New Thruster System for Small Satellite : Gas-Liquid Equilibrium Thruster
スポンサーリンク
概要
- 論文の詳細を見る
In the proposed gas-liquid equilibrium thruster, fuel is mainly stored in the liquid phase in the tank and is ejected in the gas phase, powered by the vapor pressure of the fuel. As compared to conventional thrusters, the thrust level of this thruster is low. However, the system configuration of this thruster is simple because components such as combustors or high-pressure reservoirs are not required. Further, this thruster is lighter than other thrusters. Fuels with low toxicity and that are easily available can be selected in this thruster from many kinds of fuel candidates. As a result, this thruster can be easily handled. This thruster can be used as an actuator for controlling the attitude and maneuvering the orbit of small satellites.
- THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCESの論文
THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES | 論文
- Study on Ignition and Electron Emission Characteristics of Inductively Coupled Plasma Cathode
- Research and Development of a Debris Removal Method Using Interaction between Space and Electrode with Applied Voltage
- Disaster Monitoring Using ALOS/PALSAR Data
- Design and Experimental Validation of Inter-Satellite Link System for Formation Flight SCOPE Mission
- Magnetic Inflation of Magnetic Plasma Sail by One Component Plasma Simulation