Cooling device for a rocket engine nozzle

USD1107629SActive Publication Date: 2025-12-30LETARA LTD
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Patent Information

Application Number
US35/520425
Authority / Receiving Office
US · United States
Patent Type
Designs(United States)
Current Assignee / Owner
Priority Date
2024-01-19
Filing Date
2024-01-19
Publication Date
2025-12-30
Estimated Expiration
2040-12-30

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Description

[0001] 1. Cooling device for a rocket engine nozzle

[0002] FIG. 1.1: Front perspective view of a cooling device for a rocket engine nozzle.

[0003] FIG. 1.2: Front view thereof.

[0004] FIG. 1.3: Rear view thereof.

[0005] FIG. 1.4: Plan view thereof.

[0006] FIG. 1.5: Bottom view thereof.

[0007] FIG. 1.6: Cross-sectional view thereof taken through front to back center, and sectioned horizontally at the center of the front view.

[0008] FIG. 1.7: Cross-sectional view thereof taken through front to back center, and sectioned horizontally at the center of the plan view.

[0009] FIG. 1.8: Cross-sectional view thereof taken through front to back center, and sectioned horizontally at the center of the plan view.

[0010] FIG. 1.9: Cross-sectional view thereof sectioned vertically at the center of the plan view.

[0011] FIG. 1.10: Right side view thereof.

[0012] FIG. 1.11: Left side view thereof.

[0013] 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.

Citation Information

Patent Citations

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