A device for controlling a spacecraft by gating gas via a...

B - Operations – Transporting – 64 – G

Patent

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B64G 1/26 (2006.01) F02K 9/86 (2006.01)

Patent

CA 2188393

A device for controlling a spacecraft by gating gas, the device comprising a nozzle (20), a gas feed duct (12), a gate having a seat (22) and a plunger (18) interposed between the feed duct and the nozzle, and control means (40) for opening and closing the gate in order to put the feed duct selectively into communication with the nozzle. The seat (22) of the gate is secured to the nozzle (20) and the nozzle is movable such that the gate is opened and closed by displacement of the nozzle, which displacement is driven directly by the hot gas, without calling on an auxiliary fluid.

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