The present invention also relates to a method for using said device (105) for connecting two segments (103a, 103b) of a nozzle (3), as well as to a propelling nozzle (3) thus assembled and to a rocket engine (1) including same.
The invention relates to the field of propelling nozzles, and in particular to a device (105) for connecting a first segment (103a) and a second segment (103b) of a propelling nozzle, made of thermally dissimilar materials.
The action is the force produced by the expulsion of gasses of combustion from the nozzle.
Requêtes fréquentes français :1-200, -1k, -2k, -3k, -4k, -5k, -7k, -10k, -20k, -40k, -100k, -200k, -500k, -1000k,
Requêtes fréquentes anglais :1-200, -1k, -2k, -3k, -4k, -5k, -7k, -10k, -20k, -40k, -100k, -200k, -500k, -1000k,
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