Cooling Device for a Rocket Engine Nozzle
Claims (1)
The ornamental design for a cooling device for a rocket engine nozzle as shown and described.
Full Description
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1. Cooling device for a rocket engine nozzle
FIG. 1 . 1 : Front perspective view of a cooling device for a rocket engine nozzle.
FIG. 1 . 2 : Front view thereof.
FIG. 1 . 3 : Rear view thereof.
FIG. 1 . 4 : Plan view thereof.
FIG. 1 . 5 : Bottom view thereof.
FIG. 1 . 6 : Cross-sectional view thereof taken through front to back center, and sectioned horizontally at the center of the front view.
FIG. 1 . 7 : Cross-sectional view thereof taken through front to back center, and sectioned horizontally at the center of the plan view.
FIG. 1 . 8 : Cross-sectional view thereof taken through front to back center, and sectioned horizontally at the center of the plan view.
FIG. 1 . 9 : Cross-sectional view thereof sectioned vertically at the center of the plan view.
FIG. 1 . 10 : Right side view thereof.
FIG. 1 . 11 : Left side view thereof.
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.
Citations
This patent cites (9)
- US10697393
- US10808646
- US12092023
- US12371319
- US2015/0377178
- US2016/0201544
- US2016/0265773
- US2025/0033957
- US2025/0230784