Patents Assigned to Nammo Faufoss AS
  • THERMAL INSULATION OF ROCKET ENGINES
    Publication number: 20130192215
    Abstract: The present invention is related to an improved thermal insulation of an exhaust tube (6) for use in a rocket engine. The thermal insulation is provided for as a layered structure wherein respective layers comprises a composite material, and wherein dominant directions of fibres in respective adjacent layers are different with respect to each other. In addition, a flexible layer might be used to attach the thermal insulation to an inner wall of the exhaust tube (6).
    Type: Application
    Filed: October 11, 2011
    Publication date: August 1, 2013
    Applicant: Nammo Faufoss AS
    Inventor: Erland Ørbekk