Cooling device for a rocket engine nozzle
1. Cooling device for a rocket engine nozzle
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This product is a cooling device for a rocket engine nozzle, and more specifically, is a nozzle case for cooling the nozzle from the outside. The broken lines in the drawings illustrate portions of the cooling device for a rocket engine nozzle that form no part of the claimed design.
Claims
The ornamental design for a cooling device for a rocket engine nozzle as shown and described.
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Type: Grant
Filed: Jan 19, 2024
Date of Patent: Dec 30, 2025
Assignee: Letara Ltd. (Sapporo)
Inventors: Landon Thomas Kamps (Sapporo), Shota Hirai (Sapporo)
Primary Examiner: Darlington Ly
Assistant Examiner: Jessica Lynn Devilbiss
Application Number: 35/520,425