Patent Number: 6,308,514

Title: Rocket engine nozzle

Abstract: A rocket engine nozzle with an outlet portion having a curved profile inaxial section. In order to control the flow separation occurring withinthe nozzle outlet, the radius of the outlet portion, in axial section,varies circumferentially in length.

Inventors: Haggander; Jan (Trollhattan, SE), Pekkari; Lars-Olof (Ytterby, SE)

Assignee:

International Classification:

Expiration Date: 10/32013