Launcher stage comprising a temporary support structure for temporarily supporting nozzle sections allowing access to the core of the engine
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United States of America Patent
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Jun 5, 2018
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app pub date -
Apr 12, 2013
filing date -
Apr 13, 2012
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Abstract
A stage of a space launcher including an engine core, a tank secured above the engine core, and a nozzle including a first deployable nozzle section secured below the engine core, the nozzle further including a second and a third section configured to be situated extending from each other when the nozzle is in a deployed propulsion configuration. The stage further includes a structure for temporarily supporting nozzle sections mounted on the tank, configured to change the nozzle to a configuration for accessing the engine core wherein the nozzle sections are inserted into each other, with the third section bearing against a lower support of the temporary structure.
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