发明公开
EP3212503A1 SATELLITE ARTIFICIEL ET PROCÉDÉ DE REMPLISSAGE D'UN RÉSERVOIR DE GAZ PROPULSIF DUDIT SATELLITE ARTIFICIEL
有权
SATELLITE ARTIFICIEL ETPROCÉDÉDE REMPLISSAGE D'UNRÉSERVOIRDE GAZ PROPULSIF DUDIT SATELLITE ARTIFICIEL
- 专利标题： SATELLITE ARTIFICIEL ET PROCÉDÉ DE REMPLISSAGE D'UN RÉSERVOIR DE GAZ PROPULSIF DUDIT SATELLITE ARTIFICIEL
- 专利标题（英）： Artificial satellite and method for filling a tank of propellent gas of said artificial satellite
- 专利标题（中）： SATELLITE ARTIFICIEL ETPROCÉDÉDE REMPLISSAGE D'UNRÉSERVOIRDE GAZ PROPULSIF DUDIT SATELLITE ARTIFICIEL
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申请号： EP16705226.5申请日： 2016-01-22
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公开(公告)号： EP3212503A1公开(公告)日： 2017-09-06
- 发明人: WALKER, Andrew, Nicholas
- 申请人： Airbus Defence and Space SAS
- 申请人地址： 51-61 Route de Verneuil 78130 Les Mureaux FR
- 专利权人： Airbus Defence and Space SAS
- 当前专利权人： Airbus Defence and Space SAS
- 当前专利权人地址： 51-61 Route de Verneuil 78130 Les Mureaux FR
- 代理机构： Cabinet Plasseraud
- 优先权： FR1550613 20150127
- 国际公布： WO2016120547 20160804
- 主分类号： B64G1/40
- IPC分类号： B64G1/40 ; B64G1/50 ; B64G1/64
摘要：
The invention relates to an artificial satellite which includes: a mounting structure supporting equipment-bearing walls; a launcher-adapter rigidly connected to the mounting structure; a first radiator (26); and at least one first system (42) for transporting heat by a fluid, including at least one duct (44) having a first heat-exchange section (50) and a second heat-exchange section (52), said second heat-exchange section (52) being capable of being in thermal contact with said first radiator (26), characterised in that said first heat-exchange section (50) is in thermal contact with at least one portion of the launcher-adapter (16). The invention also relates to a method for filling a tank of propellent gas of said artificial satellite.
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