Patents.us
Patents/USD1107629

Cooling Device for a Rocket Engine Nozzle

USD1107629No. D 1,107,629designGranted 12/30/2025

Claims (1)

Claim 1 (Independent)

The ornamental design for a cooling device for a rocket engine nozzle as shown and described.

Full Description

Show full text →

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