发明名称 |
THRUST NOZZLE SYSTEM AND METHOD FOR THE ORBIT AND ATTITUDE CONTROL OF A GEOSTATIONARY SATELLITE |
摘要 |
A thrust nozzle system is provided for a satellite designed to be stabilized in autorotation over a geostationary orbit, the satellite comprising three reference axes X, Y and Z, the Y axis representing the North/South axis and the Z axis corresponding to an Earth pointing direction. The thrust nozzle system comprises a first set of thrust nozzles configured for maintaining the satellite in station, the first set comprising an even number of thrust nozzles using electrical propulsion, with a pre-adjusted orientation, the even number being equal to at least 4, the thrust nozzles being oriented along three spatial components, and having, taken in pairs, different signs of X and Y components. |
申请公布号 |
US2015307214(A1) |
申请公布日期 |
2015.10.29 |
申请号 |
US201414553801 |
申请日期 |
2014.11.25 |
申请人 |
THALES |
发明人 |
AMALRIC Joel |
分类号 |
B64G1/40;B64G1/10 |
主分类号 |
B64G1/40 |
代理机构 |
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代理人 |
|
主权项 |
1. A thrust nozzle system for a satellite designed to be stabilized in autorotation over a geostationary orbit, the said satellite comprising three reference axes X, Y and Z, the Y axis representing the North/South axis and the Z axis corresponding to an Earth pointing direction, comprising a first set of thrust nozzles configured for maintaining the satellite in station, the first set comprising an even number of thrust nozzles using electrical propulsion, with a pre-adjusted orientation, the said even number being equal to at least 4, the said thrust nozzles being oriented along three spatial components, and having, taken in pairs, different signs of X and Y components. |
地址 |
NEUILLY-SUR-SEINE FR |