USD1107629SActiveUtility

Cooling device for a rocket engine nozzle

10
Assignee: LETARA LTDPriority: Jan 19, 2024Filed: Jan 19, 2024Granted: Dec 30, 2025
Est. expiryJan 19, 2044(~17.5 yrs left)· nominal 20-yr term from priority
Inventors:Landon Thomas KampsShota Hirai
10
PatentIndex Score
0
Cited by
17
References
1
Claims

Claims

exact text as granted — not AI-modified
CLAIM 
     
       The ornamental design for a cooling device for a rocket engine nozzle as shown and described.

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