Thermal insulating blanket for spacecraft, and spacecraft...

B - Operations – Transporting – 64 – G

Patent

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Details

B64G 1/58 (2006.01) B64G 1/64 (2006.01)

Patent

CA 2223534

The structure of a spacecraft, such as a satellite, is covered at least partially by a thermal insulating blanket assembled out of a number of pieces (14) that are zippered together (16). Zippers (18) are also used to attach the pieces (14) to the structure of the satellite.

La structure d'un engin spatial tel qu'un satellite est recouverte au moins partiellement d'une couverture thermiquement isolante obtenue en assemblant bord à bord plusieurs morceaux (14), au moyen de fermetures à glissières (16). Des fermetures à glissières (18) sont aussi utilisées pour fixer les morceaux (14) sur la structure du satellite.

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