Controlled-emission solar tabs for attitude solar sailing

Details Controlled-emission solar tabs for attitude solar sailing Controlled-emission solar tabs for attitude solar sailing

B - Operations, Transporting

64

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B64G 1/24 (2006.01) B64G 1/28 (2006.01) B64G 1/40 (2006.01) B64G 1/44 (2006.01)

Patent

CA 2198046

Solar tabs are provided which have thermal emissivity and absorptivity properties designed to increase the attitude-control torques that can be generated with rotatable wings in a spacecraft. These increased torques enhance the ability to offset attitude- disturbance torques which typically tend to alter the attitude of a spacecraft from a desired attitude. The tabs include highly absorptive and nonemissive front faces, highly emissive back faces and a high thermal conductivity between the front faces and the back faces.

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