulator UPSSim was developed. The pressurant pipelines were separated into several nodes, each node used lumped parameter model; while the propellant feed pipelines used distributed parameter model. Heat transfer between components and environment was also taken into account. The model accurately predicts the transient behavior of the spacecraft propulsion system during start-up and shutdown process, as well as the effect of pipe initial pressure on the priming waterhammer amplitude. The simulation result demonstrates the adequacy of the modular modeling methodology for spacecraft propulsion system dynamic simulation.


2008 ◽  
Vol 31 (4) ◽  
pp. 1014-1027 ◽  
Author(s):  
Yoshihiro Ichimura ◽  
Akira Ichikawa

2011 ◽  
Vol 34 (5) ◽  
pp. 1329-1341 ◽  
Author(s):  
Ryo Jifuku ◽  
Akira Ichikawa ◽  
Mai Bando

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