Invention Grant
- Patent Title: Radiator deployable for a satellite stabilized on three axes
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Application No.: US15103834Application Date: 2014-12-15
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Publication No.: US10207824B2Publication Date: 2019-02-19
- Inventor: Jérôme Lemaire , Yann Miegeville
- Applicant: AIRBUS DEFENCE AND SPACE SAS , THALES , CENTRE NATIONAL D'ETUDES SPATIALES CNES
- Applicant Address: FR Toulouse FR Neuilly sur Seine FR Paris
- Assignee: AIRBUS DEFENCE AND SPACE SAS,THALES,CENTRE NATIONAL D'ETUDES SPATIALES CNES
- Current Assignee: AIRBUS DEFENCE AND SPACE SAS,THALES,CENTRE NATIONAL D'ETUDES SPATIALES CNES
- Current Assignee Address: FR Toulouse FR Neuilly sur Seine FR Paris
- Agency: Im IP Law
- Agent C. Andrew Im; Chai Im
- Priority: FR1362606 20131213
- International Application: PCT/EP2014/077746 WO 20141215
- International Announcement: WO2015/086851 WO 20150618
- Main IPC: B64G1/44
- IPC: B64G1/44 ; B64G1/22 ; B64G1/50 ; B64G1/66 ; F28D15/00 ; F28D15/02 ; F28F1/00 ; F28D21/00

Abstract:
A photovoltaic generator deployable for a satellite stabilized on three axes. The photovoltaic generator includes an assembly of planar panels articulated with respect to each other, and an attachment arm to the structure of the body of the satellite. In a first or launch position of the photovoltaic generator, the planar panels are folded one over the other. In a second or deployed position of the photovoltaic generator, the planar panels are fully deployed with at least a part of the planar panels being photovoltaic panels. At least one planar panel consists of a thermal radiator, with the radiative face thereof being orientated to be opposite the face of the photovoltaic panels carrying the photovoltaic sensors when the photovoltaic generator is in the deployed position. This radiative face is termed the “shade” face, and the face opposite the panel shaped radiator is termed the “sun” face.
Public/Granted literature
- US20160311561A1 RADIATOR DEPLOYABLE FOR A SATELLITE STABILIZED ON THREE AXES Public/Granted day:2016-10-27
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